This disclosure is related to long-wave infrared (LWIR) sensors, particularly microbolometers.
Long-wave infrared (LWIR) cameras detect infrared radiation, and convert the detected infrared radiation into an image that can illustrate the heat emission pattern of a viewed area. Such cameras can be used in a variety of applications, including surveillance, building inspection, safety systems, and other applications in which heat emission patterns may be captured or analyzed.
In particular, transmission of LWIR radiation through the atmosphere has a peak in the 8-12 μm range. By utilizing components which also transmit substantial amounts of LWIR radiation within this range, the efficiency of the LWIR radiation transmission and detection can be increased. Typical camera components, such as ordinary glass, may not be sufficiently transmissive to LWIR radiation to be used in an LWIR camera, requiring the optical elements to be formed from specific LWIR-transmissive materials, such as germanium, chalcogenide glass, or low-oxygen silicon.
The systems, methods and devices of this disclosure each have several innovative aspects, no single one of which is solely responsible for the desirable attributes disclosed herein. One innovative aspect of the subject matter described in this disclosure can be implemented in an apparatus including a glass substrate, an active matrix array formed over the glass substrate, the active matrix array including a plurality of thin-film transistors (TFTs), an array of microbolometer sensors supported by the glass substrate and electrically connected to the active matrix array, each of the microbolometer sensors including a long-wave infrared (LWIR) absorber suspended over the glass substrate, and a thermistor disposed adjacent the LWIR absorber, an LWIR-transmissive layer overlying at least one of the microbolometer sensors, and at least one ancillary CMOS substrate electrically connected to the active matrix array.
In some implementations, the at least one ancillary CMOS substrate can include measurement or control circuitry. In some implementations, the at least one ancillary CMOS substrate is bonded to the glass substrate. In further implementations, the active matrix array and array of microbolometer sensors can be located over a first surface of the glass substrate, and the at least one ancillary CMOS substrate can be bonded to a second surface of the glass substrate opposite the first surface of the glass substrate. In still further implementations, the apparatus can additionally include at least one via extending between the first surface of the glass substrate and the second surface of the glass substrate and forming at least a part of an electrical connection between the ancillary CMOS circuitry and the active matrix array.
In some implementations, both the glass substrate and the at least one ancillary CMOS substrate can be bonded to a carrier substrate. In further implementations, at least a portion of the glass substrate, the carrier substrate, and the at least one ancillary CMOS substrate can be encapsulated by a packaging material without occluding the array of microbolometer sensors.
In some implementations, the active matrix array can include a row address decoder and a column output multiplexer. In further implementations, the apparatus can additionally include a second ancillary CMOS substrate, where the first ancillary CMOS substrate is electrically connected to the row address decoder and includes control circuitry, and the second ancillary CMOS substrate is electrically connected to the column output multiplexer and includes measurement circuitry.
In some implementations, each microbolometer sensor can additionally include an LWIR reflector underlying and spaced apart from the LWIR absorber and the thermistor. In further implementations, the LWIR reflector can include a getter material.
In some implementations, the apparatus can additionally include a window substrate sealed to the glass substrate by a seal to form a hermetically sealed cavity surrounding the array of microbolometer sensors, where the window substrate includes the LWIR-transmissive layer. In at least a first further implementation, the pressure within the hermetically sealed cavity can be less than about 0.1 mbar. In at least a second further implementation, the seal can include a plurality of metal layers bonded to one another. In at least a first still further implementation, two adjacent metal layers in the plurality of metal layers can include the same metal. In at least a second still further implementation, the apparatus can additionally include a passivation layer extending between a portion of the seal and a conductive component within or electrically connected to the active matrix array. In at least a third further implementation, the seal can include an adhesion layer or an electroplating seed layer. In at least a fourth further implementation, the seal can be a low temperature seal including silicon oxide. In at least a fifth further implementation, the window substrate can include a recess in a portion of the window substrate overlying the array of microbolometer sensors. In still further implementations, the recess is located between standoff structures formed on the window substrate.
In some implementations, the LWIR-transmissive layer can include germanium. In some implementations, the apparatus can additionally include at least one LWIR anti-reflection layer located on a surface of the LWIR-transmissive layer overlying the array of microbolometer sensors. In some implementations, at least a portion of the microbolometer sensors can serve as reference pixels. In at least a first further implementation, the apparatus can additionally include an LWIR-opaque material overlying the microbolometer sensors that serve as reference pixels. In at least a first further implementation, the microbolometer sensors that serve as reference pixels can be thermally sunk to the glass substrate.
In some implementations, the apparatus can be an LWIR camera, and the glass substrate, the active matrix array, the array of microbolometer sensors, the LWIR-transmissive layer, and the at least one ancillary CMOS substrate can form at least a portion of a focal plane array within the LWIR camera.
Another innovative aspect of the subject matter described in this disclosure can be implemented in a method of fabricating a microbolometer device, including forming an active matrix array over a glass substrate, where the active matrix array includes a plurality of thin-film transistors (TFTs), forming an array of microbolometer sensors over at least a portion of the active matrix array, where each of the microbolometer sensors include: a long-wave infrared (LWIR) absorber suspended over the glass substrate, and a thermistor disposed adjacent the LWIR absorber, forming at least one hermetically-sealed package encapsulating the array of microbolometer sensors and including an LWIR-transmissive layer overlying at least one of the microbolometer sensors, and electrically connecting the active matrix array to at least one ancillary CMOS substrate including measurement or control circuitry.
