CN103345041B - Space camera mirror assembly dress school position conversion device - Google Patents
Space camera mirror assembly dress school position conversion device Download PDFInfo
- Publication number
- CN103345041B CN103345041B CN201310269966.0A CN201310269966A CN103345041B CN 103345041 B CN103345041 B CN 103345041B CN 201310269966 A CN201310269966 A CN 201310269966A CN 103345041 B CN103345041 B CN 103345041B
- Authority
- CN
- China
- Prior art keywords
- mirror assembly
- space camera
- camera mirror
- screw
- connection block
- 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.)
- Expired - Fee Related
Links
Abstract
The invention provides a kind of space camera mirror assembly dress school position conversion device, belong to space optics technical field.Solve existing mirror assembly and be transitioned into by debuging, detecting frock the attitude, the position deviation problem that occur in the conversion connection process of space camera support frame.This device comprises debugs working plate, bottom plate and guide piece, described guide piece comprises transition Connection Block and the axis of guide, described bottom plate is connected with the bottom of debuging working plate, transition Connection Block with debug working plate top and be connected, the axis of guide is connected with space camera mirror assembly back through transition Connection Block, bottom plate arranges screw, and described screw is connected with bottom space camera mirror assembly.Conversion equipment of the present invention can reduce space camera mirror assembly and be transitioned into position deviation in the coupled position transfer process of space camera support frame by debuging, detecting position, the position dress position deviation of changing in process is controlled within 0.01mm.
Description
Technical field
The invention belongs to space optics technical field, be specifically related to space camera mirror assembly dress school position conversion device.
Background technology
Debug in process at space camera mirror assembly and support frame, first tackle mirror assembly and carry out ripple phase difference detection, by debuging, detecting frock, mirror assembly height, displacement, pitching, inclination, rotation are adjusted, obtain best ripple phase difference detection result, now mirror assembly is in optimum detection attitude, namely with the connection attitude of support frame, then is connected with space camera support frame.Conventional method of attachment is: by mirror assembly and support frame screw pretension, and what rely on screw axially fastens the mirror assembly not off-target test pose after demonstrate,proving connection of trying hard to keep; Again by mirror assembly with debug, detect frock and be separated; Mirror assembly and support frame attachment screw torque spanner are locked, complete by debug, detect frock be transitioned into space camera support frame conversion connect.Rapid is in two steps consider screw lock to debug, detect before frock is separated with mirror assembly and still have pulling force effect to assembly, avoids once locking and causes assembly stressed, produce irrecoverable distortion.
Mirror assembly due to self gravitation reason, when with debug, detect after frock is separated, only rely on screw pretightning force that assembly cannot be avoided radial at screw, namely vertical direction is to bottom offset; Each screw is different from gap between screw, because assembly can cause again assembly inclination, pitching to bottom offset.Finally, mirror assembly is connected with support frame and retrodeviates from optimum detection attitude, can not get best ripple phase difference detection result.Mirror assembly has to be separated with support frame, then re-starts adjustment; Again debug, also may there will be same problem.
Summary of the invention
The object of the invention is to be transitioned into by debuging, detecting frock the attitude, the position deviation problem that occur in the conversion connection process of space camera support frame in order to solve existing mirror assembly, providing a kind of space camera mirror assembly to fill school position conversion device.
Space camera mirror assembly dress school position conversion device, this device comprises debugs working plate, bottom plate and guide piece, described guide piece comprises transition Connection Block and the axis of guide, described bottom plate is connected with the bottom of debuging working plate, transition Connection Block with debug working plate top and be connected, the axis of guide is connected with space camera mirror assembly back through transition Connection Block, and bottom plate arranges screw, and described screw is connected with bottom space camera mirror assembly.
Principle of work of the present invention
The invention provides a kind of space camera mirror assembly dress school position conversion device, this conversion equipment comprises debugs working plate, bottom plate and guide piece, described guide piece comprises transition Connection Block and the axis of guide, bottom plate arranges screw, be connected with space camera mirror assembly by the screw that bottom plate is arranged, eliminate gravity effect, avoid space camera mirror assembly and debug, detect frock and be separated position deviation on time space camera mirror assembly vertical direction; The described axis of guide is connected with space camera mirror assembly back through transition Connection Block, and the axis of guide serves location, orientation, prevents space camera mirror assembly to tilt, rotate and lie on the back.
Beneficial effect of the present invention
The invention provides a kind of space camera mirror assembly dress school position conversion device, compare with prior art, conversion equipment of the present invention can reduce space camera mirror assembly greatly by the position deviation debug, detect position and be transitioned in the transfer process of the coupled position of space camera support frame, position, the dress school conversion of implementation space camera mirror assembly high precision, high stability, and the position dress position deviation of changing in process is controlled within 0.01mm.
