WO1988004037A1 - Integrated detector dewar cryoengine - Google Patents

Integrated detector dewar cryoengine Download PDF

Info

Publication number
WO1988004037A1
WO1988004037A1 PCT/US1987/002572 US8702572W WO8804037A1 WO 1988004037 A1 WO1988004037 A1 WO 1988004037A1 US 8702572 W US8702572 W US 8702572W WO 8804037 A1 WO8804037 A1 WO 8804037A1
Authority
WO
WIPO (PCT)
Prior art keywords
detector
expander
thermal energy
removing thermal
detector means
Prior art date
Application number
PCT/US1987/002572
Other languages
French (fr)
Inventor
Fred J. Neitzel
Leonard E. Peck, Jr.
Richard M. Rall
Original Assignee
Santa Barbara Research Center
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Santa Barbara Research Center filed Critical Santa Barbara Research Center
Priority to DE3789380T priority Critical patent/DE3789380T2/en
Priority to JP62506868A priority patent/JPH0695046B2/en
Publication of WO1988004037A1 publication Critical patent/WO1988004037A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
    • F25D19/00—Arrangement or mounting of refrigeration units with respect to devices or objects to be refrigerated, e.g. infrared detectors
    • F25D19/006—Thermal coupling structure or interface
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
    • G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
    • G01J5/02—Constructional details
    • G01J5/06—Arrangements for eliminating effects of disturbing radiation; Arrangements for compensating changes in sensitivity
    • G01J5/061—Arrangements for eliminating effects of disturbing radiation; Arrangements for compensating changes in sensitivity by controlling the temperature of the apparatus or parts thereof, e.g. using cooling means or thermostats
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
    • G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
    • G01J5/02—Constructional details
    • G01J5/06—Arrangements for eliminating effects of disturbing radiation; Arrangements for compensating changes in sensitivity
    • G01J2005/065—Arrangements for eliminating effects of disturbing radiation; Arrangements for compensating changes in sensitivity by shielding