In some implementations, forming an active matrix array can additionally include forming a row address decoder and a column output multiplexer, and electrically connecting the active matrix array to at least one ancillary CMOS substrate including measurement or control circuitry can include electrically connecting a first ancillary CMOS substrate including control circuitry to the row address decoder, and electrically connecting a second ancillary CMOS substrate including measurement circuitry to the column output multiplexer.
In some implementations, forming at least one hermetically-sealed package encapsulating the array of microbolometer sensors can include sealing a window substrate including the LWIR-transmissive layer to the glass substrate. In further implementations, sealing the window substrate to the glass substrate can include one of bonding at least two metal layers together using one of a thermocompression process, a plasma bonding process, or a metal diffusion bonding process, or using laser annealed compression bonding, anodic bonding, fusion bonding, a layer of frit glass, or a low-temperature seal including silicon oxide.
In some implementations, forming an array of microbolometer sensors over at least a portion of the active matrix array can include forming a layer of sacrificial material over at least a portion of the active matrix array, forming the LWIR absorbers and thermistors over the layer of sacrificial material, and performing a release etch to remove the layer of sacrificial material. In further implementations, the sacrificial material can include a fluorine-etchable sacrificial material.
Another innovative aspect of the subject matter described in this disclosure can be implemented in an apparatus, including an glass substrate, where the glass substrate includes glass, an active matrix array formed over the glass substrate, the active matrix array including a plurality of thin-film transistors (TFTs), an array of microbolometer sensors supported by the glass substrate and electrically connected to the active matrix array, each of the microbolometer sensors including: a long-wave infrared (LWIR) absorber suspended over the glass substrate, and a thermistor disposed adjacent the LWIR absorber, means for hermetically encapsulating the array of microbolometer sensors, an LWIR-transmissive layer overlying at least one of the microbolometer sensors, and at least one ancillary CMOS substrate electrically connected to the active matrix array.
In some implementations, the encapsulating means can include a window substrate sealed to the glass substrate. In further implementations, a portion of the window substrate overlying the array of microbolometer sensors can serve as the LWIR-transmissive layer. In further implementations, the window substrate can support the LWIR-transmissive layer.
Another innovative aspect of the subject matter described in this disclosure can be implemented in an apparatus, including a glass substrate, an active matrix array formed over the glass substrate, the active matrix array including a plurality of thin-film transistors (TFTs), an array of microbolometer sensors supported by the glass substrate and electrically connected to the active matrix array, each of the microbolometer sensors including a long-wave infrared (LWIR) absorber suspended over the glass substrate, and a thermistor disposed adjacent the LWIR absorber, a plurality of shell structures, each shell structure encapsulating a portion of the array of microbolometer sensors, where at least a portion of the plurality of shell structures include an LWIR-transmissive layer overlying at least one microbolometer sensor.
In some implementations, the apparatus can additionally include at least one ancillary CMOS substrate electrically connected to the active matrix array, where the at least one ancillary CMOS substrate includes measurement or control circuitry. In at least a first further implementation, the at least one ancillary CMOS substrate can be bonded to the glass substrate. In still further implementations, the active matrix array and array of microbolometer sensors can be located over a first surface of the glass substrate, and the at least one ancillary CMOS substrate can be bonded to a second surface of the glass substrate opposite the first surface of the glass substrate. In still further implementations, the apparatus can additionally include at least one via extending between the first surface of the glass substrate and the second surface of the glass substrate and forming at least a part of an electrical connection between the ancillary CMOS circuitry and the active matrix array. In at least a second further implementation, each of the glass substrate and the at least one ancillary CMOS substrate can be bonded to a carrier substrate. In still further implementations, at least a portion of the glass substrate, the carrier substrate, and the at least one ancillary CMOS substrate can be encapsulated by a packaging material without occluding the array of microbolometer sensors. In at least a third further implementation, the active matrix array can include a row address decoder and a column output multiplexer. In still further implementations, the apparatus can additionally include a second ancillary CMOS substrate, where the first ancillary CMOS substrate is electrically connected to the row address decoder and includes control circuitry, and the second ancillary CMOS substrate is electrically connected to the column output multiplexer and includes measurement circuitry.
In some implementations, each of the plurality of shell structures can encapsulate a single microbolometer sensor. In some implementations, each of the plurality of shell structures can include a shell layer having an aperture extending therethrough, and a sealing layer overlying at least the aperture and sealing the aperture. In at least a first further implementation, the aperture can overlie at least a portion of a microbolometer sensor, and the sealing layer can include an LWIR-transmissive material. In at least a first further implementation, the aperture can be laterally offset from any microbolometer sensor within the shell structure, and the sealing layer can include an LWIR-opaque material.
In some implementations, each microbolometer sensor can additionally include an LWIR reflector underlying and spaced apart from the LWIR absorber and the thermistor. In further implementations, the LWIR reflector can include a getter material. In some implementations, at least a portion of the microbolometer sensors can serve as reference pixels. In at least a first further implementation, the apparatus can additionally include an LWIR-opaque material overlying the microbolometer sensors that serve as reference pixels. In at least a second further implementation, the microbolometer sensors that serve as reference pixels can be thermally sunk to the glass substrate.