Accompanying drawing explanation
A kind of space camera mirror assembly dress of Fig. 1 the present invention school position conversion device schematic layout pattern.
The structural representation of a kind of space camera mirror assembly dress of Fig. 2 the present invention school position conversion device.
Fig. 3 debugs working plate and the connection diagram debuging, detect frock in the position conversion device of a kind of space camera mirror assembly dress of the present invention school.
In figure, 1, debug, detect frock, 2, space camera mirror assembly dress school position conversion device, 3, space camera mirror assembly, 4, support frame, 5, working plate is debug, 6, bottom plate, 7, transition Connection Block, 8, the axis of guide, 9, screw, 10, plate A, 11, plate B, 12, screw.
Embodiment
Composition graphs 1, Fig. 2 and Fig. 3 illustrates present embodiment, a kind of space camera mirror assembly dress school position conversion device, as shown in Figure 2, this device comprises debugs working plate 5, bottom plate 6 and guide piece, described guide piece comprises transition Connection Block 7 and the axis of guide 8, described bottom plate 6 is connected with the bottom of debuging working plate 5, transition Connection Block 7 with debug working plate 5 top and be connected, the axis of guide 8 is connected with space camera mirror assembly 3 back through transition Connection Block 7, bottom plate 6 is arranged screw 9, described screw 9 is connected with bottom space camera mirror assembly 3.
A kind of space camera mirror assembly dress of present embodiment school position conversion device schematic layout pattern as shown in Figure 1, described working plate 5 front end of debuging is connected with space camera mirror assembly 3 screw, back with debug, detect frock 1 and be connected, bottom plate 6 is arranged screw 9 to be connected with the bottom of space camera mirror assembly 3, the axis of guide 8 is connected with space camera mirror assembly 3 back through transition Connection Block 7.
Debug working plate and debug, detect the connection diagram of frock as shown in Figure 3 in the position conversion device of a kind of space camera mirror assembly dress of present embodiment school, described debug working plate 5 and debug, the plate A10 detected in frock 1 is connected, described debuging, detect frock 1 is displacement jacking gear, plate A10 there is screw, screw in screw 12, relative for plate A10 plate B11 can be risen, realize debuging working plate 5 and rise; Screw out screw 12, relative for A10 plate B11 can be declined, realize debuging working plate 5 and decline, meet mirror assembly 3 at the adjustment needs detecting, debug 6 degree of freedom in process.
When space camera mirror assembly 3 adjusts to optimum detection position, unclamp space camera mirror assembly 3 and the attachment screw debuging working plate 5, due to the supporting role of bottom plate 6 and the positioning action of the axis of guide 8, space camera mirror assembly 3 can not depart from screw unclamp before optimum detection position; Mirror assembly 3 is moved along the axis of guide 8 in transition Connection Block 7, contacts with support frame 4, connect with screw, and all go up torque locking; To debug, and detect frock 1 and be separated completely with space camera mirror assembly 3, unload the axis of guide 8 on mirror assembly 3, complete by detecting, debuging the conversion of position to mirror assembly 3 and support frame 4 link position.
Claims (1)
1. space camera mirror assembly dress school position conversion device, this device comprises debugs working plate (5), bottom plate (6) and guide piece, it is characterized in that, described guide piece comprises transition Connection Block (7) and the axis of guide (8), described bottom plate (6) is connected with the bottom of debuging working plate (5), transition Connection Block (7) with debug working plate (5) top and be connected, debug working plate (5) front end to be connected with space camera mirror assembly (3) screw, back with debug, detect frock (1) to connect, the axis of guide (8) is connected with space camera mirror assembly (3) back through transition Connection Block (7), bottom plate (6) is arranged screw (9), described screw (9) is connected with space camera mirror assembly (3) bottom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310269966.0A CN103345041B (en) | 2013-06-28 | 2013-06-28 | Space camera mirror assembly dress school position conversion device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310269966.0A CN103345041B (en) | 2013-06-28 | 2013-06-28 | Space camera mirror assembly dress school position conversion device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103345041A CN103345041A (en) | 2013-10-09 |
| CN103345041B true CN103345041B (en) | 2016-03-02 |
Family
ID=49279853
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310269966.0A Expired - Fee Related CN103345041B (en) | 2013-06-28 | 2013-06-28 | Space camera mirror assembly dress school position conversion device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103345041B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104317033B (en) * | 2014-10-29 | 2017-01-11 | 云南北方驰宏光电有限公司 | Method for adjusting reflectors through decentration measuring instrument |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05157957A (en) * | 1991-12-06 | 1993-06-25 | