CN206556767U - A kind of high-precision infrared imaging system image planes docking facilities - Google Patents

A kind of high-precision infrared imaging system image planes docking facilities Download PDF

Info

Publication number
CN206556767U
CN206556767U CN201720123079.6U CN201720123079U CN206556767U CN 206556767 U CN206556767 U CN 206556767U CN 201720123079 U CN201720123079 U CN 201720123079U CN 206556767 U CN206556767 U CN 206556767U
Authority
CN
China
Prior art keywords
infrared
optics
guide rail
parallel light
image detector
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
CN201720123079.6U
Other languages
Chinese (zh)
Inventor
武力
曹剑中
刘伟
淡佳伟
屈波
杨凯
党艳玲
何月娜
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xi'an Zhongke Feitu Photoelectric Technology Co Ltd
Original Assignee
Xi'an Zhongke Feitu Photoelectric Technology Co Ltd
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 Xi'an Zhongke Feitu Photoelectric Technology Co Ltd filed Critical Xi'an Zhongke Feitu Photoelectric Technology Co Ltd
Priority to CN201720123079.6U priority Critical patent/CN206556767U/en
Application granted granted Critical
Publication of CN206556767U publication Critical patent/CN206556767U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Photometry And Measurement Of Optical Pulse Characteristics (AREA)

Abstract

The utility model is related to a kind of high-precision infrared imaging system image planes docking facilities, image planes docking, punching applied to Aeronautics and Astronautics field infrared optical imaging system.The device includes being sequentially installed with image detector, infrared optics imaging lens and parallel light tube on display and horizontally disposed optics guide rail, optics guide rail;Image detector is connected by combining mobile station with optics guide rail;Image detector is included towards the image detector focal plane of infrared optics imaging lens, and image detector is connected with display;Infrared optics imaging lens are connected by combining mobile station with optics guide rail;Parallel light tube is connected by parallel light tube support with optics guide rail;Parallel light tube support and combination mobile station can carry out three-dimensional translating and rotation.The utility model infrared imaging system punching apparatus structure is simple, easy to operate, can be widely applied in engineering practice, especially produces in enormous quantities in scientific research mission.

