Patent Application
20240363302
An aspect of the present invention relates to a photoelectric conversion device, an electromagnetic wave detection device, a photoelectric conversion method and an electromagnetic wave detection method.
Typically there are four types of electron emission such as thermionic emission, photoelectric emission, secondary emission, and field emission. The thermionic emission is achieved by heating electrode. The photoelectric emission is achieved by application of photons. The secondary emission is achieved by bombarding light speed electron. The field emission is achieved in the presence of electrostatic field. US Patent Application Publication No. 2016/0216201 illustrates an electromagnetic wave detection system which detects an electromagnetic wave. The system includes a photoelectric conversion device which converts an electromagnetic wave into an electron. The photoelectric conversion device is provided with an electron emitter having a metamaterial structure. The system detects an electromagnetic wave entering the electron emitter.
The electron emitter of the photoelectric conversion device mentioned above emits an electron in response to incidence of the electromagnetic wave. The system detects the entered electromagnetic wave, based on the electron emitted from the electron emitter. According to the system mentioned above, for example, a terahertz-wave can be detected.
There is a demand for detecting the polarization state of the entered electromagnetic wave. For detecting the polarization state, it is conceivable to use an optical system in which a polarizer and a detector are combined. For example, an optical system in which a wire grid and a detector are combined is used. However, when such an optical system is used, the structure of the device is complicated, and the cost of detecting the polarization state is high.
An object of an aspect of the present invention is to provide a photoelectric conversion device capable of easily achieving detection of the polarization state of an electromagnetic wave. An object of another aspect of the present invention is to provide an electromagnetic wave detection device capable of easily detecting the polarization state of an electromagnetic wave. An object of yet another aspect of the present invention is to provide a photoelectric conversion method capable of easily achieving detection of the polarization state of an electromagnetic wave. An object of another aspect of the present invention is to provide an electromagnetic wave detection method capable of easily detecting the polarization state of an electromagnetic wave.
A photoelectric conversion device according to an aspect of the present invention is provided with an electron emitter. The electron emitter includes a meta-surface emitting an electron in response to incidence of an electromagnetic wave. The meta-surface includes a first antenna portion, a first bias portion, a second antenna portion, and a second bias portion. The first antenna portion extends in a first direction and emits an electron in response to incidence of the electromagnetic wave. The first bias portion faces the first antenna portion and is configured to generate an electric field having a component in the first direction between the first bias portion and the first antenna portion. The second antenna portion extends in a second direction intersecting the first direction and emits an electron in response to incidence of the electromagnetic wave. The second bias portion faces the second antenna portion and is configured to generate an electric field having a component in the second direction between the second bias portion and the second antenna portion.
In this photoelectric conversion device, the first antenna portion and the second antenna portion extend in the first and second directions, which intersect with each other. The first bias portion is configured to generate an electric field having a component in the first direction between the first bias portion and the first antenna portion. The second bias portion is configured to generate an electric field having a component in the second direction between the second bias portion and the second antenna portion. According to such a configuration, the first antenna portion emits an electron according to the component in the first direction of the electric field strength of the entered electromagnetic wave. The second antenna portion emits an electron according to the component in the second direction of the electric field strength of the entered electromagnetic wave. As a result, there can be detected an electron emitted according to the component in the first direction of the electric field strength of the entered electromagnetic wave and an electron emitted according to the component in the second direction of the electric field strength of the entered electromagnetic wave. With the detection of them, detection of the polarization state of an electromagnetic wave can be easily achieved.
In the aspect mentioned above, the photoelectric conversion device may further include a potential control unit configured to control electric potentials applied to the meta-surface. The potential control unit may switch between a first state and a second state and switch between a third state and a fourth state by controlling the electric potentials applied to the meta-surface. In the first state, a component of an electric field from the first bias portion toward the first antenna portion in the first direction may be positive. In the second state, a component of an electric field from the first bias portion toward the first antenna portion in the first direction may be negative. In the third state, a component of an electric field from the second bias portion toward the second antenna portion in the second direction may be positive. In the fourth state, a component of an electric field from the second bias portion toward the second antenna portion in the second direction may be negative. In this case, when the electromagnetic wave enters the meta-surface in the first state, the electron is emitted from the first antenna portion according to the positive component in the first direction of the electric field strength of the entered electromagnetic wave. When the electromagnetic wave enters the meta-surface in the second state, the electron is emitted from the first antenna portion according to the negative component in the first direction of the electric field strength of the entered electromagnetic wave. When the electromagnetic wave enters the meta-surface in the third state, the electron is emitted from the second antenna portion according to the positive component in the second direction of the electric field strength of the entered electromagnetic wave. When the electromagnetic wave enters the meta-surface in the fourth state, the electron is emitted from the second antenna portion according to the negative component in the second direction of the electric field strength of the entered electromagnetic wave. Therefore, the photoelectric conversion device can achieve measurement of the electric field strength of the electromagnetic wave entering the electron emitter for each polarity in each of the first direction and the second direction by detecting the electron emitted from the meta-surface in each of the states. As a result, the detection of the polarization state of the electromagnetic wave can be achieved more accurately.
In the aspect mentioned above, the first antenna portion may include first and second leading ends which are disposed at mutually different positions in the first direction. The first bias portion may include a first portion and a second portion. The first portion may face the first leading end and generate an electric field having a component in the first direction between the first portion and the first leading end. The second portion may face the second leading end and generate an electric field having a component in the first direction between the second portion and the second leading end. The second antenna portion may include third and fourth leading ends which are disposed at mutually different positions in the second direction. The second bias portion may include a third portion and a fourth portion. The third portion may face the third leading end and generate an electric field having a component in the second direction between the third portion and the third leading end. The fourth portion may face the fourth leading end and generate an electric field having a component in the second direction between the fourth portion and the fourth leading end. In the first direction, the second portion, the second leading end, the first leading end, and the first portion may be disposed in this order. In the second direction, the fourth portion, the fourth leading end, the third leading end, and the third portion may be disposed in this order. In this case, the measurement of the electric field strength of the electromagnetic wave entering the electron emitter can be achieved for each polarity in each of the first direction and the second direction by detecting the electron emitted from the meta-surface, with a simple configuration.
In the aspect mentioned above, a potential control unit configured to control electric potentials applied to the meta-surface may be further included. The potential control unit may switch between a first state and a second state and switch between a third state and a fourth state by controlling the electric potentials applied to the meta-surface. In the first state, a component of the electric field from the first leading end toward the first portion in the first direction may be positive, a component of the electric field from the second portion toward the second leading end in the first direction may be positive, a component of the electric field from the third leading end toward the third portion in the second direction may be positive, and a component of the electric field from the fourth leading end toward the fourth portion in the second direction may be negative. In the second state, a component of the electric field from the first portion toward the first leading end in the first direction may be negative, a component of the electric field from the second leading end toward the second portion in the first direction may be negative, a component of the electric field from the third leading end toward the third portion in the second direction may be positive, and a component of the electric field from the fourth leading end toward the fourth portion in the second direction may be negative. In the third state, a component of the electric field from the first leading end toward the first portion in the first direction may be positive, a component of the electric field from the second leading end toward the second portion in the first direction may be negative, a component of the electric field from the third leading end toward the third portion in the second direction may be positive, and a component of the electric field from the fourth portion toward the fourth leading end in the second direction may be positive. In the fourth state, a component of the electric field from the first leading end toward the first portion in the first direction may be positive, a component of the electric field from the second leading end toward the second portion in the first direction may be negative, a component of the electric field from the third portion toward the third leading end in the second direction may be negative, and a component of the electric field from the fourth leading end toward the fourth portion in the second direction may be negative. In this case, when the electromagnetic wave enters the meta-surface in the first state, the electron is emitted from the first antenna portion according to the positive component in the first direction of the electric field strength of the entered electromagnetic wave, and the emission of electron according to the other component of the electric field strength of the entered electromagnetic wave is suppressed. When the electromagnetic wave enters the meta-surface in the second state, the electron is emitted from the first antenna portion according to the negative component in the first direction of the electric field strength of the entered electromagnetic wave, and the emission of electron according to the other component of the electric field strength of the entered electromagnetic wave is suppressed. When the electromagnetic wave enters the meta-surface in the third state, the electron is emitted from the second antenna portion according to the positive component in the second direction of the electric field strength of the entered electromagnetic wave, and the emission of electron according to the other component of the electric field strength of the entered electromagnetic wave is suppressed. When the electromagnetic wave enters the meta-surface in the fourth state, the electron is emitted from the second antenna portion according to the negative component in the second direction of the electric field strength of the entered electromagnetic wave, and the emission of electron according to the other component of the electric field strength of the entered electromagnetic wave is suppressed.
In the aspect mentioned above, a potential control unit configured to control electric potentials applied to the meta-surface may be further included. The potential control unit may switch between a first state and a second state and switch between a third state and a fourth state by controlling the electric potentials applied to the meta-surface. In the first state, an electric potential applied to the first portion may be lower than an electric potential applied to the first antenna portion, an electric potential applied to the second portion may be higher than the electric potential applied to the first antenna portion, an electric potential applied to the third portion may be lower than the electric potential applied to the second antenna portion, and an electric potential applied to the fourth portion may be lower than the electric potential applied to the second antenna portion. In the second state, the electric potential applied to the first portion may be higher than the electric potential applied to the first antenna portion, the electric potential applied to the second portion may be lower than the electric potential applied to the first antenna portion, the electric potential applied to the third portion may be lower than the electric potential applied to the second antenna portion, and the electric potential applied to the fourth portion may be lower than the electric potential applied to the second antenna portion. In the third state, the electric potential applied to the first portion may be lower than the electric potential applied to the first antenna portion, the electric potential applied to the second portion may be lower than the electric potential applied to the first antenna portion, the electric potential applied to the third portion may be lower than the electric potential applied to the second antenna portion, and the electric potential applied to the fourth portion may be higher than the electric potential applied to the second antenna portion. In the fourth state, the electric potential applied to the first portion may be lower than the electric potential applied to the first antenna portion, the electric potential applied to the second portion may be lower than the electric potential applied to the first antenna portion, the electric potential applied to the third portion may be higher than the electric potential applied to the second antenna portion, and the electric potential applied to the fourth portion may be lower than the electric potential applied to the second antenna portion. In this case, an electric potential difference occurs between the first leading end and the first portion, between the second leading end and the second portion, between the third leading end and the third portion, and between the fourth leading end and the fourth portion. An electric field is generated by the electric potential difference. As a result, when the electromagnetic wave enters the meta-surface in the first state, the electron is emitted from the first antenna portion according to the positive component in the first direction of the electric field strength of the entered electromagnetic wave, and the emission of electron according to the other component of the electric field strength of the entered electromagnetic wave is suppressed. When the electromagnetic wave enters the meta-surface in the second state, the electron is emitted from the first antenna portion according to the negative component in the first direction of the electric field strength of the entered electromagnetic wave, and the emission of electron according to the other component of the electric field strength of the entered electromagnetic wave is suppressed. When the electromagnetic wave enters the meta-surface in the third state, the electron is emitted from the second antenna portion according to the positive component in the second direction of the electric field strength of the entered electromagnetic wave, and the emission of electron according to the other component of the electric field strength of the entered electromagnetic wave is suppressed. When the electromagnetic wave enters the meta-surface in the fourth state, the electron is emitted from the second antenna portion according to the negative component in the second direction of the electric field strength of the entered electromagnetic wave, and the emission of electron according to the other component of the electric field strength of the entered electromagnetic wave is suppressed.
In the aspect mentioned above, the first direction and the second direction may be orthogonal to each other. The meta-surface may further include a third antenna portion and a third bias portion. The third antenna portion may extend in a third direction intersecting the first direction and the second direction and may emit an electron in response to incidence of the electromagnetic wave. The third bias portion may face the third antenna portion and be configured to generate an electric field having a component in the third direction between the third bias portion and the third antenna portion. According to such a configuration, the third antenna portion emits an electron according to the component in the third direction of the electric field strength of the entered electromagnetic wave. In this case, an electron emitted according to the component in the third direction of the electric field strength of the entered electromagnetic wave can be further detected. Therefore, the polarization state of the entered electromagnetic wave including circular polarization can be detected by a simple computation processing by detecting the electron emitted from the meta-surface.
In the aspect mentioned above, a potential control unit configured to control electric potentials applied to the meta-surface may be further included. The potential control unit may switch between the first state and the second state, switch between the third state and the fourth state, and switch between a fifth state and a sixth state by controlling the electric potentials applied to the meta-surface. In the first state, a component of an electric field from the first bias portion toward the first antenna portion in the first direction may be positive. In the second state, a component of an electric field from the first bias portion toward the first antenna portion in the first direction may be negative. In the third state, a component of an electric field from the second bias portion toward the second antenna portion in the second direction may be positive. In the fourth state, a component of an electric field from the second bias portion toward the second antenna portion in the second direction may be negative. In the fifth state, a component of an electric field from the third bias portion toward the third antenna portion in the third direction may be negative. In the sixth state, a component of an electric field from the third bias portion toward the third antenna portion in the third direction may be positive. In this case, when the electromagnetic wave enters the meta-surface in the first state, the electron is emitted from the first antenna portion according to the positive component in the first direction of the electric field strength of the entered electromagnetic wave. When the electromagnetic wave enters the meta-surface in the second state, the electron is emitted from the first antenna portion according to the negative component in the first direction of the electric field strength of the entered electromagnetic wave. When the electromagnetic wave enters the meta-surface in the third state, the electron is emitted from the second antenna portion according to the positive component in the second direction of the electric field strength of the entered electromagnetic wave. When the electromagnetic wave enters the meta-surface in the fourth state, the electron is emitted from the second antenna portion according to the negative component in the second direction of the electric field strength of the entered electromagnetic wave. When the electromagnetic wave enters the meta-surface in the fifth state, the electron is emitted from the second antenna portion according to the negative component in the third direction of the electric field strength of the entered electromagnetic wave. When the electromagnetic wave enters the meta-surface in the sixth state, the electron is emitted from the second antenna portion according to the positive component in the third direction of the electric field strength of the entered electromagnetic wave. Therefore, the photoelectric conversion device is capable of achieving the measurement of the electric field strength of the electromagnetic wave entering the electron emitter for each polarity in each of the first direction, the second direction, and the third direction by detecting the electron emitted from the meta-surface in each of the states.
In the aspect mentioned above, the photoelectric conversion device may be further provided with a housing configured to airtightly sealed and have a window unit transmitting the electromagnetic wave. The electron emitter may be disposed in the housing. In this case, an amount of emission of the electron in response to incidence of the electromagnetic wave can be improved by making the housing vacuum or filling the housing with gas.