In some implementations, each shell structure can form a hermetically sealed cavity supported by the glass substrate and encapsulating a portion of the array of microbolometer sensors. In further implementations, the pressure within the hermetically sealed cavity can be less than about 0.1 mbar. In some implementations, the apparatus can be an LWIR camera, and where the glass substrate, the active matrix array, the array of microbolometer sensors, and plurality of shell structures can form a part of a focal plane array within the LWIR camera.
Another innovative aspect of the subject matter described in this disclosure can be implemented in a method of fabricating a microbolometer device, including forming an active matrix array over a glass substrate, where the active matrix array includes a plurality of thin-film transistors (TFTs), forming an array of microbolometer sensors over at least a portion of the active matrix array, where each of the microbolometer sensors include a long-wave infrared (LWIR) absorber suspended over the glass substrate, and a thermistor disposed adjacent the LWIR absorber, forming at least one hermetically-sealed package encapsulating the array of microbolometer sensors and including an LWIR-transmissive layer overlying at least one of the microbolometer sensors, and electrically connecting the active matrix array to at least one ancillary CMOS substrate including measurement or control circuitry.
In some implementations, forming an active matrix array additionally can include forming a row address decoder and a column output multiplexer, and electrically connecting the active matrix array to at least one ancillary CMOS substrate including measurement or control circuitry can include electrically connecting a first ancillary CMOS substrate including control circuitry to the row address decoder, and electrically connecting a second ancillary CMOS substrate including measurement circuitry to the column output multiplexer.
In some implementations, forming a plurality of shell structures can include forming discrete sections of sacrificial material over each of the microbolometer sensors, forming a shell structure over each of the discrete sections of sacrificial material, each shell structure including an aperture extending therethrough, performing a release etch to remove the discrete sections of sacrificial material, and forming a sealing layer over at least the aperture to close the aperture.
In some implementations, the sealing layer can extend over at least a portion of a microbolometer sensor and can include an LWIR-transmissive material. In some implementations, the sealing layer can be laterally offset from any microbolometer sensor within the shell structure and can include an LWIR-opaque material.
Another innovative aspect of the subject matter described in this disclosure can be implemented in an apparatus, including a glass substrate, an active matrix array formed over the glass substrate, the active matrix array including a plurality of thin-film transistors (TFTs), an array of microbolometer sensors supported by the glass substrate and electrically connected to the active matrix array, each of the microbolometer sensors including a long-wave infrared (LWIR) absorber suspended over the glass substrate, and a thermistor disposed adjacent the LWIR absorber, means for hermetically encapsulating discrete portions of the array of microbolometer sensors, and an LWIR-transmissive layer overlying at least one of the microbolometer sensors.
In some implementations, the apparatus can additionally include at least one ancillary CMOS substrate electrically connected to the active matrix array. In some implementations, the encapsulating means can include a plurality of shell structures, each shell structure separately encapsulating only a portion of the array of microbolometer sensors. In at least a first further implementation, each of the plurality of shell structures can encapsulate only a single microbolometer sensor. In at least a second further implementation, a portion of a shell structure can serve as the LWIR-transmissive layer. In some implementations, a shell structure can support the LWIR-transmissive layer.
Details of one or more implementations of the subject matter described in this disclosure are set forth in the accompanying drawings and the description below. Other features, aspects, and advantages will become apparent from the description, the drawings and the claims. Note that the relative dimensions of the following figures may not be drawn to scale.
The following description is directed to certain implementations for the purposes of describing the innovative aspects of this disclosure. However, a person having ordinary skill in the art will readily recognize that the teachings herein can be applied in a multitude of different ways.
The FPA 40 is typically a hermetic package including a supporting substrate, a read-out integrated circuit (ROIC), an overlaid sensor array such as an array of microbolometers or other LWIR-sensitive elements, and an LWIR-transmissive window joined to the substrate to form a part of the hermetic package. In some implementations, the ROIC can consist of a switch array, control circuitry, and one or more measurement circuits. In an implementation in which the FPA is formed on a silicon substrate, all components of the ROIC can be integrally formed on the silicon substrate using CMOS technology.
A typical LWIR camera core such as core 10 of
As noted above, microbolometer arrays are typically formed on silicon substrates. However, by utilizing glass substrates in an LWIR camera module rather than silicon substrates, reductions in both size and cost can be achieved. The thermal conductivity of glass (roughly 1 W/mK) is more than two orders of magnitude less than the thermal conductivity of silicon (roughly 149 W/mK). The increased thermal isolation between adjacent microbolometers formed on a glass substrate allows the overall sensitivity of the microbolometer array to be increased. In some implementations, this enables a reduction of pixel pitch within the array from 17-25 um on silicon substrates to 12 um on glass substrates.
In some implementations, depending on the desired sensitivity and complexity of the circuitry, a TFT active matrix including TFT 120 may include only a portion of the measurement and control circuitry used to control the FPA or other device including the microbolometer pixel 100, while the most sensitive measurement and control circuitry can be formed on a separate CMOS substrate and placed in electrical communication with the TFT active matrix including TFT 120. By forming the pixel 100 and underlying active matrix array on a low cost glass substrate, while forming only measurement and control circuitry on an expensive CMOS substrate, the overall cost of the microbolometer can be reduced. In addition, by forming the pixel 100 and underlying active matrix array on the glass substrate, the thermal isolation of the pixels from the surrounding environment, and hence the sensitivity of the bolometer, may be improved.
The pixel 100 may include a long-wave infrared mirror 130 located on the opposite side of a cavity 132 from an overlying suspended sensor 140. The LWIR mirror 130 may be used to reflect at least a portion of infrared light incident on the mirror 130. In some implementations, the LWIR mirror 130 can be a layer of aluminum (Al) with thicknesses ranging from 50-1000 nm, although other materials and other thicknesses both above and below that range may be used. In some implementations, the LWIR mirror 130 may be the top layer within the TFT 120.
The sensor 140 may be supported over the LWIR mirror 130 by arms 134 in electrical communication with electrodes 122. While the arms 134 may include some conductive material in order to electrically connect the sensor 140 to the electrodes 122, the arms 134 may also have a thin cross section so as to achieve a low thermal conduction in order to thermally isolate the sensor 140 from the remainder of the device. Although schematically depicted as distinct structures overlying the TFT 120, the electrodes 122 may be formed within the TFT active matrix array containing TFT 120. A pixel array may include a plurality of pixels such as pixels 100 disposed across the array, with each pixel 100 connected to one or more TFTs 120 and one or more electrodes 122.
The sensor 140 is a multilayer structure including at least a long-wave infrared absorber 142 that absorbs LWIR radiation passing through the sensor 140, and a thermistor 144 adjacent the LWIR absorber 142. While illustrated as underlying the LWIR absorber 142, the thermistor 144 may in other implementations overlie the LWIR absorber 142. The thermistor 144 can be formed from one or more of a variety of materials, including amorphous silicon (a-Si), vanadium oxide (VOx) or silicon germanium (SiGe), in thicknesses ranging from 10 nm to 1000 nm, although other materials and other thicknesses of materials may also be used. For example, alternate implementations may utilize silicon (Si), germanium (Ge), polysilicon-germanium (poly SiGe), silicon carbide (SiC), SiCON, vanadium oxide (VOx) with or without the inclusion of tungsten (W), barium strontium titanate (BST), or yttrium barium copper oxide (YBaCuO) as the thermistor 144 material. The LWIR absorber 142 may also be formed from one or more of a variety of materials, including but not limited to titanium nitride (TiN), aluminum (Al), or platinum (Pt) in thicknesses ranging from 5 nm to 100 nm, although other materials and other thicknesses of materials may also be used.
In some implementations, the sensor 140 may contain additional components. For example, in the illustrated implementation, the sensor 140 includes a layer of support material 146. In the illustrated implementation, the layer of support material 146 underlies the thermistor 144 and the LWIR absorber 142, although the layer of support material 146 may in other implementations overlie these or other layers, or lay between the materials. In addition to providing additional physical support to the other components of the sensor 140, the layer of support material 146 may also be used to balance residual stresses within the sensor 140 to prevent undesired flexure of the elements after removal of a supporting sacrificial layer as discussed below.
In some implementations, the sensor 140 may include an LWIR anti-reflection layer, although in other implementations, an LWIR anti-reflection layer may be formed separate from the sensor 140 itself but in the path of incident radiation, such as on a surface of an overlying window 150, as will be discussed in greater detail herein. Suitable materials and thicknesses for an LWIR anti-reflection layer include, but are not limited to, titanium oxide (TiO2), tantalum oxide (Ta2O5), and silicon oxide SiO2, in thicknesses ranging from 5 nm to 1000 nm. The LWIR anti-reflection layer may also be a multilayer stack of layers ranging from 50 nm to 1000 nm.
Although the sensor is depicted in the illustrated implementation as including several individual layers, certain of these functions can be performed by a single layer, which may replace two or more of the depicted layers. For example, a single layer of a titanium-aluminum (TiAl) alloy may serve as both a thermistor and an LWIR absorber, and can even serve as a support membrane.
Overlying the sensor 140 is an LWIR window 150 that allows light in the 8-12 μm wavelength range to pass through, such that the light 162 that passes through the LWIR window 150 includes light with wavelengths in the 8-12 μm range. In some implementations, the LWIR window 150 may also filter incident light 160 to prevent some or all of other wavelengths of light from passing through the LWIR window 150, but in other implementations, filtering of other wavelengths may be performed by structures at an earlier point along the optical path of the light 160 incident upon LWIR window 150, such as at lens 30 of an LWIR camera core 10 (see
Portions of incident light 162 may pass through the sensor 140, and can then be reflected by the underlying LWIR mirror 130 back into the sensor 140 to increase the sensitivity of the sensor 140 to incident infrared radiation. In some implementations, as discussed elsewhere herein, one or both surfaces of the LWIR window 150 may be coated with an anti-reflective coating (not shown in
In some implementations, a thermal ground plane (not shown) can be provided close to the sensors 140 to improve uniformity of the sensors 140, and may include a layer of aluminum nitride (AlN), graphene, copper (Cu), diamond-like carbon, or silicon carbide (SiC). If the thermal ground plane is formed from a conductive material, the thermal ground plane may be electrically isolated from the sensors 140 and/or the active matrix array.
The sensor 140 may be suspended within a moderate vacuum having a pressure of less than about 0.1 mBar. In some implementations, the pressure of the vacuum may be as low as or lower than 0.001 mBar. This level of vacuum may be achieved by hermetically sealing the LWIR window 150 to the substrate 110 as discussed in greater detail below. In some implementations, in order to maintain the vacuum after sealing, it may be advantageous to include a getter inside the pixel that removes various gases: those that leak through the seal, and those that diffuse out of the deposited sensor and TFT layers. In one specific implementation, the underlying LWIR mirror 130 may include a thin film getter that not only functions as an IR mirror, but also is capable of gettering gases.
Each pixel 100 includes a sensor 140 such as a microbolometer, and a switch 105 in electrical communication with a switch control line 174 to allow addressing of that pixel 100. LWIR radiation 162 incident upon an active pixel 100 in which the switch 105 is closed will result in a pixel output on the connected output line 176. Additional TFT structures (not shown) including a row address decoder and a column output multiplexer can be formed elsewhere in the TFT layer. For example, such additional TFT structures can be formed at a periphery of the active matrix array.
In some implementations, reference pixels 106 may be provided that are shielded from or otherwise less affected by incident LWIR radiation to provide for temperature correction or calibration, as the thermistors 144 (see
Various implementations of reference pixels may be employed. For example, a pixel may be blocked by a shielding structure 108 that prevents LWIR radiation from reaching a sensor 140 in a reference pixel 106 by absorbing and/or reflecting the LWIR radiation. The shielding structure 108 may be located on a surface of an LWIR window 150 (see
In some implementations, reference pixels 106 may be disposed on the periphery of a pixel array. In other implementations, reference pixels 106 may be disposed throughout the array, such as in a regular pattern, in order to further improve calibration and correction by providing temperature information throughout the array. Differences in the output signals from reference pixels at different locations within the array may be indicative of temperature gradients or hot/cold spots within the array, and localized correction of the output signals of adjacent LWIR pixels can be performed to provide a more accurate image. When the reference pixels 106 are located throughout the array instead of at the periphery, the reference pixels may form areas within the array unresponsive to LWIR radiation, essentially forming “dead” pixels. However, the reference pixels on an image produced by the array may be compensated for by estimating the LWIR incident upon those reference pixels 106 using interpolation from the data measured by adjacent active pixels.
Although the reference pixel 106 in
In one implementation, the ancillary CMOS control circuitry 436 may include digital control and/or driver circuitry, which is configured to receive power and digital control signals from an external input source (not shown). The control CMOS circuitry 436 may power the pixel array, and may address both the drive lines as well as the switch lines within the active matrix TFT array.
The measurement CMOS circuitry 446 may receive outputs from the column output multiplexer 442, and output measurement data to external circuitry or an external processor (output pads and external circuitry or processor are not shown). The measurement CMOS circuitry 446 may include analog signal conditioning circuitry, an analog-to-digital converter (ADC) and data drivers, each of which may operate on the received output signals to generate measurement data to be output. The measurement CMOS circuitry 446 may also receive control and synchronization signals from the control CMOS circuitry 436, whether directly or through the TFT array, and the control CMOS circuitry 436 may also send column select data to the column output multiplexer 442.
In
In
The sacrificial layer 236 may include apertures 238 extending from the top surface of sacrificial layer 236 to an exposed surface of electrode 222 or other conductive surface. In some implementations, the apertures 238 are formed after deposition of the first sacrificial layer 236 by a patterning and etching process. The dimensions and shape of these apertures 238 will determine the dimensions and shape of the support arms which will suspend the sensor. In one implementation, the apertures 238 may include a ramp or angled surface that extends upward from the electrode 222. Such angled apertures may allow the formation of support arms which are longer than the height of the sacrificial layer, as they will extend upward and at an angle to the underlying layers, further increasing the thermal isolation of the supported sensor.
In
Sensor 240 is also formed over the first sacrificial layer 236 by depositing one or more layers over the sacrificial layer and patterning the deposited one or more layers to form sensor 240. In the illustrated implementation, a support layer 246 is deposited over the first sacrificial layer 236, followed by a thermistor 244 and an LWIR absorber 242. In some implementations, the three layers which form the support layer 246, the thermistor 244 and the LWIR absorber 242 are deposited prior to patterning of any of those layers, while in other implementations, at least some of these layers may be patterned before an overlying layer is deposited. In some implementations, a single etch may be used to pattern all three layers, while in other implementations, multiple etches may be used. In some implementations the sensor 240 may be perforated with holes that enable the first sacrificial layer to be readily removed, particularly when the first sacrificial layer has a very high aspect ratio and is much larger in one or more dimensions than in other dimensions.
In some implementations, at least some of the layers which form sensor 240 can also be used to form the support arms 234. In other implementations, support arms 234 can be formed and patterned prior to deposition of the layers that form sensor 240. Although the support arms and the sensor 240 appear to encapsulate a portion of the sacrificial layer 236, the support arms 234 may be relatively narrow in the plane out of the picture. Because of the dimensions of the support arms 234, a substantial amount of the first sacrificial layer 236 underlying the sensor 240 remains connected to adjacent portions after the formation of the support arms 234 and overlying sensor layers 240. The contiguous first sacrificial layer 236 facilitates removal of the first sacrificial layer 236 in a subsequent step, including the portions between support arms 234.
The resultant structure after the steps of
In some implementations, the second sacrificial layer 256 may be an oxygen-etchable polymer, or may be a fluorine-etchable material, such as Mo, W, or a-Si. In some implementations, the second sacrificial layer 256 includes the same material as the first sacrificial layer 236, or a material which is etchable by the same etch chemistry as the material of the first sacrificial layer, so that both sacrificial layers 236 and 256 can be etched by a single release etch in a subsequent step. In some implementations, the second sacrificial layer 256 can be between 5 and 20 um, and may be thicker than the first sacrificial layer 236. Because the second sacrificial layer 256 will define a distance between the sensor 240 and an overlying protective shell, the additional spacing between the sensor 240 and the shell due to the thicker second sacrificial layer 256 will protect against mechanical interference with or damage to the sensor 240.