Definitions

  • This invention relates to the field of infrared sensing, and more particularly to an integrated detector dewar cryoengine.
  • Infrared detectors are often used in conjunction with missiles and night vision systems to sense the presence of electromagnetic radiation having a wavelength of 1-15 urn. Because they are often most sensitive when operating at approximately 77oK, infrared detectors such as those fabricated from mercury-cadmium-telluride often require a cryoengine assembly to produce and maintain the required operating temperature. Such cryoengine assemblies are typically used in conjunction with an evacuated dewar in which the infrared detector is placed. The dewar is evacuated to remove thermally conductive gases which would otherwise occupy the region surrounding the detector.
  • the dewar is cooled by placing an indented region ("coldwell") of the dewar in contact with an expansion chamber ("expander") of the cryoengine assembly which is supplied with a cooling fluid such as helium.
  • the coldwell and the expander are separated by a gap to allow for variation in the dimensional characteristics of the dewar and expander, as well as to accommodate for differences in their thermal expansion characteristics.
  • the cryoengine assembly often includes a compressor which delivers the fluid to the expander through a transfer line.
  • the temperature of the expander is related to the amount of fluid delivered by the compressor, the temperature of the detector may be controlled by varying the compressor speed. While the infrared detector assemblies described above were able to produce and irmintain the temperature levels required for sensitive operation of the mercury-cadmi um-telluride detectors, they often had several disadvantages in terms of thermal conduction between the expander and the environment. Because the dewar and expander are structurally independent, the gap between the expander and the dewar acted as an insulator to prevent optimal conduction between the expander and the detector.
  • the cross-sectional area through which cold loss occurred not only included the cross-sectional area of expander, but also included the walls of the dewar which were adjacent to the expander. These two features necessarily meant that the capacity of the cryoengine had to be somewhat larger than would otherwise be required.
  • An apparatus for detecting electromagnetic radiation comprises a detector for detecting electromagnetic radiation.
  • the apparatus also comprises an expander end cap for removing thermal energy frcm said detector.
  • the device for removing thermal energy frcm said detector mechanically communicates with the detector.
  • FIG. 1 is a cross-sectional view of the integrated detector dewar cryoengine by the present invention
  • FIG. 2 is an exploded perspective view of the integrated detector cryoengine shown in FIG. 1.
  • the integrated detector dewar cryoengine 10 includes an infrared detector 12 for receiving infrared radiation and generating responsive electrical signals. While the detector 12 may be made from a layer of mercury-cadmium-telluride on a sapphire substrate material, other suitable materials such as CdTe and CdSe may also be used.
  • the detector 12 is secured on a detector platform 14 by a thermally conductive adhesive, which rpermits thermal energy to flow from the detector 12. While the detector platform 14 may be fabricated from beryllium, other suitable materials may be used.
  • the integrated detector dewar cryoengine 10 further comprises an expander assembly 16 (see FIG. 2).
  • the expander assembly 16 includes an expander end cap 18 which mechanically communicates with the detector platform 14 so that thermal energy can flow from the detector platform 14 to the expander end cap 18.
  • the detector platform 14 is disposed between two of four castellations located on the expander end cap 18 and is secured to the expander end cap 18 by means of a thermally conductive adhesive.
  • the expander end cap 18 is disc shaped so as to have a low thermal mass and a high thermal conductivity.
  • the expander end cap 18 is preferably fabricated from beryllium so as to provide a relatively high degree of thermal conductivity, though it is to be understood that other suitable materials may be used.
  • the expander assembly 16 also includes an expander tube 20 which is brazed to the expander end cap 18.
  • the expander tube 20 houses the refrigeration mechanism for cooling the detector 12 and receives cooling fluid such as helium from a compressor (not shown). By expansion of the fluid inside the expander tube 20, thermal energy is drawn frcm the expander end cap 18 thereby cooling the detector 12.
  • the expander tube 20 is preferably fabricated frcm Inconel so as to have low tiiermal conductivity while being sufficiently rigid to minimize detector movement during operation.
  • an expander housing 22 is provided to support the expander tube 20.
  • the expander housing 22 is brazed to the expander tube 20 and is connected to the cryoengine compressor (not shown).
  • the expander assembly 16 also includes a cable support 24 which is used to support the flex cables described below.