An electromagnetic wave detection device according to the other aspect of the present invention is provided with the photoelectric conversion device mentioned above, a detection unit and a computing unit. The detection unit is configured to detect an electron emitted from the electron emitter. The computing unit is configured to compute polarization information of the electromagnetic wave based on a result of detection of the detection unit in the first state, a result of detection of the detection unit in the second state, a result of detection of the detection unit in the third state, and a result of detection of the detection unit in the fourth state. In this case, the electromagnetic wave detection device is capable of easily detecting the polarization state of an electromagnetic wave.
A photoelectric conversion method according to yet another aspect of the present invention is provided with a step of using a meta-surface including a first antenna portion extending a first direction, a first bias portion facing the first antenna portion, a second antenna portion extending in a second direction intersecting the first direction, and a second bias portion facing the second antenna portion, and emitting an electron from a first antenna portion in a state where an electric field having a component in the first direction is generated between the first bias portion and the first antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface, and a step of using the meta-surface and emitting an electron from the second antenna portion in a state where an electric field having a component in the second direction is generated between the second bias portion and the second antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. The first antenna portion extends in the first direction. The first bias portion faces the first antenna portion. The second antenna portion extends in the second direction intersecting the first direction. The second bias portion faces the second antenna portion.
In the photoelectric conversion method, an electron is emitted from the first antenna portion when the electromagnetic wave to be measured enters the meta-surface in a state where an electric field having a component in the first direction is generated between the first bias portion and the first antenna portion. An electron is emitted from the second antenna portion when the electromagnetic wave to be measured enters the meta-surface in a state where an electric field having a component in the second direction is generated between the second bias portion and the second antenna portion. In this case, the first antenna portion emits an electron according to the component in the first direction of the electric field strength of the entered electromagnetic wave. The second antenna portion emits an electron according to the component in the second direction of the electric field strength of the entered electromagnetic wave. As a result, there can be detected an electron emitted according to the component in the first direction of the electric field strength of the entered electromagnetic wave and an electron emitted according to the component in the second direction of the electric field strength of the entered electromagnetic wave. According to the detection of them, detection of the polarization state of an electromagnetic wave can be easily achieved.
In yet another aspect mentioned above, the step of emitting an electron from the first antenna portion may be provided with a first electron emission step and a second electron emission step. In the first electron emission step, in the first state, an electron may be emitted from the first antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the first state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the first bias portion toward the first antenna portion in the first direction is positive. In the second electron emission step, in the second state, an electron may be emitted from the first antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the second state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the first bias portion toward the first antenna portion in the first direction is negative. The step of emitting an electron from the second antenna portion may be provided with a third electron emission step and a fourth electron emission step. In the third electron emission step, in the third state, an electron may be emitted from the second antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the third state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the second bias portion toward the second antenna portion in the second direction is positive. In the fourth electron emission step, in the fourth state, an electron may be emitted from the second antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the fourth state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the second bias portion toward the second antenna portion in the second direction is negative. In this case, in the first state, a component of an electric field from the first bias portion toward the first antenna portion in the first direction is positive. Therefore, when the electromagnetic wave enters the meta-surface in the first state, the electron is emitted from the first antenna portion according to the positive component in the first direction of the electric field strength of the entered electromagnetic wave. In the second state, a component of an electric field from the first bias portion toward the first antenna portion in the first direction is negative. Therefore, when the electromagnetic wave enters the meta-surface in the second state, the electron is emitted from the first antenna portion according to the negative component in the first direction of the electric field strength of the entered electromagnetic wave. In the third state, a component of an electric field from the second bias portion toward the second antenna portion in the second direction is positive. Therefore, when the electromagnetic wave enters the meta-surface in the third state, the electron is emitted from the second antenna portion according to the positive component in the second direction of the electric field strength of the entered electromagnetic wave. In the fourth state, a component of an electric field from the second bias portion toward the second antenna portion in the second direction is negative. Therefore, when the electromagnetic wave enters the meta-surface in the fourth state, the electron is emitted from the second antenna portion according to the negative component in the second direction of the electric field strength of the entered electromagnetic wave. Therefore, according to the photoelectric conversion method, measurement of the electric field strength of the electromagnetic wave entering the electron emitter can be achieved for each polarity in each of the first direction and the second direction by detecting the electron emitted from the meta-surface in each of the states.
In yet another aspect mentioned above, the first direction and the second direction may be orthogonal to each other. The meta-surface may further include a third antenna portion and a third bias portion. The third antenna portion may extend in the third direction intersecting the first direction and the second direction. The third bias portion may face the third antenna portion. The photoelectric conversion method may be further provided with a step of emitting an electron from the third antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In this case, the third antenna portion emits an electron according to the component in the third direction of the electric field strength of the entered electromagnetic wave. Therefore, there can be detected an electron emitted according to the component in the third direction of the electric field strength of the entered electromagnetic wave. Therefore, the polarization state of the entered electromagnetic wave including circular polarization can be detected by a simple computation processing by detecting the electron emitted from the meta-surface.
In yet another aspect mentioned above, the step of emitting an electron from the first antenna portion may be provided with a first electron emission step and a second electron emission step. In the first electron emission step, in the first state, an electron may be emitted from the first antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the first state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the first bias portion toward the first antenna portion in the first direction is positive. In the second electron emission step, in the second state, an electron may be emitted from the first antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the second state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the first bias portion toward the first antenna portion in the first direction is negative. The step of emitting an electron from the second antenna portion may be provided with a third electron emission step and a fourth electron emission step. In the third electron emission step, in the third state, an electron may be emitted from the second antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the third state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the second bias portion toward the second antenna portion in the second direction is positive. In the fourth electron emission step, in the fourth state, an electron may be emitted from the second antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the fourth state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the second bias portion toward the second antenna portion in the second direction is negative. The step of emitting an electron from the third antenna portion may be provided with a fifth electron emission step and a sixth electron emission step. In the fifth electron emission step, in the fifth state, an electron may be emitted from the third antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the fifth state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the third bias portion toward the third antenna portion in the third direction is positive. In the sixth electron emission step, in the sixth state, an electron may be emitted from the third antenna portion in response to incidence of an electromagnetic wave to be measured on the meta-surface. In the sixth state, the electric potentials may be applied to the meta-surface in such a manner that the component of the electric field from the third bias portion toward the third antenna portion in the third direction is negative. Therefore, when the electromagnetic wave enters the meta-surface in the fifth state, the electron is emitted from the second antenna portion according to the positive component in the third direction of the electric field strength of the entered electromagnetic wave. Therefore, when the electromagnetic wave enters the meta-surface in the sixth state, the electron is emitted from the second antenna portion according to the negative component in the third direction of the electric field strength of the entered electromagnetic wave. Therefore, measurement of the electric field strength of the electromagnetic wave entering the electron emitter can be achieved for each polarity in each of the first direction, the second direction, and the third direction by detecting the electron emitted from the meta-surface in each of the states.
An electromagnetic wave detection method according to yet another aspect of the present invention is provided with the photoelectric conversion method mentioned above, and is further provided with a first detection step, a second detection step, a third detection step, a fourth detection step, and a computing step. In the first detection step, an electron emitted from an electron emitter in a first electron emission step is detected. In the second detection step, an electron emitted from the electron emitter in a second electron emission step is detected. In the third detection step, an electron emitted from the electron emitter in a third electron emission step is detected. In the fourth detection step, an electron emitted from the electron emitter in a fourth electron emission step is detected. In the computing step, polarization information of an electromagnetic wave is computed based on results of detection in the first detection step, the second detection step, the third detection step, and the fourth detection step. In this case, the polarization state of an electromagnetic wave can easily be detected.
According to an aspect of the present invention, it is possible to provide a photoelectric conversion device capable of easily achieving detection of the polarization state of an electromagnetic wave. According to another aspect of the present invention, it is possible to provide an electromagnetic wave detection device capable of easily detecting the polarization state of an electromagnetic wave. According to yet another aspect of the present invention, it is possible to provide a photoelectric conversion method capable of easily achieving detection of the polarization state of an electromagnetic wave. According to yet another aspect of the present invention, it is possible to provide an electromagnetic wave detection method capable of easily detecting the polarization state of an electromagnetic wave.
Hereinafter, an embodiment of the present invention will be described in detail with reference to the accompanying drawings. In the following description, the same elements or corresponding elements will be denoted with the same reference numerals and a redundant explanation will be omitted.
First, a configuration of an electromagnetic wave detection device according to the present embodiment will be described with reference to
An electromagnetic wave detection device 1 detects an entered electromagnetic wave. The electromagnetic wave detection device 1 includes a photoelectric conversion device 2. The photoelectric conversion device 2 emits an electron in response to incidence of the electromagnetic wave. In the present specification, the term “light” includes the other electromagnetic waves than a visible light. In the present embodiment, the electromagnetic wave detection device 1 detects the entered electromagnetic wave based on the electron emitted from the photoelectric conversion device 2 in response to incidence of the electromagnetic wave. The photoelectric conversion device 2 emits the electron, for example, in response to the incidence of the electromagnetic wave having a range of wavelength between a so-called millimeter wave and an infrared light. The range of wavelength between the millimeter wave and the infrared light corresponds, for example, to a frequency range between about 0.01 and 150 THz. In the present specification, the term “range of wavelength” may include a range of a plurality of wavelength regions separated from each other, or may be a range of one continuous wavelength region. The photoelectric conversion device 2 emits an electron by a field electron emission (field emission), for example.
The electromagnetic wave detection device 1 is, for example, an electron tube which outputs an electric signal in response to incidence of an electromagnetic wave. For example, the electromagnetic wave detection device 1 emits an electron in response to incidence of the electromagnetic wave, detects the emitted electron and outputs an electric signal based of the result of detection, in an inner portion of the electron tube. The electron tube is, for example, a photomultiplier tube (PMT). The electromagnetic wave detection device 1 emits the electron in the inner portion when the electromagnetic wave enters, and multiplies the emitted electron. According to a modification of the present embodiment, the electromagnetic wave detection device 1 may not be provided with a configuration for detecting the electron in the electron tube. In other words, the electromagnetic wave detection device 1 may be provided with an electron tube emitting the electron to an outer portion in response to incidence of the electromagnetic wave as the photoelectric conversion device 2, and may be provided with a detection unit detecting the electron emitted from the electron tube in an outer portion of the electron tube.
The electromagnetic wave detection device 1 is provided with a housing 10, an electron emitter 20, a holder 30, an electron multiplying unit 40, an electron collecting unit 50, a power supply unit 70, and a computing unit 75. The electron emitter 20, the holder 30, the electron multiplying unit 40 and the electron collecting unit 50 are disposed in the housing 10. The photoelectric conversion device 2 is provided with the housing 10, the electron emitter 20 and the power supply unit 70, and configures a part of the electromagnetic wave detection device 1.
The housing 10 has a valve 11 and a stem 12. The inner portion of the housing 10 is airtightly sealed by the valve 11 and the stem 12. In the present embodiment, the inner portion of the housing 10 is held in a vacuum. The vacuum in the housing 10 may not be an absolute vacuum, but may be a state where the housing is filled with gas having a lower pressure than an atmospheric pressure. For example, the inner portion of the housing 10 is held at 1×10−4 to 1×10−7 Pa.
The valve 11 includes a window unit 11a having an electromagnetic wave transparency. In the present specification, the term “electromagnetic wave transparency” means a property of transmitting at least a partial frequency range of wavelength of the range of wavelength of the entered electromagnetic wave. In the present embodiment, the housing 10 has a circular cylindrical shape. The housing 10 extends in a X-axis direction as illustrated in
The window unit 11a configures a bottom surface facing the stem 12. For example, the window unit 11a is formed into a circular shape as viewed from the X-axis direction while setting a direction of YZ axis to a diametrical direction. A frequency characteristic of transmittance of the electromagnetic wave is different depending on a material. Therefore, the window unit 11a is configured by an appropriate material depending on a frequency range of the electromagnetic wave entering the housing 10. For example, the window unit 11a includes at least one selected from quartz, silicon, germanium, sapphire, zinc selenide, zinc sulfide, magnesium fluoride, lithium fluoride, barium fluoride, calcium fluoride, magnesium oxide, calcium carbonate, diamond and chalcogenide glass. Therefore, an electromagnetic wave having an arbitrary frequency range between millimeter wave and infrared light can be guided into the inner portion of the housing 10. For example, the quartz is suitable for a material of a member transmitting an electromagnetic wave having a frequency range of 0.1 to 5 THz, the silicon is suitable for a material of a member transmitting an electromagnetic wave having a frequency range of 0.04 to 11 THz and 46 THz or more, the magnesium fluoride is suitable for a material of a member transmitting an electromagnetic wave having a frequency range of 40 THz or more, the germanium is suitable for a material of a member transmitting an electromagnetic wave having a frequency range of 13 THz or more, and the zinc selenide is suitable for a material of a member transmitting an electromagnetic wave having a frequency range of 14 THz or more.
The housing 10 further has a plurality of wires 13 for enabling electrical connection between an outer portion and an inner portion of the housing 10. The plurality of wires 13 are, for example, lead wires or pins. In the present embodiment, the plurality of wires 13 are pins penetrating the stem 12 and extend from the inner portion of the housing 10 to the outer portion thereof. At least one of the plurality of wires 13 is connected to various members provided in the inner portion of the housing 10.
The electron emitter 20 emits the electron in response to incidence of the electromagnetic wave. The electron emitter 20 is provided with a supporting body 21. The supporting body 21 has, for example, a plate shape. The supporting body 21 is formed, for example, into a rectangular shape in plan view. The supporting body 21 has a principal surface 21a and a principal surface 21b facing each other. The principal surface 21a and the principal surface 21b are surfaces of the supporting body 21 which are positioned in opposite sides to each other. The principal surface 21a and the principal surface 21b are, for example, flat surfaces, and are formed into a rectangular shape in plan view. The principal surface 21a and the principal surface 21b are disposed in parallel to the window unit 11a. The principal surface 21a faces the window unit 11a. The electromagnetic wave passing through the window unit 11a enters the principal surface 21a.
The supporting body 21 has an electromagnetic wave transparency with respect to the electromagnetic wave passing through the window unit 11a. As a result, the supporting body 21 transmits at least partial frequency range of the electromagnetic wave passing through the window unit 11a. The supporting body 21 can be made of the same material as that of the window unit 11a. The material of the supporting body 21 includes, for example, silicon. In one photoelectric conversion device 2, the supporting body 21 and the window unit 11a may not be made of the same material. The supporting body 21 is spaced away from the window unit 11a and the electron multiplying unit 40.
