A photodetector can be a monolithic semiconductor structure or a heterostructure consisting of a photocathode and an electron sensor. The electron sensor in the heterostructure photodetector can be an electron-bombarded charge coupled device (EBCCD) or a micro-channel plate (MCP). The photocathode and the electron sensor generally are mutually facing planar devices separated by a vacuum gap across which a large (e.g., 10 kV) electric field is imposed. As photons from a field of view strike the photocathode, electrons are emitted from the surface of the photocathode facing the electron sensor. The emitted electrons are accelerated across the vacuum gap and strike the electron sensor. The electron sensor amplifies the electron current. In the case of the EBCCD, amplification of the electron current is obtained by exploiting the quantum yield of the semiconductor material of the EBCCD. In the case of the MCP, amplification is obtained by providing the interior surfaces of the glass tubes constituting the MCP with a high electron yield surface. Each incoming electron ricochets on a tube interior surface many times, producing as many as 300 additional electrons for each incoming electron.
The performance of the photodetector is limited by the efficiency with which the photocathode emits electrons in response to incoming photons. The photocathode is generally a planar semiconductor crystal. Each incident photon creates a hole-electron pair in the semiconductor crystal by elevating an electron from the valence band to the conduction band, leaving a hole in the valence band. Generally, a semiconductor material having a bandgap energy corresponding to the infrared region (such as GaAs) does not readily emit electrons from its surface when struck by photons, due to an energy barrier that arises at the crystal surface of the semiconductor. In order for surface emission to occur, the electron must overcome both the work function of the surface and the band gap energy of the semiconductor. Conventionally, this problem is overcome by “activating” the surface of the photocathode in such a manner that this energy barrier is overcome. In the case of a UV or IR photodetector, the photocathode can be a group III semiconductor or group III-V compound semiconductor, and the “activation” consists of depositing a thin Cesium (Cs) coating on the crystal surface. The Fermi levels in the Cs and semiconductor layers equilibrate at the interface between the layers, forcing the valence and conduction band structures in the semiconductor layer to “bend” so much that the conduction band at the surface is below the Fermi level and the bulk conduction band bottom lies above the vacuum level at the surface. This condition is favorable for electron emission from the photocathode surface because electrons excited in the bulk can diffuse toward the surface where they can tunnel or be ballistically emitted from the crystal into the vacuum.
The problem is that the Cs coating step can only be performed in a vacuum, because Cs is highly reactive with oxygen and therefore unstable in oxygen containing environments. The surface activation of the photocathode is therefore extremely difficult and expensive to perform, and the “cesiated” device is neither robust nor permanent. It is unstable and not long lasting, being subject to attack when exposed even slightly to oxygen atoms or molecules. On the other hand, Cesium coating of the GaAs surface provides highly desirable photocathode attributes, specifically (a) a high yield of photoelectrons when under illumination (because it has a short photon absorption length for efficient photon absorption, a long electron diffusion length to minimize photoelectron losses, and a small or negative electron affinity), and (b) high conductivity to avoid charging due to electron loss by photoemission. It has seemed that such desirable attributes could only be realized through the expensive and impermanent Cesium coating step. The result is that the photocathode is chemically unstable. What is needed, therefore, is another way of activating the photocathode that realizes all of the foregoing desirable attributes (high yield and high conductivity) while at the same time providing a structure that is highly stable and robust both chemically and physically (unlike cesiated GaAs structures).
In addition, it would be desirable to have a material system that is activated for photoelectron emission as mentioned above in which the photon absorption spectrum can be independently adjusted without compromising or sacrificing any of the foregoing desired attributes. In particular, for some space applications it is important that the sensor be blind to visible light (e.g., from the sun), and therefore it is useful to be able to set the photon absorption spectrum of the detector to exclude certain wavelength regions while including desired ones.
A photocathode, for generating electrons in response to incident photons in a photodetector, includes a base layer having a first lattice structure and an active layer having a second lattice structure and epitaxially formed on the base layer, the first and second lattice structures being sufficiently different to create a strain in the active layer with a corresponding piezoelectrically induced polarization field in the active layer, the active layer having a band gap energy corresponding to a desired photon energy.
In one implementation, the base and active layers are each formed of p-type AlGaN, and the aluminum mole fraction in the base layer exceeds the aluminum mole fraction in the active layer by an amount sufficient to create the strain. In this implementation, the aluminum mole fraction y of said active layer fixes the band gap energy and corresponding spectral cut-off frequency of said photocathode, and the aluminum mole fraction x of said base layer is selected to provide the requisite difference between the mole fractions.
We have discovered a class of highly efficient photocathodes that do not require deposition an activating metal such as Cesium, and are impervious to exposure to atmosphere and may therefore be manufactured in a relatively efficient and inexpensive manner. Specifically, we found that certain semiconductor crystals such as nitrides of Group III elements have particularly favorable piezo-electric behavior that enables surface activation of such a crystal for purposes of photoelectron surface emission. Such piezoelectric activation is accomplished by inducing piezo-electric strain in the crystal surface from which photoelectrons are to be emitted. The strain is induced by epitaxially growing a p-doped thin Group III-nitride layer on a base p-doped Group III-nitride layer (e.g., by molecular beam epitaxial deposition), but providing sufficiently different lattice constants in the two layers to generate the desired crystal strain in the thin layer. The difference in lattice constants is obtained and controlled by the difference in mole fraction of a second Group III element in the two Group III-nitride layers. The piezoelectric effect from the lattice strain induces high polarization fields near the surface. This piezoelectric polarization, in conjunction with any spontaneous polarization, can lead to a 2-dimensional electron gas at the surface, producing the desired conditions for electron emission from the surface. (Spontaneous polarization is the polarization field in the crystal when it is not strained and at some nominal temperature).
Specifically, and as one working example of the invention, the two layers can be formed of the ternary system of aluminum gallium nitride (AlGaN). In this example, the mole fraction of Al is different in the respective layers, and can even be zero in one of them. The resulting strain in the thin deposited epitaxial crystal layer contributes to the net polarization fields in the crystal that are compensated by a redistribution of electrons in the surface layer to form the dense 2-dimensional electron gas. The resulting bending of the crystalline band structure drives the conduction band at the crystal surface below the Fermi level and the vacuum level at the surface below the bottom of the bulk conduction band. This condition is sufficient for photoelectron surface emission.
The 2-dimensional electron gas at the photocathode surface can be controlled by controlling the differential aluminum content in the adjacent layers in the AlGaN ternary system. Photocathode performance parameters such as photon absorption efficiency are controlled by controlling the density of the p-type impurities in each of the two layers. We have discovered a highly advantageous feature in the AlGaN ternary system, namely that the Aluminum content can be varied to choose the band gap energy without significantly affecting the photon absorption efficiency, over a very large range of Aluminum content, corresponding to a band gap energy range of 3.4 eV to 6.2 eV. Thus, separate independent control over different performance parameters (absorption efficiency vs. band gap energy) of the AlGaN photocathode is attained by varying the Aluminum content and by varying the p-type dopant concentration.
A significant advantage of the AlGaN ternary system is that it is very stable chemically and robust physically, so that the piezo-electric strain-activated AlGaN photocathode is relatively permanent and fairly immune to attack from the exposure to atmosphere, even at elevated temperatures. This feature permits thermal degassing of atmosphere-exposed Group III-nitride photocathode materials, a significant advantage.
An even greater advantage of the AlGaN ternary system is its strong piezoelectric constants (which are an order of magnitude greater than GaAs crystals). Piezoelectricity in AlGaN is a non-isotropic phenomenon characterized by a tensor relating strain in 3-dimensional space to corresponding polarization vector components. The preferred epitaxial growth direction is along the piezoelectrically active axis of the crystal. In AlGaN, a relatively small amount of lattice strain produces a large change in polarization which can lead to the formation of a dense 2-dimensional electron gas at the surface of the strained layer (which may be referred to as a piezo-induced surface charge). For example, a 10% change in aluminum content in one of the two AlGaN layers (relative to the other layer) can double the piezo-induced surface charge. Determination of the band gap energy is still independent of the surface charge. The bandgap is set by the selection of the aluminum content in the active AlGaN layer, while the mismatch in aluminum content of the two layers is selected to achieve a particular level of strain in the thin layer, independently determining the amount of surface charge. In addition, photon absorption is controlled independently by the p-type doping level of the AlGaN crystal.
The invention is useful in a heterostructure photodetector that includes a photocathode and an electron sensor such as an MCP or EBCCD separated by a vacuum from the photocathode. The invention is also applicable to a monolithic semiconductor photodetector.
Referring to
The photocathode 10 consists of a base layer 24 that includes the photon-illuminated surface 10a. The base layer is a semiconductor crystal. An active layer 26 epitaxially grown on the base layer 24 includes the electron-emitting surface 10b and has a band gap energy corresponding to the desired spectral response. A band gap structure favorable for surface emission of electrons and a large surface electron charge at the electron-emitting surface 10b is attained by piezo-electrically induced fields in the active layer. These fields are established by a designed mismatch between the lattice constants of the two layers 24, 26.
In an exemplary embodiment, each of the two layers is a p-type Group III-nitride semiconductor, and the fractional content of a selected Group III species is different in the two layers 24, 26. As one example, each of the two layers is formed of the p-doped AlGaN ternary system, in which the aluminum content is different in each of the two layers 24, 26. Thus, in an exemplary embodiment, the base layer 24 is AlxGa1-xN while the active layer 26 is AlyGa1-yN. In the case of the active layer 26, the aluminum mole fraction y is selected to provide the desired band gap energy and corresponding spectral cut-off frequency. In the case of the base layer 24, the aluminum mole fraction x is selected to provide the desired difference in aluminum content between the two layers 24, 26 to produce the desired lattice strain for attaining the corresponding band “bending” and electron surface charge (to enable electron emission from the photocathode emission surface 10b). The key to this latter feature is the difference between the aluminum mole fractions x and y of the two layers.
Generally, the aluminum content of the base layer 24 exceeds that of the active layer 26, so that x>y. The active layer aluminum mole fraction y may be zero in some implementations, so that the active layer 26 is GaN in such cases.
As illustrated in
In the implementation of
In the implementation of
The spacing between adjacent tubular holes 42 determines the resolution of the detected image.
The semiconductor band structure of the photocathode 10 of
From the foregoing description of
The embodiments of
The foregoing description mainly has concerned photodetectors of the type having a discrete photocathode and an electron sensor separated from the photocathode by a vacuum gap. However, the invention can be employed in a monolithic photodetector in which the photocathode and the electron sensor are not separate. For example,
While the invention has been described in detail with reference embodiments employing crystalline materials, other embodiments may be made using polycrystalline materials. While the invention has been in detail with reference to embodiments employing elements described as planar device, the surface finish in various embodiments may be very smooth or textured or rough.
While the invention has been described in detail by specific reference to preferred embodiments, it is understood that variations and modifications thereof may be made without departing from the true spirit and scope of the invention.
This invention described herein was made in the performance of work under a NASA contract, and is subject to the provisions of Public Law 96-517 (35 U.S.C. § 202) in which the Contractor has elected not to retain title.
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