  • thermal sensors 26 are located adjacent to the detector 12 on the flex cables described below. The outputs from the thermal sensors 26 are used to control the compressor speed which in turn controls the temperature of the expander assembly 16. Each of the thermal sensors 26 may be a 2N2222 switching diode, though it is to be understood that other suitable temperature sensors which are sensitive to temperature variation in the requisite ranges may be used.
  • a thermal sensor mount 28 is provided to mount the thermal sensors 26 on the expander end cap 18.
  • the thermal sensors 26 are secured to the thermal sensor mount 28 by means of a thermally conductive adhesive.
  • the thermal sensor mount 28 may be fabricated from a ceramic, though other suitable materials may be used.
  • the flex cables 30 permit signals generated by the detector 12 to be delivered to a distribution board 32.
  • the flex cables 30 are attached at one end to the conductive pads of the detector 12 through gold lead wires.
  • the other end of the flex cables 30 connect to a distribution board 32.
  • the flex cables shown in FIG. 1 have been rotated by 45°.
  • the flex cables 30 comprise a flexible etched circuit having metallic conductors disposed between layers of rxolymide base dielectric material attached by means of an acrylic adhesive.
  • the distribution board 32 includes a plurality of internal conductors oriented to permit access to the electrical signals delivered to one side of the distribution board by the flex cables 30 to the opposing side of the distribution board 32.
  • a plurality of load springs 34 and screws 36 are provided to clamp the flex cables 30 to the distribution board 32.
  • a connector 38 is provided.
  • the connector 38 receives the electrical signals frcm the distribution board 32 through a plurality of conductive pins 40.
  • the conductive pins 40 extend frcm the distribution board 32 through the connector 38 to a position above the connector 38 where they can be accessed.
  • a shroud 39 is provided to protect the distribution board 32 from the environment.
  • the bias resistor board 42 is provided which electrically communicates with the connector 38.
  • the bias resistor board 42 functions as a voltage divider so that the appropriate voltages are delivered to the detector 12 to ensure proper operation.
  • the integrated detector dewar cryoengine 10 further comprises an assembly housing 44 and a mount plate 46.
  • the assembly housing 44 is used to provide structural support to the components of the integrated detector dewar cryoengine 10, and may be fabricated from a low expansion alloy. It is to be understood, however, that other suitable materials may be used.
  • the mount plate 46 is used to secure the integrated detector dewar cryoengine 10 in its appropriate position.
  • the mount plate 46 mechanically communicates with a base adjustment nut 48, which permits rotation of the mount plate 46 independent of the expander housing 22.
  • An O-ring 50 is disposed between expander housing 22 and the mount plate 46 to provide friction upon rotation of the mount plate 46.
  • the integrated detector dewar cryoengine 10 further comprises a bulkhead 52 and a shield 54.
  • the bulkhead 52 is welded to the assembly housing 44 and mechanically communicates with an evacuation tube 56.
  • the evacuation tube 56 is used to withdraw gases from the integrated detector dewar cryoengine 10 to maximize the thermal isolation.
  • the bulkhead 52 also communicates with two getter feedthrus 58 which communicates with two getters 60.
  • the getters 60 are used during the evacuation process to further eliminate gases inside the integrated detector dewar cryoengine 10.
  • the bulkhead 52 mechanically communicates with shield 54 and a frame 64 to form the sides of the vacuum chamber.
  • a window 66 and a window housing 68 are provided to form the top of the vacuum chamber.
  • the window 66 is fabricated from germanium or zinc selenide to produce the desired transmission band, and is used to transmit incoming infrared radiation on the detector 12.
  • the window housing 68 is used to support the window 66 and to permit the integrated detector dewar cryoengine 10 to be evacuated.
  • a coldshield 70 is provided which is centrally located over the detector 12.
  • the coldshield 70 is connected to two of four castellations on the expander end cap 18 and has an aperture which provides an unobstructed path for infrared radiation from the environment to be received by the detector 12.
  • the coldshield 70 has a thin wall and is fabricated frcm a high conductivity material so as to have a relatively low thermal mass which reduces cooldown time. While the coldshield may be fabricated from 6061-T6 aluminum, it is to be understood that other suitable materials may be used.
  • the detector 12 is in direct thermal communication with the expander end cap 18, the detector 12 may be cooled more rapidly than would otherwise be possible.
  • the dewar and the expander form an integrated unit, the cross-sectional area through which cold loss can occur is reduced.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • Radiation Pyrometers (AREA)
  • Photometry And Measurement Of Optical Pulse Characteristics (AREA)
  • Measurement Of Radiation (AREA)