The electron emitter 20 includes a meta-surface 22. The meta-surface 22 is provided in the supporting body 21. The meta-surface 22 emits the electron in response to incidence of the electromagnetic wave. For example, the meta-surface 22 has a sensitivity for the electromagnetic wave in a range of wavelength between the so-called millimeter wave and the infrared light. The meta-surface 22 also has a sensitivity for terahertz-wave. The range of wavelength of the terahertz-wave corresponds to a frequency range between 100 GHz and 30 THz. The term “having a sensitivity for an electromagnetic wave” means that an electron is emitted in response to incidence of the electromagnetic wave.
For example, the meta-surface 22 includes an oxide layer formed on the principal surface 21b of the supporting body 21, and a metal layer formed on the oxide layer. The material of the oxide layer includes, for example, silicon dioxide and titanium oxide. For example, the oxide layer includes a layer including the silicon dioxide, and a layer including the titanium oxide. The material of the metal layer includes, for example, gold. In the present embodiment, the oxide layer is formed on the principal surface 21b of the supporting body 21 made of quartz, and the metal layer is formed on the oxide layer. For example, a thickness of the supporting body 21 is 525 μm, a thickness of the layer including the silicon diode in the meta-surface 22 is 1 μm, a thickness of the layer including the titanium dioxide in the meta-surface 22 is 10 nm, and a thickness of the metal layer in the meta-surface 22 is 200 nm. The meta-surface 22 has a rectangular shape in plan view. In the modification of the present embodiment, the meta-surface 22 may be provided on the principal surface 21a.
The holder 30 holds the electron emitter 20 in the inner portion of the housing 10. The holder 30 is positioned to the inner surface 10a of the housing 10. The holder 30 positions the electron emitter 20 for the housing 10. The holder 30 has a frame shape along the inner surface 10a of the housing 10, and a penetration opening is formed in the holder 30. The meta-surface 22 of the electron emitter 20 is disposed in an inner side of an edge defining the penetration opening as seen from an orthogonal direction to the principal surfaces 21a and 21b of the electron emitter 20.
The electron multiplying unit 40 is disposed in the inner portion of the housing 10, and has an incidence surface 40a on which the electron emitted from the electron emitter 20 enters. The electron multiplying unit 40 multiplies the electron entering the incidence surface 40a. In the present embodiment, the principal surface 21b of the electron emitter 20 faces the incidence surface 40a of the electron multiplying unit 40. The meta-surface 22 faces the incidence surface 40a of the electron multiplying unit 40, and the electron emitted from the meta-surface 22 enters the incidence surface 40a. The principal surface 21a of the electron emitter 20 faces the window unit 11a of the housing 10. The electron multiplying unit 40 has, for example, multistage dynodes.
The electron collecting unit 50 is disposed in the inner portion of the housing 10, and collects the electron which is multiplied by the electron multiplying unit 40. The electron collecting unit 50 is a detection unit detecting the electron emitted from the electron emitter 20. The electromagnetic wave detection device 1 detects the electromagnetic wave by detecting the electron in the electron collecting unit 50. In the present embodiment, for example, the electron collecting unit 50 has an anode to which one of a plurality of wires 13 is connected. A predetermined electric potential is applied to the anode through the wire 13. The anode catches the electron which is multiplied by the dynodes of the electron multiplying unit 40. The electron collecting unit 50 may have a diode in place of the anode.
In the present embodiment, the meta-surface 22 is of an active type and is operated by application of bias voltage. The meta-surface 22 is operated by application of electric potentials by means of the power supply unit 70. The power supply unit 70 is electrically connected to the meta-surface 22. The power supply unit 70 includes a potential application unit 71 and a potential control unit 72. The potential application unit 71 applies the electric potential to the meta-surface 22. The potential control unit 72 controls the potential application unit 71. The electric potentials applied to the meta-surface 22 are controlled by the potential control unit 72. The meta-surface 22 is operated in response to the electric potential controlled by the potential control unit 72. In other words, the meta-surface 22 emits the electron in response to the control of electric potential by the potential control unit 72.
The computing unit 75 acquires a result of detection in the electron collecting unit 50, and computes information relating to an electric field strength of an electromagnetic wave based on the result of detection. For example, the computing unit 75 acquires an electric signal based on the electron collected in the electron collecting unit 50 as the result of detection. The information relating to the electric field strength of the electromagnetic wave to be computed may be the electric field strength itself. The computing unit 75 computes the polarization information of the electromagnetic wave based on the information relating to the electric field strength of the electromagnetic wave. The “polarization information” is information relating the “polarization state”. For example, the computing unit 75 computes the polarization direction of linear polarization. For example, the computing unit 75 outputs and displays the information relating to the computed electric field strength and the polarization information on a display unit which is not illustrated.
The potential control unit 72 and the computing unit 75 are one computer or a plurality of computers, for example, constructed by a hardware and a software such as programs. The potential control unit 72 and the computing unit 75 are provided, for example, with a processor, a main storage unit, an auxiliary storage unit, a communication device and an input device, as the hardware. The processor executes an operating system and an application program. The main storage is constructed by Read Only Memory (ROM) and Random Access Memory (RAM). The auxiliary storage unit is a storage medium which is constructed by a hard disc and a flash memory. The auxiliary storage unit generally stores a larger amount of data than the main storage unit. The communication device is constructed by a network card or a wireless communication module. The input device is constructed by a keyboard, a mouse and a touch panel. The potential control unit 72 and the computing unit 75 may be integrally configured or may be separated.
Next, the photoelectric conversion device 2 will be described further in detail with reference to
In the example illustrated in
As illustrated in
As illustrated in
The antenna portions α1 and α2 emit the electron P in response to incidence of the electromagnetic wave W. The antenna portion α1 extends in the Z-axis direction. The bias portion β1 faces the antenna portion α1. The bias portion β1 is configured to generate an electric field having a component in the Z-axis direction between the bias portion β1 and the corresponding antenna portion α1 when the bias electric potential is applied. In the present embodiment, the bias portion β1 generates an electric field in the Z-axis direction between the bias portion β1 and the antenna portion α1. When a higher electric potential than the antenna portion α1 is applied to the bias portion β1, an electric potential barrier in the leading end portion of the bias portion β1 side in the antenna portion α1 becomes thin. When a lower electric potential than the antenna portion α1 is applied to the bias portion β1, the electric potential barrier in the leading end portion of the bias portion β1 side in the antenna portion α1 becomes thick.
The antenna portion α2 extends in the Y-axis direction. The bias portion β2 faces the antenna portion α2. The bias portion β2 is configured to generate an electric field having a component in the Y-axis direction between the bias portion β2 and the corresponding antenna portion α2 when the bias electric potential is applied. In the present embodiment, the bias portion β2 generates an electric field in the Y-axis direction between the bias portion β2 and the antenna portion α2. When a higher electric potential than the antenna portion α2 is applied to the bias portion β2, an electric potential barrier in the leading end portion of the bias portion β2 side in the antenna portion α2 becomes thin. When a lower electric potential than the antenna portion α2 is applied to the bias portion β2, the electric potential barrier in the leading end portion of the bias portion β2 side in the antenna portion α2 becomes thick. A state where a higher electric potential than the antenna portion is applied to the bias portion is called as “forward bias”. A state where a lower electric potential than the antenna portion is applied to the bias portion is called as “reverse bias”.
When the electromagnetic wave W enters the antenna portions α1 and α2, the electric field is induced around the antenna portions α1 and α2. The electric potential barrier at the antenna-vacuum interface becomes thin by the electric field induced around the antenna portions α1 and α2. In a case where the electric potential barrier becomes further thin by the incidence of the electromagnetic wave W on the antenna portions α1 and α2 in the forward bias state, the electron existing in the antenna portions α1 and α2 can slip out of the electric potential barrier due to a tunnel effect. The electron P slipping out of the electric potential barrier is accelerated by the electric field around the antenna portions α1 and α2. As mentioned above, the field electron emission can be generated by the incidence of the electromagnetic wave W on the antenna portions α1 and α2 in the forward bias state.
Each of the patterns 31, 32, 33, 34, and 35 is disposed on the principal surface 21b of the supporting body 21. The plurality of patterns 31, 32, 33, 34, and 35 are connected via an oxide layer. The plurality of patterns 31, 32, 33, 34, and 35 are separated from each other by the oxide layer, and are insulated from each other at least when the photoelectric conversion device 2 is not operated. Each of the patterns 31, 32, 33, 34, and 35 is a conductive line, and conducts the electron. Each of the patterns 31, 32, 33, 34, and 35 includes a metal layer which is formed at least on the oxide layer of the meta-surface 22. A material of the metal layer includes, for example, gold.
In the example illustrated in
The pattern 32 includes a plurality of linear parts 43 and a linear part 44 electrically connecting the plurality of linear parts 43 to each other. Each of the linear parts 43 extends in a Y-axis direction. Each of the linear parts 43 configures the bias portion β1. Each of the linear parts 43 is formed into a rectangular shape extending in the Y-axis direction, for example. The linear part 41 and the linear part 43 corresponding to each other are disposed on the same line extending in the Z-axis direction. The pattern 35 is disposed between the linear part 41 and the linear part 43 corresponding to each other. The linear part 44 is connected to each of the linear parts 43. In the present embodiment, the plurality of linear parts 43 are arrayed on the same line in the Y-axis direction, and the linear parts 43 adjacent to each other are connected by a plurality of linear parts 44. A plurality of groups each including the plurality of linear parts 43 disposed on the same line extending in the Y-axis direction, are arrayed in parallel to each other in the Z-axis direction. The pattern 35 is disposed between the one group including the plurality of linear parts 41 and the one group including the plurality of linear parts 43. When the linear part 41 corresponds to the first portion, the linear part 43 corresponds to the second portion.
The pattern 33 includes a plurality of linear parts 46 and a linear part 47 electrically connecting the plurality of linear parts 46 to each other. Each of the linear parts 46 extends in a Z-axis direction. Each of the linear parts 46 configures the bias portion 2. Each of the linear parts 46 is formed into a rectangular shape extending in the Z-axis direction, for example. The linear part 47 is connected to each of the linear parts 46. In the present embodiment, the plurality of linear parts 46 are arrayed on the same line in the Z-axis direction, and the linear parts 46 adjacent to each other are connected by a plurality of linear parts 47. A plurality of groups each including the plurality of linear parts 46 disposed on the same line extending in the Z-axis direction, are arrayed in parallel to each other in the Y-axis direction.
The pattern 34 includes a plurality of linear parts 48 and a linear part 49 electrically connecting the plurality of linear parts 48 to each other. Each of the linear parts 48 extends in a Z-axis direction. Each of the linear parts 48 configures the bias portion β2. Each of the linear parts 48 is formed into a rectangular shape extending in the Z-axis direction, for example. The linear part 46 and the linear part 48 corresponding to each other are disposed on the same line extending in the Y-axis direction. The pattern 35 is disposed between the linear part 46 and the linear part 48 corresponding to each other. The linear part 49 is connected to each of the linear parts 48. In the present embodiment, the plurality of linear parts 48 are arrayed on the same line in the Z-axis direction, and the linear parts 48 adjacent to each other are connected by a plurality of linear parts 49. A plurality of groups each including the plurality of linear parts 48 disposed on the same line extending in the Z-axis direction, are arrayed in parallel to each other in the Y-axis direction. The pattern 35 is disposed between the one group including the plurality of linear parts 46 and the one group including the plurality of linear parts 48. When the linear part 46 corresponds to the third portion, the linear part 48 corresponds to the fourth portion.
The pattern 35 extends toward the patterns 31 and 32 and the patterns 33 and 34. In a state where a lower electric potential than that applied to the pattern 31, the pattern 32, the pattern 33, or the pattern 34 is applied to the pattern 35, the pattern 35 emits the electron P in response to incidence of the electromagnetic wave W. The pattern 35 includes a plurality of linear parts 51 and a plurality of linear parts 52. The linear part 51 and the linear part 52 respectively extend in directions intersecting each other. In other words, a direction where the linear part 51 extends and a direction where the linear part 52 extends intersect each other. In the present embodiment, the linear part 51 and the linear part 52 respectively extend in directions orthogonal to each other.
Each of the linear parts 51 extends in a Z-axis direction. Each of the linear parts 51 configures the antenna portion α1. Each of the linear parts 51 is formed into a rectangular shape extending in the Z-axis direction, for example. The plurality of linear parts 51 are in parallel to each other. The pattern 35 includes a linear part 53 electrically connecting the plurality of linear parts 51 to each other. The linear part 53 is connected to each of the linear parts 51. In the present embodiment, the plurality of linear parts 51 are arrayed on the same line in the Y-axis direction, and the linear parts 51 adjacent to each other are connected by a plurality of linear parts 53. A plurality of groups each including the plurality of linear parts 51 disposed on the same line extending in the Z-axis direction, are arrayed in the Y-axis direction. The plurality of linear parts 51 included in mutually different groups are disposed on the same line extending in the Z-axis direction.
Each of the linear parts 51 extends in a +Z-axis direction and a-Z-axis direction from a portion connected to the linear part 53. Each of the linear parts 53 is connected to the center of each of the linear parts 51. Each of the linear parts 51 includes a pair of linear parts 51a and 51b. The linear part 51a extends in a +Z-axis direction from a portion connected to the linear part 53. The linear part 51b extends in a-Z-axis direction from a portion connected to the linear part 53. In the present embodiment, the pair of linear parts 51a and 51b in each of the linear parts 51 extend on the same line extending in the Z-axis direction. Each of the linear parts 51 is disposed between a pair of bias portions β1 in the Z-axis direction. Each of the linear parts 51 is disposed between the pattern 31 and the pattern 32 in the Z-axis direction. Each of the linear parts 51 is disposed between the linear part 41 and the linear part 43 in the Z-axis direction.
Each of the linear parts 52 extends in a Y-axis direction. Each of the linear parts 52 configures the antenna portion α2. Each of the linear parts 52 is formed into a rectangular shape extending in the Y-axis direction, for example. The plurality of linear parts 52 are in parallel to each other. The above-mentioned linear part 53 electrically connects the plurality of linear parts 52 to each other. The linear part 53 is connected to each of the linear parts 52. In the present embodiment, the plurality of linear parts 52 are arrayed on the same line in the Z-axis direction, and the linear parts 52 adjacent to each other are connected by a plurality of linear parts 53. A plurality of groups each including the plurality of linear parts 52 disposed on the same line extending in the Z-axis direction, are arrayed in the Y-axis direction. The plurality of linear parts 52 included in mutually different groups are disposed on the same line extending in the Y-axis direction. In the present embodiment, the plurality of linear parts 51 and the plurality of linear parts 52 are electrically connected by the linear part 53.
Each of the linear parts 52 extends in a +Y-axis direction and a-Y-axis direction from a portion connected to the linear part 53. Each of the linear parts 53 is connected to the center of each of the linear parts 52. Each of the linear parts 52 includes a pair of linear parts 52a and 52b. The linear part 52a extends in a +Y-axis direction from a portion connected to the linear part 53. The linear part 52b extends in a-Y-axis direction from a portion connected to the linear part 53. In the present embodiment, the pair of linear parts 52a and 52b in each of the linear parts 52 extend on the same line extending in the Y-axis direction. Each of the linear parts 52 is disposed between a pair of bias portions β2 in the Y-axis direction. Each of the linear parts 52 is disposed between the pattern 33 and the pattern 34 in the Y-axis direction. Each of the linear parts 52 is disposed between the linear part 46 and the linear part 48 in the Y-axis direction.
The pattern 35 includes a leading end 36 facing the pattern 31, a leading end 37 facing the pattern 32, a leading end 38 facing the pattern 33, and a leading end 39 facing the pattern 34. For example, the leading end 36 corresponds to the first leading end, the leading end 37 corresponds to the second leading end, the leading end 38 corresponds to the third leading end, and the leading end 39 corresponds to the fourth leading end. In the present embodiment, each of the linear parts 51 configuring the antenna portion α1 includes the leading end 36 and the leading end 37, and each of the linear parts 52 configuring the antenna portion α2 includes the leading end 38 and the leading end 39.
The leading ends 36 and the leading end 37 are positioned in both ends of each of the linear parts 51. The leading end 36 is included in the linear part 51a. The leading end 37 is included in the linear part 51b. The leading end 36 and the leading end 37 included in the same linear part 51 are disposed on the same line extending in the Z-axis direction. The leading ends 38 and the leading end 39 are positioned in both ends of each of the linear parts 52. The leading end 38 is included in the linear part 52a. The leading end 39 is included in the linear part 52b. The leading end 38 and the leading end 39 included in the same linear part 52 are disposed on the same line extending in the Y-axis direction.
The leading end 36 faces the bias portion β1. The leading end 36 faces the corresponding linear part 41 of the bias portion β1. The linear part 41 generates an electric field having a Z-axis directional component between the linear part 41 and the leading end 36. The leading end 36 is the closest portion to the pattern 31 in the linear part 51 including the leading end 36. The leading end 36 is disposed closer to the corresponding linear part 41 than the other portions of the pattern 35.
The leading end 37 faces the bias portion β1. The leading end 37 faces the corresponding linear part 43 of the bias portion β1. The linear part 43 generates an electric field having a Z-axis directional component between the linear part 43 and the leading end 37. The leading end 37 is the closest portion to the pattern 32 in the linear part 51 including the leading end 37. The leading end 37 is disposed closer to the corresponding linear part 43 than the other portions of the pattern 35.
The leading end 36 and the leading end 37, and the linear part 41 and the linear part 43 are disposed in the order of the linear part 43, the leading end 37, the leading end 36, and the linear part 41 in the Z-axis direction. In the photoelectric conversion unit 25, each of the linear parts 51 can emit the electron P in response to incidence of the electromagnetic wave W in a state where a lower electric potential than the linear part 41 or the linear part 43 is applied thereto.
The leading end 38 faces the bias portion β2. The leading end 38 faces the corresponding linear part 46 of the bias portion β2. The linear part 46 generates an electric field having a Y-axis directional component between the linear part 46 and the leading end 38. The leading end 38 is the closest portion to the pattern 33 in the linear part 52 including the leading end 38. The leading end 38 is disposed closer to the corresponding linear part 46 than the other portions of the pattern 35.
The leading end 39 faces the bias portion β2. The leading end 39 faces the corresponding linear part 48 of the bias portion β2. The linear part 48 generates an electric field having a Y-axis directional component between the linear part 48 and the leading end 39. The leading end 39 is the closest portion to the pattern 34 in the linear part 52 including the leading end 39. The leading end 39 is disposed closer to the corresponding linear part 48 than the other portions of the pattern 35.
The leading end 38 and the leading end 39, and the linear part 46 and the linear part 48 are disposed in the order of the linear part 48, the leading end 39, the leading end 38, and the linear part 46 in the Y-axis direction. In the photoelectric conversion unit 25, each of the linear parts 52 can emit the electron P in response to incidence of the electromagnetic wave W in a state where a lower electric potential than the linear part 46 or the linear part 48 is applied thereto.
The photoelectric conversion unit 25 is configured to correspond to a range of wavelength, for example, from a millimeter wave to an infrared light by a change of a configuration of the linear parts 51 and 52. For example, a length of the linear part 51 in the Z-axis direction corresponds to a wavelength region of the electromagnetic wave W which allows the electron P to be emitted in the photoelectric conversion unit 25. For example, the length of the linear part 51 in the Z-axis direction is designed according to a desired wavelength region emitting the electron P from the photoelectric conversion unit 25. In the same manner, a length of the linear part 52 in the Y-axis direction corresponds to a wavelength region of the electromagnetic wave W which allows the electron P to be emitted in the photoelectric conversion unit 25. For example, the length of the linear part 52 in the Y-axis direction is designed according to a desired wavelength region emitting the electron P from the photoelectric conversion unit 25. For example, each of the linear parts 51 and 52 has a length which is half the length of a center wavelength in the desired wavelength region. The length of each of the linear parts 51 is a length from the leading end 36 to the leading end 37 in the Z-axis direction. The length of each of the linear parts 52 is a length from the leading end 38 to the leading end 39 in the Y-axis direction.
In a case where the electromagnetic wave W having transmitted the supporting body 21 enters the linear parts 51 and 52 as in the present embodiment, a refractive index of the supporting body 21 through which the electromagnetic wave has passed is also taken into consideration. For example, in a case where a wavelength of the electromagnetic wave entering the electron tube is 600 μm, and a refractive index of the supporting body 21 is 3.4 for the electromagnetic wave W, a wavelength of the electromagnetic wave entering the linear parts 51 and 52 is 600 μm/3.4=176 μm. Therefore, in this case, for example, as the length of the linear part 51 in the Z-axis direction and the length of the linear part 52 in the Y-axis direction, 176 μm/2=88 μm may be appropriate.
The electron emitter 20 is further provided with a plurality of electrodes 61, 62, 63, 64, and 65 which are spaced away from each other, as illustrated in
For example, the electrode 61 is included in the pattern 31. The electrode 61 is electrically connected to the plurality of linear parts 41 via the linear part 42. The electrode 61 may be integrally formed with the linear part 42 and the plurality of linear parts 41. The electrode 62 is included in the pattern 32. The electrode 62 is electrically connected to the plurality of linear parts 43 via the linear part 44. The electrode 62 may be integrally formed with the linear part 44 and the plurality of linear parts 43. The electrode 63 is included in the pattern 33. The electrode 63 is electrically connected to the plurality of linear parts 46 via the linear part 47. The electrode 63 may be integrally formed with the linear part 47 and the plurality of linear parts 46. The electrode 64 is included in the pattern 34. The electrode 64 is electrically connected to the plurality of linear parts 48 via the linear part 49. The electrode 64 may be integrally formed with the linear part 49 and the plurality of linear parts 48. The electrode 65 is included in the pattern 35. The electrode 65 is electrically connected to the plurality of linear parts 51 and 52 via the linear part 53. The electrode 65 may be integrally formed with the linear part 53 and the plurality of linear parts 51 and 52.
The photoelectric conversion unit 25 is operated by application of electric potentials from the power supply unit 70 via the plurality of electrodes 61, 62, 63, 64, and 65. The potential application unit 71 of the power supply unit 70 applies the electric potentials to the photoelectric conversion unit 25 via the plurality of electrodes 61, 62, 63, 64, and 65. The potential control unit 72 of the power supply unit 70 controls the electric potentials applied to the photoelectric conversion unit 25 of the meta-surface 22.
Next, an operation of the photoelectric conversion device 2 according to the present embodiment will be described in detail with reference to
The potential control unit 72 switches between the first state and the second state and switches between the third state and the fourth state by controlling the electric potentials applied to the plurality of patterns 31, 32, 33, 34, and 35. The first state corresponds to the state illustrated by
In the first state, an electric potential applied to the pattern 35 is higher than an electric potential applied to the pattern 31, and is lower than an electric potential applied to the pattern 32. In other words, an electric potential applied to the linear part 41 configuring the bias portion β1 is lower than an electric potential applied to the linear part 51a configuring the antenna portion α1. An electric potential applied to the linear part 43 configuring the bias portion β1 is higher than an electric potential applied to the linear part 51b configuring the antenna portion α1.
In this case, as illustrated in
As a result, in the first state, an electric potential barrier of the leading end portion of the antenna portion α1 configured by the linear part 51a becomes thick. In other words, an electric potential barrier in an antenna-vacuum interface becomes thicker due to the electric potential difference between the pattern 35 and the pattern 31. Therefore, the emission of electron from the linear part 51a in response to incidence of the electromagnetic wave W on the linear part 51a is suppressed. In the first state, the component of the electric field from the leading end 36 of the linear part 51a toward the linear part 41 configuring the bias portion β1 in the Z-axis direction is positive.
In the first state, an electric potential barrier of the leading end portion of the antenna portion α1 configured by the linear part 51b becomes thin. In other words, an electric potential barrier in an antenna-vacuum interface becomes thinner due to the electric potential difference between the pattern 35 and the pattern 32. Therefore, the emission of electron P from the linear part 51b in response to incidence of the electromagnetic wave W on the linear part 51b is promoted. In the first state, the component of the electric field from the linear part 43 configuring the bias portion β1 toward the leading end 37 of the linear part 51b configuring the antenna portion α1 in the Z-axis direction is positive. Therefore, in a case where the component of the electric field strength of the electromagnetic wave W entering the photoelectric conversion unit 25 in the first state in the Z-axis direction is positive, the electric potential barrier in the antenna-vacuum interface becomes further thinner in response to incidence of the electromagnetic wave W. Therefore, in a case where the component of the electric field strength of the electromagnetic wave W entering the photoelectric conversion unit 25 in the first state in the Z-axis direction is positive, the electron P is emitted from the linear part 51b.
In the first state, the electric potential applied to pattern 35 is higher than electric potentials applied to pattern 33 and pattern 34. In other words, the electric potential applied to the linear part 46 configuring the bias portion β2 is lower than an electric potential applied to the linear part 51b configuring the antenna portion α2. A electric potential applied to the linear part 48 configuring the bias portion 2 is lower than an electric potential applied to the linear part 51b configuring the antenna portion α2.
In this case, as illustrated in
As a result, in the first state, an electric potential barrier in each of the leading end portions of the antenna portion α2 configured by the linear parts 52a and 52b becomes thick. In other words, an electric potential barrier in an antenna-vacuum interface becomes thicker due to the electric potential differences between the pattern 35 and the patterns 33 and 34. Therefore, the emission of electron from the linear parts 52a and 52b in response to incidence of the electromagnetic wave W on the linear parts 52a and 52b is suppressed. In the first state, the component of the electric field from the leading end 38 of the linear part 52a toward the linear part 46 configuring the bias portion β2 in the Y-axis direction is positive, and the component of the electric field from the leading end 39 of the linear part 52b toward the linear part 48 configuring the bias portion β2 in the Y-axis direction is negative.
In the second state, the electric potential applied to the pattern 35 is lower than the electric potential applied to the pattern 31, and is higher than the electric potential applied to the pattern 32. In other words, the electric potential applied to the linear part 41 configuring the bias portion β1 is higher than the electric potential applied to the linear part 51a configuring the antenna portion α1. The electric potential applied to the linear part 43 configuring the bias portion β1 is lower than the electric potential applied to the linear part 51b configuring the antenna portion α1.
In this case, as illustrated in
As a result, in the second state, an electric potential barrier of the leading end portion of the antenna portion α1 configured by the linear part 51a becomes thin. In other words, an electric potential barrier in an antenna-vacuum interface becomes thinner due to the electric potential difference between the pattern 35 and the pattern 31. Therefore, the emission of electron P from the linear part 51a in response to incidence of the electromagnetic wave W on the linear part 51a is promoted. In the second state, the component of the electric field from the linear part 41 configuring the bias portion β1 toward the leading end 36 of the linear part 51a configuring the antenna portion α1 in the Z-axis direction is negative. Therefore, in a case where the component of the electric field strength of the electromagnetic wave W entering the photoelectric conversion unit 25 in the second state in the Z-axis direction is negative, the electric potential barrier in the antenna-vacuum interface becomes further thinner in response to incidence of the electromagnetic wave W. As a result, in a case where the component of the electric field strength of the electromagnetic wave W entering the photoelectric conversion unit 25 in the second state in the Z-axis direction is negative, the electron P is emitted from the linear part 51a.
In the second state, an electric potential barrier of the leading end portion of the antenna portion α1 configured by the linear part 51b becomes thick. In other words, an electric potential barrier in an antenna-vacuum interface becomes thicker due to the electric potential difference between the pattern 35 and the pattern 32. Therefore, the emission of electron from the linear part 51b in response to incidence of the electromagnetic wave W on the linear part 51b is suppressed. In the second state, the component of the electric field from the leading end 37 of the linear part 51b toward the linear part 43 configuring the bias portion β1 in the Z-axis direction is negative.
In the second state, the electric potential applied to the pattern 35 is higher than the electric potential applied to the pattern 33 and the pattern 34, in the same manner as the first state. In other words, the electric potential applied to the linear part 46 configuring the bias portion β2 is lower than the electric potential applied to the linear part 51b configuring the antenna portion α2. The electric potential applied to the linear part 48 configuring the bias portion β2 is lower than the electric potential applied to the linear part 51b configuring the antenna portion α2.
Also in the second state, as illustrated in
Therefore, the emission of electron from the linear parts 52a and 52b in response to incidence of the electromagnetic wave W on the linear parts 52a and 52b is suppressed. In the second state, the component of the electric field from the leading end 38 of the linear part 52a toward the linear part 46 configuring the bias portion β2 in the Y-axis direction is positive, and the component of the electric field from the leading end 39 of the linear part 52b toward the linear part 48 configuring the bias portion β2 in the Y-axis direction is negative.
In the third state, the electric potential applied to pattern 35 is higher than the electric potentials applied to pattern 31 and pattern 32. In other words, the electric potential applied to the linear part 41 configuring the bias portion β1 is lower than the electric potential applied to the linear part 51a configuring the antenna portion α1. The electric potential applied to the linear part 43 configuring the bias portion β1 is lower than the electric potential applied to the linear part 51a configuring the antenna portion α1.
In this case, as illustrated in
As a result, in the third state, an electric potential barrier in each of the leading end portions of the antenna portion α1 configured by the linear parts 51a and 51b becomes thick. In other words, an electric potential barrier in an antenna-vacuum interface becomes thicker due to the electric potential differences between the pattern 35 and the patterns 31 and 32. Therefore, the emission of electron from the linear parts 51a and 51b in response to incidence of the electromagnetic wave W on the linear parts 51a and 51b is suppressed. In the third state, the component of the electric field from the leading end 36 of the linear part 51a toward the linear part 41 configuring the bias portion β1 in the Z-axis direction is positive, and the component of the electric field from the leading end 37 of the linear part 51b toward the linear part 43 configuring the bias portion β1 in the Z-axis direction is negative.
In the third state, the electric potential applied to the pattern 35 is higher than the electric potential applied to the pattern 33, and is lower than the electric potential applied to the pattern 34. In other words, the electric potential applied to the linear part 46 configuring the bias portion β2 is lower than the electric potential applied to the linear part 52a configuring the antenna portion α2. The electric potential applied to the linear part 48 configuring the bias portion β2 is higher than the electric potential applied to the linear part 52b configuring the antenna portion α2.
In this case, as illustrated in
As a result, in the third state, an electric potential barrier of the leading end portion of the antenna portion α2 configured by the linear part 52a becomes thick. In other words, an electric potential barrier in an antenna-vacuum interface becomes thicker due to the electric potential difference between the pattern 35 and the pattern 33. Therefore, the emission of electron from the linear part 52a in response to incidence of the electromagnetic wave W on the linear part 52a is suppressed. In the third state, the component of the electric field from the leading end 38 of the linear part 52a toward the linear part 46 configuring the bias portion β2 in the Y-axis direction is positive.
In the third state, an electric potential barrier of the leading end portion of the antenna portion α2 configured by the linear part 52b becomes thin. In other words, an electric potential barrier in an antenna-vacuum interface becomes thinner due to the electric potential difference between the pattern 35 and the pattern 34. Therefore, the emission of electron P from the linear part 52b in response to incidence of the electromagnetic wave W on the linear part 52b is promoted. In the third state, the component of the electric field from the linear part 48 configuring the bias portion β2 toward the leading end 39 of the linear part 52b configuring the antenna portion α2 in the Y-axis direction is positive. Therefore, in a case where the component of the electric field strength of the electromagnetic wave W entering the photoelectric conversion unit 25 in the third state in the Y-axis direction is positive, the electric potential barrier in the antenna-vacuum interface becomes further thinner in response to incidence of the electromagnetic wave W. Therefore, in a case where the component of the electric field strength of the electromagnetic wave W entering the photoelectric conversion unit 25 in the third state in the Z-axis direction is positive, the electron P is emitted from the linear part 52b.
In the fourth state, the electric potential applied to the pattern 35 is higher than the electric potentials applied to the pattern 31 and the pattern 32, in the same manner as the third state. In other words, the electric potential applied to the linear part 41 configuring the bias portion β1 is lower than the electric potential applied to the linear part 51a configuring the antenna portion α1. The electric potential applied to the linear part 43 configuring the bias portion β1 is lower than the electric potential applied to the linear part 51a configuring the antenna portion α1.
Also in the fourth state, as illustrated in
Therefore, the emission of electron from the linear parts 51a and 51b in response to incidence of the electromagnetic wave W on the linear parts 51a and 51b is suppressed. In the fourth state, the component of the electric field from the leading end 36 of the linear part 51a toward the linear part 41 configuring the bias portion β1 in the Z-axis direction is positive, and the component of the electric field from the leading end 37 of the linear part 51b toward the linear part 43 configuring the bias portion β1 in the Z-axis direction is negative.
In the fourth state, the electric potential applied to the pattern 35 is lower than the electric potential applied to the pattern 33, and is higher than the electric potential applied to the pattern 34. In other words, the electric potential applied to the linear part 46 configuring the bias portion β2 is higher than the electric potential applied to the linear part 52a configuring the antenna portion α2. The electric potential applied to the linear part 48 configuring the bias portion 2 is lower than the electric potential applied to the linear part 52b configuring the antenna portion α2.
In this case, as illustrated in
As a result, in the fourth state, an electric potential barrier of the leading end portion of the antenna portion α2 configured by the linear part 52a becomes thin. In other words, an electric potential barrier in an antenna-vacuum interface becomes thinner due to the electric potential difference between the pattern 35 and the pattern 33. Therefore, the emission of electron P from the linear part 52a in response to incidence of the electromagnetic wave W on the linear part 52a is promoted. In the fourth state, the component of the electric field from the linear part 46 configuring the bias portion β2 toward the leading end 38 of the linear part 52a configuring the antenna portion 2 in the Y-axis direction is negative. Therefore, in a case where the component of the electric field strength of the electromagnetic wave W entering the photoelectric conversion unit 25 in the fourth state in the Y-axis direction is negative, the electric potential barrier in the antenna-vacuum interface becomes further thinner in response to incidence of the electromagnetic wave W. As a result, in a case where the component of the electric field strength of the electromagnetic wave W entering the photoelectric conversion unit 25 in the fourth state in the Y-axis direction is negative, the electron P is emitted from the linear part 52a.
In the fourth state, an electric potential barrier of the leading end portion of the antenna portion α2 configured by the linear part 52b becomes thick. In other words, an electric potential barrier in an antenna-vacuum interface becomes thicker due to the electric potential difference between the pattern 35 and the pattern 34. Therefore, the emission of electron from the linear part 52b in response to incidence of the electromagnetic wave W on the linear part 52b is suppressed. In the fourth state, the component of the electric field from the leading end 39 of the linear part 52b toward the linear part 48 configuring the bias portion β2 in the Y-axis direction is negative.
The computing unit 75 computes the polarization information of the electric field strength of the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the first state, the second state, the third state, and the fourth state. The result of detection of the electron collecting unit 50 is information indicating the emission intensity of the electron emitted from the electron emitter 20, for example. The emission intensity stands for the amount of the emitted electron, and depends upon the electric field strength of the electromagnetic wave W entering the electron emitter 20. For example, the computing unit 75 computes first information relating to a positive component in the Z-axis direction of the electric field strength of the electromagnetic wave W, based on the result of detection of the electron collecting unit 50 in the first state. The computing unit 75 computes second information relating to a negative component in the Z-axis direction of the electric field strength of the electromagnetic wave W, based on the result of detection of the electron collecting unit 50 in the second state. The computing unit 75 computes third information relating to a positive component in the Y-axis direction of the electric field strength of the electromagnetic wave W, based on the result of detection of the electron collecting unit 50 in the third state. The computing unit 75 computes fourth information relating to a negative component in the Y-axis direction of the electric field strength of the electromagnetic wave W, based on the result of detection of the electron collecting unit 50 in the fourth state. The computing unit 75 computes the polarization information of the electric field strength of the electromagnetic wave W entering the electron emitter 20, based on the first information, the second information, the third information, and the fourth information.
The computing unit 75 computes the electric field strength of the Z-axis directional component in the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the first state and the second state. The computing unit 75 determines the polarity in the Z-axis direction for the electric field strength of the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the first state and the second state. For example, the computing unit 75 determines the polarity of the electric field in the Z-axis direction by comparing the result of detection of the electron collecting unit 50 in the first state with the result of detection of the electron collecting unit 50 in the second state. The computing unit 75 computes the electric field strength of the Y-axis directional component in the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the third state and the fourth state. The computing unit 75 determines the polarity in the Y-axis direction for the electric field strength of the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the third state and the fourth state. For example, the computing unit 75 determines the polarity of the electric field in the Y-axis direction by comparing the result of detection of the electron collecting unit 50 in the third state with the result of detection of the electron collecting unit 50 in the fourth state. The computing unit 75 computes the polarization information of the electromagnetic wave W entering the electron emitter 20, based on the electric field strength of the Z-axis directional component and the electric field strength of the Y-axis directional component. For example, the computing unit 75 determines the polarization direction of the electromagnetic wave W entering the electron emitter 20 by comparing the electric field strength of the Z-axis directional component with the electric field strength of the Y-axis directional component.
Next, a modification of the electron emitter will be described with reference to
In this modification, an electron emitter 20 includes a meta-surface 22A. The meta-surface 22A corresponds to the meta-surface 22. The meta-surface 22A is of an active type, and is operated by application of a bias voltage. The meta-surface 22A is operated by application of electric potentials by means of a power supply unit 70.
The meta-surface 22A illustrated in
The meta-surface 22A illustrated in
The antenna portions α1, α2, and α3 emit the electron P in response to incidence of the electromagnetic wave W. The bias portion β3 faces the antenna portion α3. The bias portion β3 is configured to generate an electric field having a component in the Y-axis direction between the bias portion β3 and the corresponding antenna portion α3 when the bias electric potential is applied. In this modification, the bias portion β3 generates an electric field in the γ1-axis direction between the bias portion β3 and the antenna portion α3. The bias portion β3 generates an electric field between the bias portion β3 and the corresponding antenna portion α3 when the bias electric potential is applied. When a higher electric potential than the antenna portion α3 is applied to the bias portion β3, an electric potential barrier in the leading end portion of the bias portion β3 side in the antenna portion α3 becomes thin. When a lower electric potential than the antenna portion α3 is applied to the bias portion β3, the electric potential barrier in the leading end portion of the bias portion β3 side in the antenna portion α3 becomes thick. When the electromagnetic wave W enters the antenna portion α3, the electric field is induced around the antenna portion α3 in the same manner as the antenna portions α1 and α2, and in a case where the electric potential barrier becomes further thin by the incidence of the electromagnetic wave W on the antenna portion α3 in the forward bias state, the field electron emission can be generated.
Each of the patterns 31A, 32A, 33A, 34A, 35A, 81A, and 82A is disposed on the principal surface 21b of the supporting body 21. The plurality of patterns 31A, 32A, 33A, 34A, 35A, 81A, and 82A are connected via an oxide layer. The plurality of patterns 31A, 32A, 33A, 34A, 35A, 81A, and 82A are separated from each other by the oxide layer, and are insulated from each other at least when the photoelectric conversion device 2 is not operated. Each of the patterns 31A, 32A, 33A, 34A, 35A, 81A, and 82A is a conductive line, and conducts the electron. Each of the patterns 31A, 32A, 33A, 34A, 35A, 81A, and 82A includes a metal layer which is formed at least on the oxide layer of the meta-surface 22A. A material of the metal layer includes, for example, gold.
In the example illustrated in
The pattern 32A includes a plurality of linear parts 43A and a linear part 44A electrically connecting the plurality of linear parts 43A to each other. Each of the linear parts 43A extends in a Y-axis direction. Each of the linear parts 43A configures the bias portion β1. Each of the linear parts 43A is formed into a rectangular shape extending in the Y-axis direction, for example. The linear part 41A and the linear part 43A corresponding to each other are disposed on the same line extending in the Z-axis direction. The pattern 35 is disposed between the linear part 41A and the linear part 43A corresponding to each other. The linear part 44A is connected to each of the linear parts 43A. In this modification, the plurality of linear parts 43A are arrayed on the same line in the Y-axis direction, and the linear parts 43A adjacent to each other are connected by a plurality of linear parts 44A. When the linear part 41A corresponds to the first portion, the linear part 43A corresponds to the second portion.
The pattern 33A includes a plurality of linear parts 46A and a linear part 47A electrically connecting the plurality of linear parts 46A to each other. Each of the linear parts 46A extends in a Z-axis direction. Each of the linear parts 46A configures the bias portion β2. Each of the linear parts 46A is formed into a rectangular shape extending in the Z-axis direction, for example. The linear part 47A is connected to each of the linear parts 46A. In this modification, the plurality of linear parts 46A are arrayed on the same line in the Z-axis direction, and the linear parts 46A adjacent to each other are connected by a plurality of linear parts 47A.
The pattern 34A includes a plurality of linear parts 48A and a linear part 49A electrically connecting the plurality of linear parts 48A to each other. Each of the linear parts 48A extends in a Z-axis direction. Each of the linear parts 48A configures the bias portion 2. Each of the linear parts 48A is formed into a rectangular shape extending in the Z-axis direction, for example. The linear part 46A and the linear part 48A corresponding to each other are disposed on the same line extending in the Y-axis direction. The pattern 35 is disposed between the linear part 46A and the linear part 48A corresponding to each other. The linear part 49A is connected to each of the linear parts 48A. In this modification, the plurality of linear parts 48A are arrayed on the same line in the Z-axis direction, and the linear parts 48A adjacent to each other are connected by a plurality of linear parts 49A. When the linear part 46A corresponds to the third portion, the linear part 48A corresponds to the fourth portion.
The pattern 81A includes a plurality of linear parts 86A and a linear part 87A electrically connecting the plurality of linear parts 86A to each other. Each of the linear parts 86A extends in a γ2-axis direction. Each of the linear parts 86A configures the bias portion β3. Each of the linear parts 86A is formed into a rectangular shape extending in the γ2-axis direction, for example. The linear part 87A is connected to each of the linear parts 86A. In this modification, the plurality of linear parts 86A are arrayed on the same line in the γ2-axis direction, and the linear parts 86A adjacent to each other are connected by a plurality of linear parts 87A.
The pattern 82A includes a plurality of linear parts 88A and a linear part 89A electrically connecting the plurality of linear parts 88A to each other. Each of the linear parts 88A extends in a γ2-axis direction γ2-axis direction. Each of the linear parts 88A configures the bias portion β2. Each of the linear parts 88A is formed into a rectangular shape extending in the γ2-axis direction, for example. The linear part 86A and the linear part 88A corresponding to each other are disposed on the same line extending in the γ1-axis direction. The pattern 35 is disposed between the linear part 86A and the linear part 88A corresponding to each other. The linear part 89A is connected to each of the linear parts 88A. In this modification, the plurality of linear parts 88A are arrayed on the same line in the γ2-axis direction, and the linear parts 88A adjacent to each other are connected by a plurality of linear parts 89A. When the linear part 86A corresponds to the fifth portion, the linear part 88A corresponds to the sixth portion.