In
In some implementations, the shell layer 254 may have a substantially constant thickness, and be conformally deposited over the underlying sacrificial layers 236 and 256, while in other implementations, portions of the shell layer 254 may be thicker than other portions. Although the shell of sacrificial layers 236 and 256 is illustrated as having substantially vertical sides, these sacrificial layers 236 and 256 may in other implementations have a generally frustroconical shape or otherwise have tapered sidewalls, in order to facilitate deposition of the shell layer 254 over the sacrificial layers 236 and 256.
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The deposition of the sealing layer 258 can be done under vacuum or in a low vacuum environment to seal the sensor, so as to achieve a residual pressure after sealing of less than about 0.1 mBar, although in other implementations the residual pressure may be as low as or lower than 0.001 mBar. Alternatively, the sealing may be done at somewhat higher pressures using an ambient gas that has a small molecular cross section such as hydrogen or helium, which in some particular implementations can then be removed from the cavity 232 in a low temperature anneal during which the gas diffuses through and out of the shell layer. Depending on the material and thickness of the material of the shell layer 254, the sealing layer 258 may in some implementations be deposited over the entire shell layer 254 to provide a hermetic seal when the shell layer 254 alone does not provide a desired level of hermeticity.
In the illustrated implementation, the aperture 255 overlies a portion of the sensor 240, requiring that the sealing layer 258 used to seal the aperture 255 be formed from an LWIR-transmissive material. In some implementations, the materials listed above as suitable materials for forming the shell layer may also be utilized as suitable materials for forming an LWIR-transmissive sealing layer 258, although other materials may also be used. In some implementations, the sealing layer 258 may be thinner than the shell layer 254, and may have a thickness between about 10 and 1000 nm, although other thicknesses, including thicknesses similar to that of the shell layer 254 may be used in other implementations. In some implementations, a thin sealing layer can be formed using atomic layer deposition (ALD). In some implementations, the sealing layer 258 can include multiple layers, one or more of which can be formed by atomic layer deposition (ALD). These layers can be formed from the same or from different materials so long as the portion overlying the sensor 240 is sufficiently transmissive to LWIR light.
The pixel 200 may include additional components not depicted in
The use of a material which is not transmissive to LWIR in the fabrication process may facilitate fabrication of reference pixels, as the pixel 270 can easily be modified to be a reference pixel by extending the LWIR-opaque sealing material 278 to overlie the sensor 240 as well.
The method 500 then moves to a block 510 in which a shell layer is formed over the sacrificial material. As discussed above, at least a portion of the shell layer overlying the microbolometer can include an LWIR-transmissive material.
The method 500 then moves to a block 515 in which an aperture is formed in the shell layer, exposing at least a portion of the sacrificial material. A release etch is then performed to remove the sacrificial layer and release the microbolometer. In some implementations, the aperture is formed over at least a portion of the microbolometer sensor, while in other implementations, the aperture is laterally offset from the microbolometer sensor.
The method 500 then moves to a block 520 where a sealing layer is formed over at least the aperture in the shell layer. In implementations in which the aperture overlies a portion of the underlying sensor, the sealing layer must be substantially LWIR-transmissive to avoid blocking LWIR from reaching the sensor, unless the sensor is intended to form part of a reference pixel. In implementations in which the aperture is laterally offset from the underlying sensor so that a sealing layer can seal the aperture without overlying a portion of the sensor, LWIR-opaque materials can also be used as part of the sealing layer.
In further implementations, additional steps not specifically depicted in
In other implementations, wafer-level packaging may be utilized instead of the pixel-level packaging discussed above. While wafer-level packaging may use a greater amount of LWIR-transmissive material than the pixel-level packaging process discussed above, a wafer-level packaging process such as that described below may nevertheless be simpler and more cost-effective than other microbolometer packaging processes. In one implementation, a glass substrate comprising one or more pixel arrays is provided, and sealed to a facing window substrate to form individual packages sealing each of the pixel arrays. The glass substrate and facing window substrate may then be parted to separate the individual packages, such as through a scribe and break process. The parting may be a multi-step process which enables testing of the individual packages on the wafer.
In addition, in the illustrated implementation, a passivation layer 328 of a dielectric material has been formed over the array of pixels 300. As discussed in greater detail below, the deposition of this passivation layer 328 facilitates the deposition of subsequent layers such as through an electroplating process, and allows the use of conductive seal layers without shorting of electrical components extending under the conductive seal. In other implementations, however, the passivation layer 328 may not be formed. Although depicted for convenience as extending over the upper and outer surfaces of the components of pixel 300, the passivation layer may be patterned to localize it exclusively to surfaces that are required for sealing. However, it is also possible that the layer could be further extended, for example, by depositing the passivation layer using ALD to cover inner surfaces of the pixel 300 not covered by sacrificial material. Routing electrodes 329, which are discussed above with respect to electrodes 322, may in some implementations be a part of active matrix array 320 and extend beyond the edge of the passivation layer to allow electrical connections with external electrical elements, as discussed in greater detail below.
In
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In the illustrated implementation, the window substrate 350 includes thicker sections 351 surrounding recesses 352 which provide spacing for the underlying array of pixels 300. Other portions of the window substrate 350 not overlying an array of pixels 300 may also be made thinner than the thicker sections 351, so as to facilitate a subsequent parting process, examples of which include sawing, dicing, scribing and breaking, laser ablating, and etching processes. A complementary seed layer 370a substantially identical in shape to that of the seed layer 370b is also formed on a facing surface of the window substrate 350, such as on the thicker portions 351.
In some implementations, the recesses 352 may be formed in a thick window substrate 350 which in some particular implementations was originally a substantially planar substrate with a thickness at least that of the thicker sections 351. In some implementations, the recesses 352 may be between 5 and 50 um deep. In other implementations, the thicker sections 351 may include additional material that was built up on the surface of the substrate 350 to form thicker standoff sections. In still other implementations, if the seal material is sufficiently thick to provide a desired amount of spacing between the interior surface of the window substrate 350, a planar window substrate may be used. In addition, by forming standoffs or using a planar window substrate 350 rather than etching recesses 352 into the window substrate 350, the use of an anti-reflective coating (not shown) on both surfaces of the window substrate 350 overlying the pixels 300 may be facilitated, although anti-reflective coatings may also be formed on patterned substrates.
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In some implementations, the metallurgies are selected to allow bonding at temperatures less than 350° C. to prevent damage to the sensor or active matrix array, but in some implementations higher bonding temperatures may also be used. The allowable bonding temperature range and duration for MEMS sensors such as microbolometers and an associated active matrix array will be performance specific and highly dependent on a variety of factors, including the particular materials used. In some implementations, the allowable temperature range and duration for annealing the TFT circuitry may be a temperature of roughly 300° C. for less than about 30 minutes, although higher temperatures may be permissible for shorter durations, and longer durations may be permissible at lower temperatures. Generally, however, it may be preferable to minimize the temperature and duration of bonding processes.
Possible eutectic metallurgies include gold/tin (Au/Sn), which has a bonding temperature of roughly 280° C.; copper/tin (Cu/Sn), which has a bonding temperature of roughly 231° C.; and gold/indium (Au/In), which has a bonding temperature of roughly 156° C. Possible eutectic metallurgies at higher bonding temperatures include gold/silicon (Au/Si), which has a bonding temperature of roughly 363° C.; and gold/germanium (Au/Ge), which has a bonding temperature of roughly 361° C. In some implementations in which the components are less sensitive to higher temperatures, aluminum/germanium (Al/Ge) eutectic bonding may be used, which has a bonding temperature of roughly 419° C. As noted above, a seed layer or adhesion layer may also be used, which may include titanium, tungsten, or titanium-tungsten alloy. Layers may also be chosen to inhibit oxidation. For example, when tin is used, a gold coating having a thickness of roughly 800 Angstroms or thicker may be used to inhibit oxidation of the tin.
In some implementations, the metal layers 372a and 372b may include multiple metal layers arranged in the following order: a copper (Cu) layer adjacent the seed layer 370a or 370b, a tin (Sn) layer, and a gold (Au) layer. In other implementations, an adhesion layer such as a layer including titanium (Ti), chromium (Cr), or a titanium-tungsten (TiW) alloy may be included adjacent the Cu layer, or may otherwise form a part of metal layers 372a and 372b closest to their respective supporting substrate to improve adhesion between the metal layers 372a and 372b and an adjacent supporting layer. In some implementations, a layer of nickel (Ni) can be used in place of the copper layer, and/or a layer of palladium (Pd) can be used in place of the gold layer. In some implementations, layer of tin can be omitted. In other implementations, fewer layers and/or layers of different metals or metal compositions not explicitly mentioned may also be used.
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As discussed above, a variety of other methods may be used to form seal 374. Plasma treatment can be used to activate bonding surfaces and lower their bonding temperatures to temperatures as low as 150° C., and can be used in conjunction with the thermocompression bonding as discussed above or in another process to greatly increase the possible bonding materials within the allowable temperature range. In some implementations, metal diffusion can be used, by plating layers of like metals on facing substrates and fusing those layers together. Gold will fuse to gold at temperatures between 300 and 400° C., copper will fuse to copper at temperatures between 380 and 450° C., and aluminum will fuse to aluminum at temperatures between 375 and 425° C. Other alternatives include laser annealed compression bonding, anodic bonding, fusion or direct bonding, or the use of lead-based or lead-free frit glass. For example, some commercially available glass bonding materials have low melting temperatures (such as VANEETECT™, sold by Hitachi, Ltd., which can have a melting temperature of about 300° C. or less) and can be melted for adhesion to glass substrates at temperatures exceeding their melting temperature or by localized laser heating. In other implementations, certain solder materials will bond at temps between 150 and 250° C.
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The process 600 then moves to a block 610 where at least one layer of seal material is formed on at least one of the array substrate or a facing surface of the window substrate. In some implementations, in particular those that utilize a conductive seal layer, a passivation layer may be deposited over the array of microbolometers prior to deposition of a seal layer on the array substrate. In some implementations, seal layers may be formed on both the array substrate and the window substrate. As discussed previously, in particular implementations, the seal layers may include materials selected to provide specific metallurgies that allow bonding of the seal layers to one another at temperatures below a threshold temperature.
The process 600 then moves to a block 615 where the array substrate is sealed to the window substrate to form a package encapsulating the microbolometer array. In some implementations, the sealing process may include thermocompression bonding, although the other bonding techniques discussed herein may also be used.