Abstract

The integrated detector dewar cryoengine (10) includes a detector (12) for detecting received electromagnetic radiation. The integrated detector dewar cryoengine (10) further comprises expander end cap (18) for removing thermal energy from said detector (12) which is in mechanical communication with said detector (12).

Description

INTEGRATED DETECTOR DEWAR CRYOENGINE
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates to the field of infrared sensing, and more particularly to an integrated detector dewar cryoengine.
2. Description of Related Art
Infrared detectors are often used in conjunction with missiles and night vision systems to sense the presence of electromagnetic radiation having a wavelength of 1-15 urn. Because they are often most sensitive when operating at approximately 77ºK, infrared detectors such as those fabricated from mercury-cadmium-telluride often require a cryoengine assembly to produce and maintain the required operating temperature. Such cryoengine assemblies are typically used in conjunction with an evacuated dewar in which the infrared detector is placed. The dewar is evacuated to remove thermally conductive gases which would otherwise occupy the region surrounding the detector. The dewar is cooled by placing an indented region ("coldwell") of the dewar in contact with an expansion chamber ("expander") of the cryoengine assembly which is supplied with a cooling fluid such as helium. The coldwell and the expander are separated by a gap to allow for variation in the dimensional characteristics of the dewar and expander, as well as to accommodate for differences in their thermal expansion characteristics. To supply the expander with the cooling fluid, the cryoengine assembly often includes a compressor which delivers the fluid to the expander through a transfer line. As the fluid expands in the expander, it absorbs thermal energy from both the expander and the dewar causing the detector to cool Because the temperature of the expander is related to the amount of fluid delivered by the compressor, the temperature of the detector may be controlled by varying the compressor speed. While the infrared detector assemblies described above were able to produce and irmintain the temperature levels required for sensitive operation of the mercury-cadmi um-telluride detectors, they often had several disadvantages in terms of thermal conduction between the expander and the environment. Because the dewar and expander are structurally independent, the gap between the expander and the dewar acted as an insulator to prevent optimal conduction between the expander and the detector. In addition, the cross-sectional area through which cold loss occurred not only included the cross-sectional area of expander, but also included the walls of the dewar which were adjacent to the expander. These two features necessarily meant that the capacity of the cryoengine had to be somewhat larger than would otherwise be required.
SUMMARY OF THE INVENTION
An apparatus for detecting electromagnetic radiation is disclosed. The apparatus comprises a detector for detecting electromagnetic radiation. The apparatus also comprises an expander end cap for removing thermal energy frcm said detector. The device for removing thermal energy frcm said detector mechanically communicates with the detector.
BRIEF DESCRIPTION OF THE DRAWINGS Various advantages of the present invention will become apparent to one skilled in the art upon reading the following specification and by reference to the drawings in which:
FIG. 1 is a cross-sectional view of the integrated detector dewar cryoengine by the present invention; and FIG. 2 is an exploded perspective view of the integrated detector cryoengine shown in FIG. 1.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT With reference to the drawings, an integrated detector dewar cryoengine 10 according to the present invention is shown. The integrated detector dewar cryoengine 10 includes an infrared detector 12 for receiving infrared radiation and generating responsive electrical signals. While the detector 12 may be made from a layer of mercury-cadmium-telluride on a sapphire substrate material, other suitable materials such as CdTe and CdSe may also be used. The detector 12 is secured on a detector platform 14 by a thermally conductive adhesive, which rpermits thermal energy to flow from the detector 12. While the detector platform 14 may be fabricated from beryllium, other suitable materials may be used. To remove thermal energy from the detector 12 so as to permit optimum detector performance, the integrated detector dewar cryoengine 10 further comprises an expander assembly 16 (see FIG. 2). The expander assembly 16 includes an expander end cap 18 which mechanically communicates with the detector platform 14 so that thermal energy can flow from the detector platform 14 to the expander end cap 18. The detector platform 14 is disposed between two of four castellations located on the expander end cap 18 and is secured to the expander end cap 18 by means of a thermally conductive adhesive. The expander end cap 18 is disc shaped so as to have a low thermal mass and a high thermal conductivity. The expander end cap 18 is preferably fabricated from beryllium so as to provide a relatively high degree of thermal conductivity, though it is to be understood that other suitable materials may be used.
The expander assembly 16 also includes an expander tube 20 which is brazed to the expander end cap 18. The expander tube 20 houses the refrigeration mechanism for cooling the detector 12 and receives cooling fluid such as helium from a compressor (not shown). By expansion of the fluid inside the expander tube 20, thermal energy is drawn frcm the expander end cap 18 thereby cooling the detector 12. The expander tube 20 is preferably fabricated frcm Inconel so as to have low tiiermal conductivity while being sufficiently rigid to minimize detector movement during operation. To support the expander tube 20, an expander housing 22 is provided. The expander housing 22 is brazed to the expander tube 20 and is connected to the cryoengine compressor (not shown). The expander assembly 16 also includes a cable support 24 which is used to support the flex cables described below.
To monitor the temperature of the infrared detector array, two thermal sensors 26 are located adjacent to the detector 12 on the flex cables described below. The outputs from the thermal sensors 26 are used to control the compressor speed which in turn controls the temperature of the expander assembly 16. Each of the thermal sensors 26 may be a 2N2222 switching diode, though it is to be understood that other suitable temperature sensors which are sensitive to temperature variation in the requisite ranges may be used. To mount the thermal sensors 26 on the expander end cap 18, a thermal sensor mount 28 is provided. The thermal sensors 26 are secured to the thermal sensor mount 28 by means of a thermally conductive adhesive. The thermal sensor mount 28 may be fabricated from a ceramic, though other suitable materials may be used.
To permit electrical communication between the detector 12 and external electronics, two flex cables 30 are provided. The flex cables 30 permit signals generated by the detector 12 to be delivered to a distribution board 32. The flex cables 30 are attached at one end to the conductive pads of the detector 12 through gold lead wires. The other end of the flex cables 30 connect to a distribution board 32. For purposes of clarity, the flex cables shown in FIG. 1 have been rotated by 45°. The flex cables 30 comprise a flexible etched circuit having metallic conductors disposed between layers of rxolymide base dielectric material attached by means of an acrylic adhesive. The distribution board 32 includes a plurality of internal conductors oriented to permit access to the electrical signals delivered to one side of the distribution board by the flex cables 30 to the opposing side of the distribution board 32. A plurality of load springs 34 and screws 36 are provided to clamp the flex cables 30 to the distribution board 32.
To permit access to the electrical signals delivered to the distribution board 32 by the flex cables 30, a connector 38 is provided. The connector 38 receives the electrical signals frcm the distribution board 32 through a plurality of conductive pins 40. The conductive pins 40 extend frcm the distribution board 32 through the connector 38 to a position above the connector 38 where they can be accessed. A shroud 39 is provided to protect the distribution board 32 from the environment. To appropriately bias to the detectors 12, the bias resistor board 42 is provided which electrically communicates with the connector 38. The bias resistor board 42 functions as a voltage divider so that the appropriate voltages are delivered to the detector 12 to ensure proper operation. To provide structural integrity to the integrated detector dewar cryoengine 10, the integrated detector dewar cryoengine 10 further comprises an assembly housing 44 and a mount plate 46. The assembly housing 44 is used to provide structural support to the components of the integrated detector dewar cryoengine 10, and may be fabricated from a low expansion alloy. It is to be understood, however, that other suitable materials may be used. The mount plate 46 is used to secure the integrated detector dewar cryoengine 10 in its appropriate position. The mount plate 46 mechanically communicates with a base adjustment nut 48, which permits rotation of the mount plate 46 independent of the expander housing 22. An O-ring 50 is disposed between expander housing 22 and the mount plate 46 to provide friction upon rotation of the mount plate 46.
To environmentally isolate the detector 12 and the expander end cap 18, the integrated detector dewar cryoengine 10 further comprises a bulkhead 52 and a shield 54. The bulkhead 52 is welded to the assembly housing 44 and mechanically communicates with an evacuation tube 56. The evacuation tube 56 is used to withdraw gases from the integrated detector dewar cryoengine 10 to maximize the thermal isolation. The bulkhead 52 also communicates with two getter feedthrus 58 which communicates with two getters 60. The getters 60 are used during the evacuation process to further eliminate gases inside the integrated detector dewar cryoengine 10. The bulkhead 52 mechanically communicates with shield 54 and a frame 64 to form the sides of the vacuum chamber. A window 66 and a window housing 68 are provided to form the top of the vacuum chamber. The window 66 is fabricated from germanium or zinc selenide to produce the desired transmission band, and is used to transmit incoming infrared radiation on the detector 12. The window housing 68 is used to support the window 66 and to permit the integrated detector dewar cryoengine 10 to be evacuated. To minimize the amount of thermal radiation delivered to the detector 12 from sources other than the scene, a coldshield 70 is provided which is centrally located over the detector 12. The coldshield 70 is connected to two of four castellations on the expander end cap 18 and has an aperture which provides an unobstructed path for infrared radiation from the environment to be received by the detector 12. The coldshield 70 has a thin wall and is fabricated frcm a high conductivity material so as to have a relatively low thermal mass which reduces cooldown time. While the coldshield may be fabricated from 6061-T6 aluminum, it is to be understood that other suitable materials may be used.
Because the detector 12 is in direct thermal communication with the expander end cap 18, the detector 12 may be cooled more rapidly than would otherwise be possible. In addition, because the dewar and the expander form an integrated unit, the cross-sectional area through which cold loss can occur is reduced. It should therefore be understood that this invention was described in connection with a particular example thereof. Other modifications will become apparent to those skilled in the art after a study of the specification, drawings, and following claims.

Claims

CLAIMSWhat is Claimed is:
1. An apparatus for detecting electromagnetic radiation comprising: detector means for detecting electromagnetic radiation; and means for removing thermal energy from said detector means, said means for removing thermal energy from said detector means being in mechanical communication with said detector means.
2. The apparatus of Claim 1, wherein said means for removing thermal energy from said detector means comprises an expander.
3. The apparatus of Claim 2, wherein said expander includes an expander end cap.
4. The apparatus of Claim 3, wherein said expander end cap is disc shaped.
5. The apparatus of Claim 4, wherein said expander end cap is fabricated from beryllium.
6. The apparatus of Claim 1, wherein said means for removing thermal energy from said detector means further comprises a detector mount, said detector mount mechanically communicating with said detector means.
7. An apparatus for detecting electromagnetic radiation comprising: detector means for detecting electromagnetic radiation; means for removing thermal energy from said detector means; and means for environmentally isolating said detector means and said means for removing thermal energy from said detector meann.
8. The apparatus of Claim 7, wherein said means for removing thermal energy from said detector means comprising an expander, said means for environmentally isolating said detector means and said means for removing thermal energy from said detector means comprises an expander housing operably to mechanically support said expander.
9. The apparatus of Claim 8, wherein said means for environmentally isolating said detector means and said means for removing thermal energy from said detector means further comprises an assembly housing.
10. The apparatus of Claim 9, wherein said means for environmentally isolating said detector means and said means for removing thermal energy from said detector means further comprises a bulkhead mechanically communicating with said assembly housing.
11. The apparatus of Claim 10, wherein said means for environmentally isolating said detector means and said means for removing thermal energy from said detector means further comprises a shield mechanically communicating with said bulkhead.
12. The apparatus of Claim 11, wherein said means for environmentally isolating said detector means and said means for removing thermal energy from said detector means further comprises a frame mechanically communicating with said shield.
13. The apparatus of Claim 12, wherein said means for environmentally isolating said detector means and said means for removing thermal energy from said detector means further comprises a distribution board mechanically communicating with said frame.
14. The apparatus of Claim 13, wherein said means for environmentally isolating said detector means and said means for removing thermal energy from said detector means further comprises a window housing mechanically communicating with said assembly housing.
15. The apparatus of Claim 14, wherein said means for envirommentally isolating said detector means and said means for removing thermal energy from said detector means further comprises a window mechanically communicating with said window housing.
16. The apparatus of Claim 7, wherein said means for removing thermal energy from said detector means comprises a detector mount disposed on an expander end cap, said detector means mechanically communicating with said detector mount.
17. A method for removing thermal energy from a detector in an electromagnetic detection apparatus using an expander, said method ccmprising the steps of: evacuating a region of said apparatus surrounding said detector and said expander; and permitting thermal energy from said detector to be drawn from said detector to said expander.
18. The method of Claim 17, wherein said expander comprises a disc shaped expander end cap.
19. The method of Claim 18, wherein said detector mount is fabricated from beryllium.
20. The method of Claim 17, wherein said step of permitting thermal energy to flow from said detector to said expander includes the step of permitting thermal energy to flow through a detector mount mechanically communicating with said detector and said expander.
PCT/US1987/002572 1986-11-21 1987-10-08 Integrated detector dewar cryoengine WO1988004037A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
DE3789380T DE3789380T2 (en) 1986-11-21 1987-10-08 CRYOGENIC ENGINE WITH DEWARING VESSEL AND INTEGRATED DETECTOR.
JP62506868A JPH0695046B2 (en) 1986-11-21 1987-10-08 Integrated detector, dual and low temperature engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US93350786A 1986-11-21 1986-11-21
US933,507 1986-11-21

Publications (1)

Publication Number Publication Date
WO1988004037A1 true WO1988004037A1 (en) 1988-06-02

Family

ID=25464100

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1987/002572 WO1988004037A1 (en) 1986-11-21 1987-10-08 Integrated detector dewar cryoengine

Country Status (4)

Country Link
EP (1) EP0290517B1 (en)
JP (1) JPH0695046B2 (en)
DE (1) DE3789380T2 (en)
WO (1) WO1988004037A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2629912A1 (en) * 1988-08-05 1989-10-13 Detecteurs Infrarouges Ste Fse Infrared detection device operating at low temperature
EP0364347A1 (en) * 1988-10-13 1990-04-18 SAT (SOCIETE ANONYME DE TELECOMMUNICATIONS) Société Anonyme française Cryostat for a radiation detector
EP0518515A1 (en) * 1991-06-03 1992-12-16 Hughes Aircraft Company Rapid cooldown dewar