The pattern 35A extends toward the patterns 31A and 32A, the patterns 33A and 34A, and the patterns 81A and 82A. In a state where a lower electric potential than that applied to the pattern 31A, the pattern 32A, the pattern 33A, the pattern 34A, the pattern 81A, or the pattern 82A is applied to the pattern 35A, the pattern 35A emits the electron P in response to incidence of the electromagnetic wave W. The pattern 35A includes a plurality of linear parts 91, a plurality of linear parts 92, and a plurality of linear parts 95. The linear part 91, the linear part 92, and the linear part 95 respectively extend in directions intersecting one another in the YZ plane. In other words, a direction where the linear part 91 extends, a direction where the linear part 92 extends, and a direction where the linear part 95 extends intersect each other. In the present modification, the linear part 91 and the linear part 92 respectively extend in directions orthogonal to each other.
Each of the linear parts 91 extends in the Z-axis direction and has the same configuration as that of the above-described linear part 51. Each of the linear parts 91 configures the antenna portion α1 in the same manner as the linear part 51. The pattern 35A includes a linear part 93 electrically connecting the plurality of linear parts 91 to each other. The linear part 93 is connected to each of the linear parts 91. Each of the linear parts 91 includes a pair of linear parts 91a and 91b corresponding to the pair of linear parts 51a and 51b. The linear part 91a extends in a +Z-axis direction from a portion connected to the linear part 93. The linear part 91b extends in a-Z-axis direction from a portion connected to the linear part 93. In this modification, each of the linear parts 91 is disposed between the linear part 41A and the linear part 43A in the Z-axis direction.
Each of the linear parts 92 extends in the Y-axis direction and has the same configuration as that of the above-described linear part 52. Each of the linear parts 92 configures the antenna portion α2 in the same manner as the linear part 52. The above-described linear part 93 electrically connects the plurality of linear parts 92 to each other. The linear part 93 is connected to each of the linear parts 92. Each of the linear parts 92 includes a pair of linear parts 92a and 92b corresponding to the pair of linear parts 52a and 52b. The linear part 92a extends in a +Y-axis direction from a portion connected to the linear part 93. The linear part 92b extends in a-Y-axis direction from a portion connected to the linear part 93. In this modification, each of the linear parts 92 is disposed between the linear part 46A and the linear part 48A in the Y-axis direction. The plurality of linear parts 91 and the plurality of linear parts 92 are electrically connected by the linear part 93.
Each of the linear parts 95 extends in a γ1-axis direction. Each of the linear parts 95 configures the antenna portion α3. Each of the linear parts 95 is formed into a rectangular shape extending in the γ1-axis direction, for example. The plurality of linear parts 95 are in parallel to each other. The above-described linear part 93 electrically connects the plurality of linear parts 95 to each other. The linear part 93 is connected to each of the linear parts 95. In this modification, the plurality of linear parts 95 are arrayed on the same line in the γ2-axis direction, and the linear parts 95 adjacent to each other are connected by a plurality of linear parts 93.
Each of the linear parts 95 extends in a +γ1-axis direction and a-γ1-axis direction from a portion connected to the linear part 93. Each of the linear parts 93 is connected to the center of each of the linear parts 95. Each of the linear parts 95 includes a pair of linear parts 95a and 95b. The linear part 95a extends in a-γ1-axis direction from a portion connected to the linear part 93. The linear part 95b extends in a +γ1-axis direction from a portion connected to the linear part 93. In the present modification, the pair of linear parts 95a and 95b in each of the linear parts 95 extend on the same line extending in the γ1-axis direction. Each of the linear parts 95 is disposed between a pair of bias portions β3 in the γ1-axis direction. Each of the linear parts 93 is disposed between the pattern 81A and the pattern 82A in the γ1-axis direction. Each of the linear parts 95 is disposed between the linear part 86A and the linear part 88A in the γ1-axis direction.
The pattern 35A includes a leading end 36A facing the pattern 31A, a leading end 37A facing the pattern 32A, a leading end 38A facing the pattern 33A, a leading end 39A facing the pattern 34A, a leading end 96A facing the pattern 81A, and a leading end 97A facing the pattern 82A. In the present modification, each of the linear parts 91 includes the leading end 36A and the leading end 37A, each of the linear parts 92 includes the leading end 38A and the leading end 39A, and each of the linear parts 95 includes the leading end 96A and the leading end 97A.
The leading ends 36A and 37A correspond to the leading ends 36 and 37 described above, respectively. The leading ends 38A and 39A correspond to the leading ends 38 and 39 described above, respectively. The leading end 36A is included in the linear part 91a. The leading end 37A is included in the linear part 91b. The leading ends 36A and the leading end 37A are positioned in both ends of each of the linear parts 91. The leading end 38A is included in the linear part 92a. The leading end 39A is included in the linear part 92b. The leading ends 38A and the leading end 39A are positioned in both ends of each of the linear parts 92.
The leading end 96A faces the bias portion β3. The leading end 96A faces the corresponding linear part 86A. The leading end 96A is the closest portion to the pattern 81A in the linear part 95 including the leading end 96A. The leading end 96A is disposed closer to the corresponding linear part 86A than the other portions of the pattern 35A.
The leading end 97A faces the bias portion β3. The leading end 97A faces the corresponding linear part 88A. The leading end 97A is the closest portion to the pattern 82A in the linear part 95 including the leading end 97A. The leading end 97A is disposed closer to the corresponding linear part 88A than the other portions of the pattern 35A.
The leading end 96A and the leading end 97A, and the linear part 86A and the linear part 88A are disposed in the order of the linear part 86A, the leading end 96A, the leading end 97A, and the linear part 88A in the y-axis direction. In the photoelectric conversion unit 25, each of the linear parts 95 can emit the electron P in response to incidence of the electromagnetic wave W in a state where a lower electric potential than the linear part 86A or the linear part 88A is applied the linear parts 95.
The photoelectric conversion unit 25A is configured to correspond to a range of wavelength, for example, from a millimeter wave to an infrared light by a change of a configuration of the linear parts 91, 92, and 95. For example, a length of the linear part 95 in the γ1-axis direction corresponds to a wavelength region of the electromagnetic wave W which allows the electron P to be emitted in the photoelectric conversion unit 25A. For example, the length of the linear part 95 in the γ1-axis direction is designed according to a desired wavelength region emitting the electron P from the photoelectric conversion unit 25A. For example, each of the linear parts 91, 92, and 95 has a length which is half the length of a center wavelength in the desired wavelength region. The length of each of the linear parts 91 is a length from the leading end 36A to the leading end 37A in the Z-axis direction. The length of each of the linear parts 92 is a length from the leading end 38A to the leading end 39A in the Y-axis direction. The length of each of the linear parts 95 is a length from the leading end 96A to the leading end 97A in the γ1-axis direction. In a case where the electromagnetic wave W having transmitted the supporting body 21 enters the linear parts 91, 92, and 95 in the same manner as the linear parts 51 and 52, a refractive index of the supporting body 21 through which the electromagnetic wave has passed is also taken into consideration.
The electron emitter 20 illustrated in
For example, the electrode 61A is included in the pattern 31A. The electrode 61A is electrically connected to the plurality of linear parts 41A via the linear part 42A. The electrode 61A may be integrally formed with the linear part 42A and the plurality of linear parts 41A. The electrode 62A is included in the pattern 32A. The electrode 62A is electrically connected to the plurality of linear parts 43A via the linear part 44A. The electrode 62A may be integrally formed with the linear part 44A and the plurality of linear parts 43A. The electrode 63A is included in the pattern 33A. The electrode 63A is electrically connected to the plurality of linear parts 46A via the linear part 47A. The electrode 63A may be integrally formed with the linear part 47A and the plurality of linear parts 46A.
The electrode 64A is included in the pattern 34A. The electrode 64A is electrically connected to the plurality of linear parts 48A via the linear part 49A. The electrode 64A may be integrally formed with the linear part 49A and the plurality of linear parts 48A. The electrode 65A is included in the pattern 35A. The electrode 65A is electrically connected to the plurality of linear parts 91, 92, and 95 via the linear part 93. The electrode 65A may be integrally formed with the linear part 93 and the plurality of linear parts 91, 92, and 95. The electrode 67A is included in the pattern 81A. The electrode 67A is electrically connected to the plurality of linear parts 86A via the linear part 87A. The electrode 67A may be integrally formed with the linear part 87A and the plurality of linear parts 86A. The electrode 68A is included in the pattern 82A. The electrode 68A is electrically connected to the plurality of linear parts 88A via the linear part 89A. The electrode 68A may be integrally formed with the linear part 89A and the plurality of linear parts 88A.
The photoelectric conversion unit 25A is operated by application of electric potentials from the power supply unit 70 via the plurality of electrodes 61A, 62A, 63A, 64A, 65A, 67A, and 68A. The potential application unit 71 of the power supply unit 70 applies the electric potentials to the photoelectric conversion unit 25A of the meta-surface 22A via the plurality of electrodes 61A, 62A, 63A, 64A, 65A, 67A, and 68A. The potential control unit 72 of the power supply unit 70 controls the electric potentials applied to the photoelectric conversion unit 25A.
In the photoelectric conversion device 2 provided with the electron emitter 20 in the present modification, the potential control unit 72 switches between the first state and the second state, switches between the third state and the fourth state, and switches between the fifth state and the sixth state by controlling the electric potentials applied to the plurality of patterns 31A, 32A, 33A, 34A, 35A, 81A, and 82A. In the first state, the electric potentials are controlled in such a manner that the electron P is emitted from the leading end 37A of the antenna portion α1 in response to incident of the electromagnetic wave W, and emission of electron from the leading end 36A of the antenna portion α1 as well as the antenna portion α2 and the antenna portion α3 is suppressed. In the second state, the electric potentials are controlled in such a manner that the electron P is emitted from the leading end 36A of the antenna portion α1 in response to incident of the electromagnetic wave W, and emission of electron from the leading end 37A of the antenna portion α1 as well as the antenna portion α2 and the antenna portion α3 is suppressed. In the third state, the electric potentials are controlled in such a manner that the electron P is emitted from the leading end 39A of the antenna portion α2 in response to incident of the electromagnetic wave W, and emission of electron from the leading end 38A of the antenna portion α2 as well as the antenna portion α1 and the antenna portion α3 is suppressed. In the fourth state, the electric potentials are controlled in such a manner that the electron P is emitted from the leading end 38A of the antenna portion α2 in response to incident of the electromagnetic wave W, and emission of electron from the leading end 39A of the antenna portion α2 as well as the antenna portion α1 and the antenna portion α3 is suppressed.
In the fifth state, the electric potentials are controlled in such a manner that the electron P is emitted from the leading end 96A of the antenna portion α3 in response to incident of the electromagnetic wave W, and emission of electron from the leading end 97A of the antenna portion α3 as well as the antenna portion α1 and the antenna portion α2 is suppressed. In the sixth state, the electric potentials are controlled in such a manner that the electron P is emitted from the leading end 97A of the antenna portion α3 in response to incident of the electromagnetic wave W, and emission of electron from the leading end 96A of the antenna portion α3 as well as the antenna portion α1 and the antenna portion α2 is suppressed.
In the fifth state, the electric potential applied to the pattern 35A is lower than the electric potentials applied to the patterns 31A, 32A, 33A, 34A, and 81A, and is higher than the electric potential applied to the pattern 82A. In other words, the electric potential applied to the linear part 88A configuring the bias portion 3 is higher than the electric potential applied to the linear part 95b configuring the antenna portion α3. The electric potential applied to the linear part 86A configuring the bias portion β3 is lower than the electric potential applied to the linear part 95a configuring the antenna portion α3. In the fifth state, the component of the electric field from the leading end 96A of the linear part 95a configuring the antenna portion α3 toward the linear part 86A configuring the bias portion 3 in the γ1-axis direction is negative, and the component of the electric field from the linear part 88A configuring the bias portion β3 toward the leading end 97A of the linear part 95b configuring the antenna portion α3 in the γ1-axis direction is negative.
In the sixth state, the electric potential applied to the pattern 35A is lower than the electric potential applied to the patterns 31A, 32A, 33A, 34A, and 82A, and is higher than the electric potential applied to the pattern 81A. In other words, the electric potential applied to the linear part 88A configuring the bias portion β3 is lower than the electric potential applied to the linear part 95b configuring the antenna portion α3. The electric potential applied to the linear part 86A configuring the bias portion β3 is higher than the electric potential applied to the linear part 95a configuring the antenna portion α3. In the sixth state, the component of the electric field from the leading end 97A of the linear part 95b configuring the antenna portion α3 toward the linear part 88A configuring the bias portion β3 in the γ1-axis direction is positive, and the component of the electric field from the linear part 86A configuring the bias portion β3 toward the leading end 96A of the linear part 95a configuring the antenna portion α3 in the γ1-axis direction is positive.
In the present modification, the computing unit 75 computes the polarization information of the electric field strength of the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the first state, the second state, the third state, the fourth state, the fifth state, and the sixth state. For example, the computing unit 75 computes the first information, the second information, the third information, and the fourth information in the same manner as the above-described embodiment. The computing unit 75 computes fifth information relating to a negative component in the γ1-axis direction of the electric field strength of the electromagnetic wave W, based on the result of detection of the electron collecting unit 50 in the fifth state. The computing unit 75 computes sixth information relating to a positive component in the γ1-axis direction of the electric field strength of the electromagnetic wave W, based on the result of detection of the electron collecting unit 50 in the sixth state. The computing unit 75 computes the polarization information of the electric field strength of the electromagnetic wave W entering the electron emitter 20, based on the first information, the second information, the third information, the fourth information, the fifth information, and the sixth information.
The computing unit 75 computes the electric field strength of the Z-axis directional component in the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the first state and the second state, in the same manner as the above-described embodiment. The computing unit 75 determines the polarity in the Z-axis direction for the electric field strength of the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the first state and the second state. The computing unit 75 computes the electric field strength of the Y-axis directional component in the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the third state and the fourth state, in the same manner as the above-described embodiment. The computing unit 75 determines the polarity in the Y-axis direction for the electric field strength of the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the third state and the fourth state. The computing unit 75 computes the electric field strength of the γ1-axis directional component in the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the fifth state and the sixth state. The computing unit 75 determines the polarity in the γ1-axis direction for the electric field strength of the electromagnetic wave W entering the electron emitter 20, based on the results of detection of the electron collecting unit 50 in the fifth state and the sixth state. For example, the computing unit 75 determines the polarity of the electric field in the Y-axis direction by comparing the result of detection of the electron collecting unit 50 in the fifth state with the result of detection of the electron collecting unit 50 in the sixth state. The computing unit 75 computes the polarization information of the electromagnetic wave W entering the electron emitter 20, based on the electric field strength of the Z-axis directional component, the electric field strength of the Y-axis directional component, and the electric field strength of the y-axis directional component. For example, the computing unit 75 determines which of linear polarization, circular polarization, and elliptic polarization the electromagnetic wave entering the electron emitter 20 is by comparing the electric field strength of the Z-axis directional component, the electric field strength of the Y-axis directional component, and the electric field strength of the y-axis directional component. The computing unit 75 determines the polarization direction of the electromagnetic wave W entering the electron emitter 20.
Next, another modification of the electron emitter will be described with reference to
The electron emitter 20 illustrated in
For example, the electrode 61B is included in the pattern 31B. The electrode 61B is electrically connected to the plurality of linear parts 41A via the linear part 42A. The electrode 61B is electrically connected to the plurality of linear parts 43A via the linear part 44A. The electrode 61B may be integrally formed with the linear parts 42A and 44A and the plurality of linear parts 41A and 43A. The electrode 63B is included in the pattern 33B. The electrode 63B is electrically connected to the plurality of linear parts 46A via the linear part 47A. The electrode 63B is electrically connected to the plurality of linear parts 48A via the linear part 49A. The electrode 63B may be integrally formed with the linear parts 47A and 49A and the plurality of linear parts 46A and 48A. The electrode 65A is included in the pattern 35B. The electrode 65A is electrically connected to the plurality of linear parts 91, 92, and 95 via the linear part 93. The electrode 65A may be integrally formed with the linear part 93 and the plurality of linear parts 91, 92, and 95. The electrode 67B is included in the pattern 81B. The electrode 67B is electrically connected to the plurality of linear parts 86A via the linear part 87A. The electrode 67B is electrically connected to the plurality of linear parts 88A via the linear part 89A. The electrode 67B may be integrally formed with the linear parts 87A and 89A and the plurality of linear parts 86A and 88A.
The photoelectric conversion unit 25A is operated by application of electric potentials from the power supply unit 70 via the plurality of electrodes 61B, 63B, 65A, and 67B. The potential application unit 71 of the power supply unit 70 applies the electric potentials to the photoelectric conversion unit 25A via the plurality of electrodes 61B, 63B, 65A, and 67B. The potential control unit 72 of the power supply unit 70 controls the electric potentials applied to the photoelectric conversion unit 25A.
In the photoelectric conversion device 2 provided with the electron emitter 20 in the present modification, the potential control unit 72 switches between the seventh state, the eighth state, and the ninth state by controlling the electric potentials applied to the plurality of patterns 31B, 33B, 35B, and 36B. In the seventh state, the electric potentials are controlled in such a manner that the electron P is emitted from the leading end 36A and the leading end 37A of the antenna portion α1 in response to incident of the electromagnetic wave W, and emission of electron from the antenna portion α2 and the antenna portion α3 is suppressed. In the eighth state, the electric potentials are controlled in such a manner that the electron P is emitted from the leading ends 38A and 39A of the antenna portion α2 in response to incident of the electromagnetic wave W, and emission of electron from the antenna portion α1 and the antenna portion α3 is suppressed. In the ninth state, the electric potentials are controlled in such a manner that the electron P is emitted from the leading ends 96A and 97A of the antenna portion α3 in response to incident of the electromagnetic wave W, and emission of electron from the antenna portion α1 and the antenna portion α2 is suppressed.
In the seventh state, the electric potential applied to the pattern 35B is lower than the electric potential applied to the pattern 31B, and is higher than the electric potentials applied to the patterns 33B and 81B. In other words, the electric potential applied to the bias portion β1 configured by the linear parts 41A and 43A is higher than the electric potential applied to the antenna portion α1 configured by the linear parts 91a and 91b. In the seventh state, the component of the electric field from the bias portion β1 configured by the linear part 41A toward the leading end 36A of the linear part 91a in the Z-axis direction is negative, and the component of the electric field from the bias portion β1 configured by the linear part 43A toward the leading end 37A of the linear part 91b in the Z-axis direction is positive.
In the eighth state, the electric potential applied to the pattern 35B is lower than the electric potential applied to the pattern 33B, and is higher than the electric potential applied to the patterns 31B and 81B. In other words, the electric potential applied to the bias portion β2 configured by the linear parts 46A and 48A is higher than the electric potential applied to the antenna portion α2 configured by the linear parts 92a and 92b. In the eighth state, the component of the electric field from the bias portion β2 configured by the linear part 46A toward the leading end 38A of the linear part 92a in the Y-axis direction is negative, and the component of the electric field from the bias portion β2 configured by the linear part 48A toward the leading end 39A of the linear part 92b in the Y-axis direction is positive.
In the ninth state, the electric potential applied to the pattern 35B is lower than the electric potential applied to the pattern 81B, and is higher than the electric potentials applied to the patterns 31B and 33B. In other words, the electric potential applied to the bias portion β3 configured by the linear parts 86A and 88A is higher than the electric potential applied to the antenna portion α3 configured by the linear parts 95a and 95b. In the ninth state, the component of the electric field from the bias portion β3 configured by the linear part 86A toward the leading end 96A of the linear part 95a in the γ1-axis direction is positive, and the component of the electric field from the bias portion β3 configured by the linear part 88A toward the leading end 97A of the linear part 95b in the γ1-axis direction is negative.
In the present modification, the computing unit 75 computes the electric field strength of the Z-axis directional component in the electromagnetic wave W entering the electron emitter 20, based on the result of detection of the electron collecting unit 50 in the seventh state. The computing unit 75 computes the electric field strength of the Y-axis directional component in the electromagnetic wave W entering the electron emitter 20, based on the result of detection of the electron collecting unit 50 in the eighth state. The computing unit 75 computes the electric field strength of the γ1-axis directional component in the electromagnetic wave W entering the electron emitter 20, based on the result of detection of the electron collecting unit 50 in the ninth state. The computing unit 75 computes the polarization information of the electromagnetic wave W entering the electron emitter 20, based on the electric field strength of the Z-axis directional component, the electric field strength of the Y-axis directional component, and the electric field strength of the γ1-axis directional component. For example, the computing unit 75 determines which of circular polarization and elliptic polarization the electromagnetic wave W entering the electron emitter 20 is by comparing the electric field strength of the Z-axis directional component, the electric field strength of the Y-axis directional component, and the electric field strength of the γ1-axis directional component.
Next, the structure of the pattern according to yet another modification of the present embodiment will be described in detail with reference to
In the examples illustrated in
In the examples illustrated in
In the examples illustrated in
The leading end 36 of the linear part 51a faces the leading end 101 and the leading end 102. In the Z-axis direction, the leading end 36 of the linear part 51 is positioned between the leading end 101 and the leading end 102. The shortest distance between the leading end 36 and the leading end 101 is equal to the shortest distance between the leading end 36 and the leading end 102. The distance between the leading end 36 and the leading end 101 in the Y-axis direction is equal to the distance between the leading end 36 and the leading end 102 in the Y-axis direction. The distance between the leading end 36 and the leading end 101 in the Z-axis direction is equal to the distance between the leading end 36 and the leading end 102 in the Z-axis direction. The leading end 101 and the leading end 102 facing the same leading end 36 are included in mutually different linear parts 41.
The leading end 37 of the linear part 51b faces the leading end 103 and the leading end 104. In the Z-axis direction, the leading end 37 of the linear part 51 is positioned between the leading end 103 and the leading end 104. The shortest distance between the leading end 37 and the leading end 103 is equal to the shortest distance between the leading end 37 and the leading end 104. The distance between the leading end 37 and the leading end 103 in the Y-axis direction is equal to the distance between the leading end 37 and the leading end 104 in the Y-axis direction. The distance between the leading end 37 and the leading end 103 in the Z-axis direction is equal to the distance between the leading end 37 and the leading end 104 in the Z-axis direction. The leading end 103 and the leading end 104 facing the same leading end 37 are included in mutually different linear parts 43.
In the example illustrated in
In the same manner as the embodiment described above, the length of the linear part 51 in the Z-axis direction is designed according to a desired wavelength region emitting the electron P from the photoelectric conversion unit 25. In the example illustrated in
In the example illustrated in
Next, an electromagnetic wave detection method according to the present embodiment will be described with reference to
An outline of the electromagnetic wave detection method according to the present embodiment will be described with reference to
Next, an electromagnetic wave W to be measured enters the electron emitter 20 (process S2). In the present embodiment, in the process S2, the application of the electromagnetic wave W to the electron emitter 20 is started, and the application of the electromagnetic wave W to the electron emitter 20 is continued until the detection of the electromagnetic wave W is finished.
Next, the process of acquiring the electric field strength in each directional component is executed (process S3). In the process S3, the computing unit 75 computes the electric field strength of each directional component.
Next, the polarization information of the electromagnetic wave W entering the electron emitter 20 is computed (process S4). In the process S4, the computing unit 75 computes the polarization information of the electromagnetic wave W entering the electron emitter 20. For example, the computing unit 75 compares the information relating to the electric field strength of each of the directional component acquired in the process S3, and computes the polarization information of the electromagnetic wave W entering the electron emitter 20. For example, the computing unit 75 compares the computed electric field strength of each directional component and outputs the polarization direction of the electromagnetic wave W entering the electron emitter 20.
Next, the process S3 will be described in detail with reference to
First, the electric potential applied to each of the patterns is determined (process S11). In the present embodiment, the potential control unit 72 determines the electric potential applied to each of the patterns 31, 32, 33, 34, and 35 so as to bring into any one of the first state, the second state, the third state, and the fourth state. For example, in the case of the configuration illustrated in
Next, an electric potential is applied to each of the patterns (process S12). For example, the potential application unit 71 applies an electric potential to each of the patterns via an electrode in accordance with an instruction from the potential control unit 72. For example, the potential application unit 71 applies the electric potential determined in the immediately preceding process S11 to each of the patterns 31, 32, 33, 34, and 35. The potential application unit 71 applies the electric potential determined in the immediately preceding process S11 to each of the patterns at least until the process S13 and the process S14 are finished.
Next, an electron is emitted from the meta-surface in a state where an electric potential is applied to each of the patterns (process S13). For example, when the electromagnetic wave W to be measured enters the meta-surface 22 in a state where the electric potential determined in the immediately preceding process S11 is applied to each of the patterns 31, 32, 33, 34, and 35, the electron emitter 20 emits the electron P from the leading end of any one of the antenna portion α1 and the antenna portion α2. Which leading end of the antenna portion α1 or the antenna portion α2 the electron P is to be emitted from depends on how the electric potential is applied to each of the patterns in the process S12. For example, if the state of electric potential applied to each of the patterns is the first state, the electron P is emitted from the leading end 37 of the antenna portion α1. If the state of electric potential applied to each of the patterns is the second state, the electron P is emitted from the leading end 36 of the antenna portion α1. If the state of electric potential applied to each of the patterns is the third state, the electron P is emitted from the leading end 39 of the antenna portion α2. If the state of electric potential applied to each of the patterns is the fourth state, the electron P is emitted from the leading end 38 of the antenna portion α2.
For example, in the configuration illustrated in
Next, the emitted electron P is detected (process S14). For example, the electron collecting unit 50 collects the electron P emitted in the process S13 and detects the collected electron P. The computing unit 75 acquires a signal output from the electron collecting unit 50.
Next, information relating to the electric field strength is computed (process S15). For example, the computing unit 75 computes information relating to an electric field strength of an electromagnetic wave W, based on the signal acquired from the electron collecting unit 50 in the process S14. For example, if the state of electric potential applied to each of the patterns is the first state in the process S13 and the process S14, the computing unit 75 computes the first information relating to the positive component of the electric field strength of the electromagnetic wave W in the Z-axis direction.
Next, it is determined whether or not information relating to the electric field strength of the positive and negative components in the same axial direction has been acquired (process S16). For example, the computing unit 75 determines whether or not information relating to the electric field strength of both the positive and negative components in the same axial direction has been acquired, regarding the directional component of the electric field strength computed in the immediately preceding process S15. For example, if it is acquired that the information relating to the electric field strength of the positive component in the direction of the Z-axis has been computed in the immediately preceding process S15, the computing unit 75 determines that the information relating to the electric field strength of the negative component in the direction of the Z-axis has not been acquired. For example, if the state of electric potential applied to each of the patterns in the immediately preceding processes S13 and S14 is the first state, the computing unit 75 determines that the information in the second state, i.e., the second information relating to the electric field strength of the negative component in the direction of the Z-axis has not been acquired.
If it is not determined that the information relating to the electric field strength of the positive and negative components in the same axial direction has been acquired, the process returns to the process S11. At this time, in the process S11, the electric potential applied to each of the patterns is determined in such a manner that the information relating to the electric field strength of the polarity having not been acquired is acquired. For example, if it is determined that the first information has been acquired and the second information has not been acquired in the process S16, the potential control unit 72 determines the electric potential applied to each of the patterns 31, 32, 33, 34, and 35 so as to bring into the second state in the process S11. For example, if it is determined that the third information has been acquired and the fourth information has not been acquired in the process S16, the potential control unit 72 determines the electric potential applied to each of the patterns 31, 32, 33, 34, and 35 so as to bring into the fourth state in the process S11.
If it is determined that the information relating to the electric field strength of the positive and negative components has been acquired, the polarity of the electric field is determined (process S17). For example, the computing unit 75 determines the polarity of the electric field of the electromagnetic wave W in the Z-axis direction, based on the first information and the second information. The computing unit 75 determines the polarity of the electric field of the electromagnetic wave W in the Y-axis direction, based on the third information and the fourth information. In the configuration illustrated in
When the process S17 is finished, it is determined whether or not information relating to the electric field strength of all the directional components has been acquired (process S18). For example, the computing unit 75 determines whether or not the first and second information relating to the electric field strength of the Z-axis directional component and the third and fourth information relating to the electric field strength of the Y-axis directional component have been acquired. In the configuration illustrated in
If it is not determined that the information relating to the electric field strength of all the directional components has been acquired, the process returns to the process S11. At this time, in the process S11, the electric potential applied to each of the patterns is determined in such a manner that the information relating to the electric field strength of the directional component having not been acquired is acquired. For example, if it is determined that the information relating to the electric field strength of the Y-axis directional component has not been acquired in the process S18, the potential control unit 72 determines the electric potential applied to each of the patterns 31, 32, 33, 34, and 35 so as to bring into the third or fourth state in the process S11. In the configuration illustrated in
If it is determined that the information relating to the electric field strength of all the directional components has been acquired, the series of process in the process S3 is finished. The process S11 to the process S17 is repeated until the information relating to the electric field strength of all the directional components is acquired in the process S18. By repeating the process S11 to the process S14, the electron P is emitted in each of the above-mentioned first to fourth states. In the present embodiment, by repeating the process S11 to the process S14, an electric potential is applied to each of the patterns in the order of the first state, the second state, the third state, and the fourth state. In the configuration illustrated in
By repeating the process S15, the electron P emitted in each of the first to fourth states is detected. In the configuration illustrated in
The orders from the process S1 to the process S4 and from the process S11 to the process S18 are not limited to the orders illustrated in
As mentioned above, in the electromagnetic wave detection method according to the present embodiment, the electron P emitted from the electron emitter 20 is detected in each of the states, and the polarization information of the electromagnetic wave W is computed. For example, the computing unit 75 computes the first information to the fourth information, and computes the polarization information of the electromagnetic wave W entering the electron emitter 20, based on the first information to the fourth information. In the configuration illustrated in
In the photoelectric conversion device 2, the antenna portion α1 and the antenna portion α2 extend in the Z-axis direction and the Y-axis direction, which intersect with each other. The bias portion β1 is configured to generate an electric field having a component in the Z-axis direction between the bias portion β1 and the antenna portion α1. The bias portion 2 is configured to generate an electric field having a component in the Y-axis direction between the bias portion β2 and the antenna portion α2. According to such a configuration, the antenna portion α1 emits the electron P according to the component in the Z-axis direction of the electric field strength of the electromagnetic wave W. The antenna portion 2 emits the electron P according to the component in the Y-axis direction of the electric field strength of the electromagnetic wave W. As a result, the electron P emitted according to the component in the Z-axis direction of the electric field strength of the electromagnetic wave W and the electron P emitted according to the component in the Y-axis direction of the electric field strength of the electromagnetic wave W can be detected. For example, according to these detection results, a rate between the component of the electric field strength of the electromagnetic wave W in the Z-axis direction and the component of the electric field strength of the electromagnetic wave W in the Y-axis direction can be computed. With the computed rate, detection of the polarization state of an electromagnetic wave can be easily achieved. The photoelectric conversion device 2 is not required to be cooled.
The photoelectric conversion device 2 further includes the potential control unit 72 controlling electric potentials applied to the meta-surface 22 or the meta-surface 22A. For example, the potential control unit 72 switches between the first state and the second state and switches between the third state and the fourth state by controlling the electric potentials applied to the plurality of patterns 31, 32, 33, 34, and 35 of the meta-surface 22. In this case, when the electromagnetic wave W enters the meta-surface 22 or the meta-surface 22A in the first state, the electron P is emitted from the antenna portion α1 according to the positive component of the electric field strength of the entered electromagnetic wave W in the Z-axis direction. When the electromagnetic wave W enters the meta-surface 22 or the meta-surface 22A in the second state, the electron P is emitted from the antenna portion α1 according to the negative component of the electric field strength of the entered electromagnetic wave W in the Z-axis direction. When the electromagnetic wave W enters the meta-surface 22 or the meta-surface 22A in the third state, the electron P is emitted from the antenna portion α2 according to the positive component of the electric field strength of the entered electromagnetic wave W in the Y-axis direction. When the electromagnetic wave W enters the meta-surface 22 or the meta-surface 22A in the fourth state, the electron P is emitted from the antenna portion α2 according to the negative component of the electric field strength of the entered electromagnetic wave W in the Y-axis direction. Therefore, the photoelectric conversion device 2 can achieve measurement of the electric field strength of the electromagnetic wave W for each polarity in the Z-axis direction by detecting the electron P emitted from the meta-surface 22 or the meta-surface 22A in the first state and the second state. In the same manner, measurement of the electric field strength of the electromagnetic wave W for each polarity in the Y-axis direction can be achieved by detecting the electron P emitted from the meta-surface 22 or the meta-surface 22A in the third state and the fourth state. As a result, the detection of the polarization state of the electromagnetic wave W can be achieved more accurately in consideration of the polarity of each directional component.
In the photoelectric conversion device 2, the computing unit 75 determines the polarity of the electric field in each axial direction in the electric field strength of the electromagnetic wave W. Therefore, in addition to the polarization state of the electromagnetic wave W, more detailed information relating to the electromagnetic wave W is acquired. For example, electric field waveform data of the electromagnetic wave W can be acquired.
In the configuration illustrated in
In the configuration illustrated in
The antenna portion α1 of the meta-surface 22 includes the leading ends 36 and 37 which are disposed at mutually different positions in the Z-axis direction. The bias portion β1 includes the linear parts 41 and 43. The linear part 41 faces the leading end 36 and generates an electric field having a component in the Z-axis direction between the linear part 41 and the leading end 36. The linear part 43 faces the leading end 37 and generates an electric field having a component in the Z-axis direction between the linear part 43 and the leading end 37. The antenna portion α2 includes the leading ends 38 and 39 which are disposed at mutually different positions in the Y-axis direction. The bias portion β2 includes the linear parts 46 and 48. The linear part 46 faces the leading end 38 and generates an electric field having a component in the Y-axis direction between the linear part 46 and the leading end 38. The linear part 48 faces the leading end 39 and generates an electric field having a component in the Y-axis direction between the linear part 48 and the leading end 39. The leading ends 36 and 37, and the linear parts 41 and 43 are disposed in the order of the linear part 43, the leading end 37, the leading end 36, and the linear part 41 in the Z-axis direction. The leading ends 38 and 39, and the linear parts 46 and 48 are disposed in the order of the linear part 48, the leading end 39, the leading end 38, and the linear part 46 in the Y-axis direction. In this case, the measurement of the electric field strength of the electromagnetic wave W entering the electron emitter 20 can be achieved for each polarity in each of the Z-axis direction and the Y-axis direction by detecting the electron P emitted from the meta-surface 22, with a simple configuration. The same operations and effects can be also achieved in the meta-surface 22A.
For example, in the first state, the component of the electric field from the leading end 36 toward the linear part 41 in the Z-axis direction is positive, the component of the electric field from the linear part 43 toward the leading end 37 in the Z-axis direction is positive, the component of the electric field from the leading end 38 toward the linear part 46 in the Y-axis direction is positive, and the component of the electric field from the leading end 39 toward the linear part 48 in the Y-axis direction is negative. In the second state, the component of the electric field from the linear part 41 toward the leading end 36 in the Z-axis direction is negative, the component of the electric field from the leading end 37 toward the linear part 43 in the Z-axis direction is negative, the component of the electric field from the leading end 38 toward the linear part 46 in the Y-axis direction is positive, and the component of the electric field from the leading end 39 toward the linear part 48 in the Y-axis direction is negative. In the third state, the component of the electric field from the leading end 36 toward the linear part 41 in the Z-axis direction is positive, the component of the electric field from the leading end 37 toward the linear part 43 in the Z-axis direction is negative, the component of the electric field from the leading end 38 toward the linear part 46 in the Y-axis direction is positive, and the component of the electric field from the linear part 48 toward the leading end 39 in the Y-axis direction is positive. In the fourth state, the component of the electric field from the leading end 36 toward the linear part 41 in the Z-axis direction is positive, the component of the electric field from the leading end 37 toward the linear part 43 in the Z-axis direction is negative, the component of the electric field from the linear part 46 toward the leading end 38 in the Y-axis direction is negative, and the component of the electric field from the leading end 39 toward the linear part 48 in the Y-axis direction is negative. In this case, when the electromagnetic wave W enters the meta-surface 22 in the first state, the electron P is emitted from the antenna portion α1 according to the positive component in the Z-axis direction of the electric field strength of the electromagnetic wave W, and the emission of electron according to the other component of the electric field strength of the electromagnetic wave W is suppressed. When the electromagnetic wave W enters the meta-surface 22 in the second state, the electron P is emitted from the antenna portion α1 according to the negative component in the Z-axis direction of the electric field strength of the electromagnetic wave W, and the emission of electron according to the other component of the electric field strength of the electromagnetic wave W is suppressed. When the electromagnetic wave W enters the meta-surface 22 in the third state, the electron P is emitted from the antenna portion α2 according to the positive component in the Y-axis direction of the electric field strength of the electromagnetic wave W, and the emission of electron according to the other component of the electric field strength of the electromagnetic wave W is suppressed. When the electromagnetic wave W enters the meta-surface 22 in the fourth state, the electron P is emitted from the antenna portion α2 according to the negative component in the Y-axis direction of the electric field strength of the electromagnetic wave W, and the emission of electron according to the other component of the electric field strength of the electromagnetic wave W is suppressed. Therefore, the measurement for each polarity of each directional component can be achieved more accurately. Furthermore, the detection of the polarization state of the electromagnetic wave W can be achieved more accurately. The same operations and effects can be also achieved in the meta-surface 22A.
For example, in the first state, the electric potential applied to the linear part 41 is lower than the electric potential applied to the antenna portion α1, the electric potential applied to the linear part 43 is higher than the electric potential applied to the antenna portion α1, the electric potential applied to the linear part 46 is lower than the electric potential applied to the antenna portion α2, and the electric potential applied to the linear part 48 is lower than the electric potential applied to the antenna portion α2. In the second state, the electric potential applied to the linear part 41 is higher than the electric potential applied to the antenna portion α1, the electric potential applied to the linear part 43 is lower than the electric potential applied to the antenna portion α1, the electric potential applied to the linear part 46 is lower than the electric potential applied to the antenna portion α2, and the electric potential applied to the linear part 48 is lower than the electric potential applied to the antenna portion α2. In the third state, the electric potential applied to the linear part 41 is lower than the electric potential applied to the antenna portion α1, the electric potential applied to the linear part 43 is lower than the electric potential applied to the antenna portion α1, the electric potential applied to the linear part 46 is lower than the electric potential applied to the antenna portion α2, and the electric potential applied to the linear part 48 is higher than the electric potential applied to the antenna portion α2. In the fourth state, the electric potential applied to the linear part 41 is lower than the electric potential applied to the antenna portion α1, the electric potential applied to the linear part 43 is lower than the electric potential applied to the antenna portion α1, the electric potential applied to the linear part 46 is higher than the electric potential applied to the antenna portion α2, and the electric potential applied to the linear part 48 is lower than the electric potential applied to the antenna portion α2. In this case, an electric potential difference occurs between the leading end 36 and the linear part 41, between the leading end 37 and the linear part 43, between the leading end 38 and the linear part 46, and between the leading end 39 and the linear part 48. Due to this electric potential difference, an electric field is generated as described above. As a result, when the electromagnetic wave W enters the meta-surface 22 in the first state, the electron P is emitted from the antenna portion α1 according to the positive component in the Z-axis direction of the electric field strength of the electromagnetic wave W, and the emission of electron according to the other component of the electric field strength of the electromagnetic wave W is suppressed. When the electromagnetic wave W enters the meta-surface 22 in the second state, the electron P is emitted from the antenna portion α1 according to the negative component in the Z-axis direction of the electric field strength of the electromagnetic wave W, and the emission of electron according to the other component of the electric field strength of the electromagnetic wave W is suppressed. When the electromagnetic wave W enters the meta-surface 22 in the third state, the electron P is emitted from the antenna portion α2 according to the positive component in the Y-axis direction of the electric field strength of the electromagnetic wave W, and the emission of electron according to the other component of the electric field strength of the electromagnetic wave W is suppressed. When the electromagnetic wave W enters the meta-surface 22 in the fourth state, the electron P is emitted from the antenna portion α2 according to the negative component in the Y-axis direction of the electric field strength of the electromagnetic wave W, and the emission of electron according to the other component of the electric field strength of the electromagnetic wave W is suppressed. Therefore, the measurement for each polarity of each directional component can be achieved more accurately. Furthermore, the detection of the polarization state of the electromagnetic wave W can be achieved more accurately. The same operations and effects can be also achieved in the meta-surface 22A.
The photoelectric conversion device 2 is further provided with the housing 10 which is airtightly sealed and has the window unit 11a transmitting the electromagnetic wave W. The electron emitter 20 is disposed within the housing 10. In this case, the amount of emission of the electron P in response to incidence of the electromagnetic wave W can be improved by making the housing 10 vacuum or filling the housing 10 with the gas.
The electromagnetic wave detection device 1 is provided with the photoelectric conversion device 2, the electron collecting unit 50 and the computing unit 75. The electron collecting unit 50 detects the electron P emitted from the electron emitter 20. The computing unit 75 computes the polarization information of the electromagnetic wave W, based on the result of detection of the electron collecting unit 50 in the first state, the result of detection of the electron collecting unit 50 in the second state, the result of detection of the electron collecting unit 50 in the third state, and the result of detection of the electron collecting unit 50 in the fourth state. In this case, the electromagnetic wave detection device 1 is capable of easily detecting the polarization state of the electromagnetic wave W. The electromagnetic wave detection device 1 is not required to be cooled.
Although the embodiments and the modifications of the present invention have been described, the present invention is not necessarily limited to the embodiments and the modifications and various changes can be made without departing from the gist thereof.
For example, the configurations of the photoelectric conversion units 25 and 25A can be appropriately combined. One electron emitter 20 may be provided with a plurality of types of photoelectric conversion units.
The disposition of various linear parts in the patterns 31, 32, 33, 34, and 35, the patterns 31A, 32A, 33A, 34A, 35A, 81A, and 82A, and the patterns 31B, 33B, and 81B is not limited to the configuration of the above-described embodiment. As long as the functional relationship between the bias portion and the antenna portion corresponding to each other is held, the number and disposition of the linear parts can be appropriately changed.
For example, one linear part may be configured to serve as both an antenna portion that emits the electron P in response to incidence of the electromagnetic wave W and a bias portion that generates an electric field. For example, the photoelectric conversion unit of the electron emitter 20 may be configured to include a pair of first and second linear parts facing each other and extending in the same direction, and may be configured so as to be capable of switching between a state in which the first linear part functions as an antenna portion and the second linear part functions as a bias portion and a state in which the first linear part functions as a bias portion and the second linear part functions as an antenna portion. Leading ends of the pair of first and second linear parts are disposed so as to face each other. For example, in the first linear part and the second linear part, switching between the state of functioning as an antenna portion and the state of functioning as a bias portion is performed by controlling electric potentials applied to an electrode electrically connected to each of the linear parts. By switching which of the first and second linear parts facing each other to function as an antenna portion, it is possible to detect the electric field strength of the electromagnetic wave W for each polarity of the component in the extending direction of the pair of linear parts.
The antenna portion α1 and the antenna portion α2 may not be orthogonal to each other. The computing unit 75 may be configured to determine the polarization state, based on the electron P emitted from the antenna portion α1 and the antenna portion α2 which are not orthogonal to each other.
| Number | Date | Country | Kind |
|---|---|---|---|
| 21190608.6 | Aug 2021 | EP | regional |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2022/072099 | 8/5/2022 | WO |