Description

A kind of high-precision infrared imaging system image planes docking facilities
Technical field
The utility model is related to a kind of high-precision infrared imaging system image planes docking facilities, applied to Aeronautics and Astronautics field The image planes docking of infrared optical imaging system, punching.
Background technology
The Infrared imaging cameras that infrared optical imaging system is constituted with infrared imaging focus plane is space flight, aviation field flight The significant components of device, video image is provided for each generic task, is easy to the monitoring and control on ground.Infrared optical imaging system is to it The registration required precision of system optical axis and imaging focal plane target surface centre normal is very high, how in infrared imaging device Ensure that These parameters requirement turns into the important step for determining infrared imaging device image quality and measurement accuracy in assembling process.
Utility model content
In order to solve that during existing infrared optical lens and infrared imaging focus plane punching optical lens can not be ensured The technical problem of the registration accuracy of optical axis and focal plane target surface centre normal, the utility model provide a kind of high accuracy it is infrared into As system image planes docking facilities.
Technical solution of the present utility model is:A kind of high-precision infrared imaging system image planes docking facilities, its is special Part is:Including display and horizontally disposed optics guide rail, infrared image detection is sequentially installed with the optics guide rail Device, infrared optics imaging lens and parallel light tube;
Described image detector is connected by combining mobile station with optics guide rail;Described image detector is included towards infrared The image detector focal plane of optical imaging lens, described image detector is connected with display;
The infrared optics imaging lens are connected by combining mobile station with optics guide rail;
The parallel light tube is connected by parallel light tube support with optics guide rail;
The parallel light tube support and combination mobile station can carry out three-dimensional translating and rotation.
Preferably, above-mentioned parallel light tube is the infrared auto-collimation collimator for being provided with graticle, the graticle is ten Word cross hair.
Preferably, aforementioned display device is the electric crosshair display of viewing area middle position self-generating.
The utility model also provides a kind of high-precision infrared imaging system image planes docking calculation, and it is characterized in that:Bag Include following steps:
1) adjustment of parallel light tube optical axis and guide rail parallelism:
On the sliding block that parallel light tube is installed on to optics guide rail one end by parallel light tube support;Adjust parallel light tube branch Frame, makes the optical axis and optics guide rail parallel of parallel light tube, then fixes parallel light tube;
2) parallel light tube optical axis and the adjustment of image detector focal plane perpendicularity:
Image detector is installed on to the other end of optics guide rail by combining mobile station;Adjust still image detector Mobile station is combined, the crosshair that the light that auto-collimation collimator is sent is formed after cross-graduation plate is passed through image detector Surface is reflected to be overlapped with the crosshair picture of parallel light tube afterwards, then still image detector, complete parallel light tube optical axis with The adjustment of image detector focal plane perpendicularity;
3) adjustment of optical lens imaging surface and image detector focal plane registration:
Between image detector and parallel light tube, optical lens is installed on guide rail by combining mobile station;Will figure As detector is connected with display, optical lens is moved along optics guide rail, makes to generate clearly image on display, complete optics Lens imaging face is adjusted with image detector focal plane registration;
4) adjustment of optical lens optical axis and image detector focal plane centre normal registration:
The combination mobile station of the fixed optical lens of regulation, makes the light source of auto-collimation collimator by being sent out after cross-graduation plate Crosshair of the directional light gone out through the electric crosshair display center of crosshair picture formed by optical lens and self-generating is overlapped, then Fixed optical lens, completes the adjustment of optical lens optical axis and image detector focal plane centre normal registration.
Preferably, above-mentioned parallel light tube is the infrared auto-collimation collimator for being provided with graticle.
Step 2) in adjusting method be:The light that auto-collimation collimator is sent reaches image detection after cross-graduation plate The picture and collimator tube reticle for the cross-graduation plate that mobile station is reflected image detector surface are combined in the surface of device, regulation As coinciding.
Above-mentioned graticle is crosshair.
Preferably, aforementioned display device is the electric crosshair display of viewing area middle position self-generating.
The beneficial effects of the utility model are:
(1) the utility model infrared imaging system punching apparatus structure is simple, easy to operate, can be widely applied to engineering real In trampling, especially produce in enormous quantities in scientific research mission;
(2) device and method that the utility model is provided reduces the error that mechanical measurement and assembling are brought, punching precision Height, can obtain good imaging effect;
(3) the image planes docking facilities and method that the utility model is provided reduce the error that mechanical measurement and assembling are brought, Punching precision is high, can obtain good imaging effect.
Brief description of the drawings
Fig. 1 is the preferred embodiment structural representation of the utility model image planes docking facilities.
Fig. 2 is that parallel light tube adjusts schematic diagram with optics guide rail parallel.
Fig. 3 is parallel light tube and image detector focal plane perpendicularity regulation schematic diagram.
Fig. 4 is infrared optics imaging lens and image detector focal plane registration regulation schematic diagram.
Embodiment
Referring to Fig. 1, the utility model provides a kind of high-precision infrared imaging system image planes docking facilities, its preferred embodiment Structure include display 9 and horizontally disposed optics guide rail 1, be sequentially installed with optics guide rail 1 infrared image detection device 7, Infrared optics imaging lens 5 and parallel light tube 3.
Wherein, infrared image detection device 7 is first installed in detector carriage 8, then again by combining mobile station 6 and optics Guide rail 1 is connected;The focal plane of infrared image detection device 7 is towards infrared optics imaging lens 5.Infrared image detection device 7 and display Device 9 is connected, and the display in the present embodiment is the electric crosshair display of viewing area middle position self-generating.
Infrared optics imaging lens 5 are first installed on lens bracket 4, then again by combining mobile station 6 and optics guide rail 1 It is connected.
Parallel light tube 3 is connected by parallel light tube support 2 with optics guide rail 1.Parallel light tube in the present embodiment is to install There is the infrared auto-collimation collimator of graticle, wherein graticle can use crosshair.
Parallel light tube support 2 and combination mobile station 6 can carry out three-dimensional translating and rotation, play the work of support and regulation With.
Use comprising the following steps that for the utility model image planes docking facilities:
Step 1, referring to Fig. 2, the optical axis of parallel light tube 3 and the optics guide rail 1 of lower section are made by adjusting parallel light tube support 2 It is parallel, and be fixed on the sliding block of optics guide rail 1.
Step 2, referring to Fig. 3, infrared image detection device 7 installed by detector carriage 8 in the opposite side of optics guide rail 1, Infrared image detection device focal plane geometric center height is adjusted, makes it highly consistent with parallel light tube, auto-collimation is infrared parallel Light pipe sends collimated light beam to the surface of image detector, and regulation combination mobile station makes the cross that image detector surface is reflected The picture and collimator tube reticle picture of graticle coincide, while fixing image detector 7
Step 3, referring to Fig. 4, infrared light is installed by lens bracket 4 in the middle of parallel light tube 3 and infrared image detection device 7 Learn imaging lens 5, connection display system and power supply.After energization, regulation infrared optics imaging lens 5 and infrared image detection device 7 The distance between, after optical lens imaging surface is overlapped with infrared image detection device focal plane position, in the electric crosshair of self-generating Clearly image can be generated on display, can realize that optical lens is imaged by adjusting the combination mobile station 6 below optical lens Face is adjusted with infrared image detection device focal plane position registration.
Step 4, after being powered to image detector, a crosshair can be formed in the electric crosshair display center of self-generating, It is the focal plane center of infrared image detection device at crosshair.The light source of auto-collimation collimator passes through crosshair graduation The ten of display center of the directional light sent after plate through crosshair picture formed by infrared optical lens and the electric crosshair of self-generating The optical axis that word silk overlaps explanation infrared optical lens is overlapped with infrared image detection device focal plane centre normal, such as misaligned, is adjusted The translational degree of freedom that section installs the combination mobile station of infrared optical lens causes the optical axis of infrared optical lens and infrared image to visit Device focal plane centre normal is surveyed to overlap.