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008014003B4 (en) * 2008-03-13 2010-02-11 Bundesrepublik Deutschland, vertr.d.d. Bundesministerium für Wirtschaft und Technologie, d.vertr.d.d. Präsidenten der Physikalisch-Technischen Bundesanstalt Cryosensor positioning device and cryostatic system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2027181A (en) * 1978-06-21 1980-02-13 Philips Electronic Associated Detectors and envelope arrangements for detectors
EP0115698A1 (en) * 1982-12-27 1984-08-15 Honeywell Inc. Cold radiation detector assembly
WO1987001448A1 (en) * 1985-09-03 1987-03-12 Santa Barbara Research Center Integrated infrared detector and cryoengine assembly

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5731181A (en) * 1980-07-08 1982-02-19 Fujitsu Ltd Cooling type photoelectric converter
JPS5727075A (en) * 1980-07-24 1982-02-13 Fujitsu Ltd Cooling type photoelectric converter

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2027181A (en) * 1978-06-21 1980-02-13 Philips Electronic Associated Detectors and envelope arrangements for detectors
EP0115698A1 (en) * 1982-12-27 1984-08-15 Honeywell Inc. Cold radiation detector assembly
WO1987001448A1 (en) * 1985-09-03 1987-03-12 Santa Barbara Research Center Integrated infrared detector and cryoengine assembly

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2629912A1 (en) * 1988-08-05 1989-10-13 Detecteurs Infrarouges Ste Fse Infrared detection device operating at low temperature
EP0364347A1 (en) * 1988-10-13 1990-04-18 SAT (SOCIETE ANONYME DE TELECOMMUNICATIONS) Société Anonyme française Cryostat for a radiation detector
FR2638023A1 (en) * 1988-10-13 1990-04-20 Telecommunications Sa CRYOSTATIC DEVICE FOR RADIATION DETECTOR
US4995236A (en) * 1988-10-13 1991-02-26 Societe Anonyme De Telecommunications Cryostatic device for a radiation detector
EP0518515A1 (en) * 1991-06-03 1992-12-16 Hughes Aircraft Company Rapid cooldown dewar

Also Published As

Publication number Publication date
JPH01502134A (en) 1989-07-27
EP0290517B1 (en) 1994-03-16
JPH0695046B2 (en) 1994-11-24
DE3789380D1 (en) 1994-04-21
EP0290517A1 (en) 1988-11-17
DE3789380T2 (en) 1994-12-15

Similar Documents

Publication Publication Date Title
EP0403880B1 (en) Radiation shield for thermoelectrically cooled infrared detectors
US5371369A (en) Conformal cold baffle for optical imaging systems
GB2370344A (en) Fast cooldown cryostat for large infrared focal plane arrays
US5187939A (en) Rapid cooldown dewar
EP0136687B1 (en) Infrared receiver
US5179283A (en) Infrared detector focal plane
US6122919A (en) Sensor/cooling system with cold finger having recessed end
GB2147739A (en) A housing for a radiation sensitive semiconductor component
US4918308A (en) Integrated detector dewar cryoengine
US4954708A (en) Low distortion focal plane platform
US6698224B2 (en) Electronic apparatus having at least two electronic parts operating at different temperatures
EP0290517B1 (en) Integrated detector dewar cryoengine
EP0235284B1 (en) Integrated infrared detector and cryoengine assembly
US4873843A (en) Multiple source and/or sensor coldhead mount
US4412427A (en) Noncontact thermal interface
US5485005A (en) Cooled x-ray sensitive photoconductor
EP0213421A2 (en) Infrared detector assembly having vacuum chambers
US4399661A (en) Prolonged cold temperature cryogenic cooler
WO1987005990A1 (en) Modular photon detector cryostat assembly and system
US4661707A (en) Disc detector assembly having prefabricated vacuum chambers
JP3110456B2 (en) Rapidly cooled cryostat for large infrared focal plane arrays
GB2186741A (en) Infrared detectors
SU1716409A1 (en) Sensor for x-ray radiometric analyzer with semiconductor detector
JPH0453246B2 (en)
Burt Cooling of very large focal plane arrays

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): JP

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): DE FR GB IT NL

WWE Wipo information: entry into national phase

Ref document number: 1987907368

Country of ref document: EP

WWP Wipo information: published in national office

Ref document number: 1987907368

Country of ref document: EP

WWG Wipo information: grant in national office

Ref document number: 1987907368

Country of ref document: EP