The process 600 moves to a block 620 where both the array substrate and at least one CMOS substrate including ancillary control and/or measurement circuitry are bonded to a carrier substrate such as a lead frame. The CMOS substrate is then placed in electrical communication with the microbolometer array, and may be placed in connection with external circuitry to serve as an input or output component.
In further implementations, additional steps not specifically depicted in
Even if not specifically noted, the materials and thicknesses described herein are exemplary, and are not intended to be limiting lists or ranges unless specifically noted otherwise. Other suitable materials and/or thicknesses of materials may also be used for each of the structures described herein.
As used herein, a phrase referring to “at least one of” a list of items refers to any combination of those items, including single members. As an example, “at least one of: a, b, or c” is intended to cover: a, b, c, a-b, a-c, b-c, and a-b-c.
The various illustrative logics, logical blocks, modules, circuits and algorithm steps described in connection with the implementations disclosed herein may be implemented as electronic hardware, computer software, or combinations of both. The interchangeability of hardware and software has been described generally, in terms of functionality, and illustrated in the various illustrative components, blocks, modules, circuits and steps described above. Whether such functionality is implemented in hardware or software depends upon the particular application and design constraints imposed on the overall system.
The hardware and data processing apparatus used to implement the various illustrative logics, logical blocks, modules and circuits described in connection with the aspects disclosed herein may be implemented or performed with a general purpose single- or multi-chip processor, a digital signal processor (DSP), an application specific integrated circuit (ASIC), a field programmable gate array (FPGA) or other programmable logic device, discrete gate or transistor logic, discrete hardware components, or any combination thereof designed to perform the functions described herein. A general purpose processor may be a microprocessor, or, any conventional processor, controller, microcontroller, or state machine. A processor also may be implemented as a combination of computing devices, such as a combination of a DSP and a microprocessor, a plurality of microprocessors, one or more microprocessors in conjunction with a DSP core, or any other such configuration. In some implementations, particular steps and methods may be performed by circuitry that is specific to a given function.
In one or more aspects, the functions described may be implemented in hardware, digital electronic circuitry, computer software, firmware, including the structures disclosed in this specification and their structural equivalents thereof, or in any combination thereof. Implementations of the subject matter described in this specification also can be implemented as one or more computer programs, i.e., one or more modules of computer program instructions, encoded on a computer storage media for execution by, or to control the operation of, data processing apparatus.
If implemented in software, the functions may be stored on or transmitted over as one or more instructions or code on a computer-readable medium. The steps of a method or algorithm disclosed herein may be implemented in a processor-executable software module which may reside on a computer-readable medium. Computer-readable media includes both computer storage media and communication media including any medium that can be enabled to transfer a computer program from one place to another. A storage media may be any available media that may be accessed by a computer. By way of example, and not limitation, such computer-readable media may include RAM, ROM, EEPROM, CD-ROM or other optical disk storage, magnetic disk storage or other magnetic storage devices, or any other medium that may be used to store desired program code in the form of instructions or data structures and that may be accessed by a computer. Also, any connection can be properly termed a computer-readable medium. Disk and disc, as used herein, includes compact disc (CD), laser disc, optical disc, digital versatile disc (DVD), floppy disk, and Blu-ray disc where disks usually reproduce data magnetically, while discs reproduce data optically with lasers. Combinations of the above also may be included within the scope of computer-readable media. Additionally, the operations of a method or algorithm may reside as one or any combination or set of codes and instructions on a machine readable medium and computer-readable medium, which may be incorporated into a computer program product.
Various modifications to the implementations described in this disclosure may be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other implementations without departing from the spirit or scope of this disclosure. Thus, the claims are not intended to be limited to the implementations shown herein, but are to be accorded the widest scope consistent with this disclosure, the principles and the novel features disclosed herein. Additionally, a person having ordinary skill in the art will readily appreciate, the terms “upper” and “lower” are sometimes used for ease of describing the figures, and indicate relative positions corresponding to the orientation of the figure on a properly oriented page, and may not reflect the proper orientation of, e.g., a microbolometer or sensor element as implemented.
Certain features that are described in this specification in the context of separate implementations also can be implemented in combination in a single implementation. Conversely, various features that are described in the context of a single implementation also can be implemented in multiple implementations separately or in any suitable subcombination. Moreover, although features may be described above as acting in certain combinations and even initially claimed as such, one or more features from a claimed combination can in some cases be excised from the combination, and the claimed combination may be directed to a subcombination or variation of a subcombination.
Similarly, while operations are depicted in the drawings in a particular order, a person having ordinary skill in the art will readily recognize that such operations need not be performed in the particular order shown or in sequential order, or that all illustrated operations be performed, to achieve desirable results. Further, the drawings may schematically depict one more example processes in the form of a flow diagram. However, other operations that are not depicted can be incorporated in the example processes that are schematically illustrated. For example, one or more additional operations can be performed before, after, simultaneously, or between any of the illustrated operations. In certain circumstances, multitasking and parallel processing may be advantageous. Moreover, the separation of various system components in the implementations described above should not be understood as requiring such separation in all implementations, and it should be understood that the described program components and systems can generally be integrated together in a single software product or packaged into multiple software products. Additionally, other implementations are within the scope of the following claims. In some cases, the actions recited in the claims can be performed in a different order and still achieve desirable results.