Claims (4)

1. a kind of high-precision infrared imaging system image planes docking facilities, it is characterised in that:Including display and horizontally disposed light Learn and be sequentially installed with image detector, infrared optics imaging lens and parallel light tube on guide rail, the optics guide rail;
Described image detector is connected by combining mobile station with optics guide rail;Described image detector is included towards infrared optics The image detector focal plane of imaging lens, described image detector is connected with display;
The infrared optics imaging lens are connected by combining mobile station with optics guide rail;
The parallel light tube is connected by parallel light tube support with optics guide rail;
The parallel light tube support and combination mobile station can carry out three-dimensional translating and rotation.
2. high-precision infrared imaging system image planes docking facilities according to claim 1, it is characterised in that:The directional light Manage that the infrared auto-collimation collimator of graticle is installed.
3. high-precision infrared imaging system image planes docking facilities according to claim 2, it is characterised in that:The graticle For crosshair.
4. according to any described high-precision infrared imaging system image planes docking facilities in claim 1-3, it is characterised in that:Institute It is the electric crosshair display of viewing area middle position self-generating to state display.
CN201720123079.6U 2017-02-10 2017-02-10 A kind of high-precision infrared imaging system image planes docking facilities Active CN206556767U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720123079.6U CN206556767U (en) 2017-02-10 2017-02-10 A kind of high-precision infrared imaging system image planes docking facilities

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720123079.6U CN206556767U (en) 2017-02-10 2017-02-10 A kind of high-precision infrared imaging system image planes docking facilities

Publications (1)

Publication Number Publication Date
CN206556767U true CN206556767U (en) 2017-10-13

Family

ID=60011169

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720123079.6U Active CN206556767U (en) 2017-02-10 2017-02-10 A kind of high-precision infrared imaging system image planes docking facilities

Country Status (1)

Country Link
CN (1) CN206556767U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106681098A (en) * 2017-02-10 2017-05-17 中国科学院西安光学精密机械研究所 Image-face abutting device and method of high-precision visible light imaging system
CN108196379A (en) * 2017-12-14 2018-06-22 中国航空工业集团公司洛阳电光设备研究所 A kind of optical system through axle light pipe and wear axis method
CN108628112A (en) * 2018-06-05 2018-10-09 汪玉洁 A kind of semiconductor chip production immersed photoetching machine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106681098A (en) * 2017-02-10 2017-05-17 中国科学院西安光学精密机械研究所 Image-face abutting device and method of high-precision visible light imaging system
CN106681098B (en) * 2017-02-10 2022-05-20 中国科学院西安光学精密机械研究所 High-precision image surface docking device and method for visible light imaging system
CN108196379A (en) * 2017-12-14 2018-06-22 中国航空工业集团公司洛阳电光设备研究所 A kind of optical system through axle light pipe and wear axis method
CN108628112A (en) * 2018-06-05 2018-10-09 汪玉洁 A kind of semiconductor chip production immersed photoetching machine
CN108628112B (en) * 2018-06-05 2020-07-21 温州杰锐电子科技有限公司 Immersion lithography machine for semiconductor chip production

Similar Documents

Publication Publication Date Title
CN106706139B (en) A kind of high-precision infrared imaging system image planes docking calculation
CN106681098A (en) Image-face abutting device and method of high-precision visible light imaging system
CN206556767U (en) A kind of high-precision infrared imaging system image planes docking facilities
CN103148826B (en) A kind of rotatable large-caliber optical element clamp
CN107320122B (en) CT center indicating assembly and PET-CT mounting rack
US20080123112A1 (en) Photogrammetric contrasting light for hole recognition
CN103024254B (en) A kind of imaging Method of Adjustment of television cameras
CN106570932A (en) Image-based human head three dimensional data acquisition system and method
CN102406504A (en) Double-column non-contact three-dimensional (3D) automatic human dimension measuring instrument
CN104197835B (en) Spatial position simulation and calibration method
CN205094465U (en) CT indicates at center subassembly and PET -CT installation frame
CN109084959A (en) A kind of parallelism of optical axis bearing calibration based on binocular location algorithm
CN107817094A (en) A kind of high accuracy double optical axises and more plain shaft parallelism adjusting process in the same direction
CN107817095A (en) A kind of high accuracy double optical axises and more plain shaft parallelism adjusting process in the same direction
Valsecchi et al. Facility for alignment, assembly, and integration of the SPO mirror modules onto the ATHENA telescope
RU2601505C1 (en) Method of guiding radiation of multi-channel laser at preset points of target and system for its implementation
Paufique et al. GRAAL on the mountaintop
CN106643745B (en) Deep space exploration planet landing simulator pose measuring device and method
CN206515608U (en) A kind of high-precision Visible imaging system image planes docking facilities
CN102431485B (en) Vehicle-mounted non-contact three-dimensional automatic human body measuring system
CN103309147B (en) Visible Light Camera focal plane rapid alignment method and device
CN212276119U (en) Device for matching high-precision assembling optical axis with guide rail moving shaft
Zhao et al. The fiber view metrology system design for spectral survey telescope
CN104581150A (en) Positioning and error compensation method
Santoro et al. Mechanical design of the Magdalena Ridge Observatory interferometer

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant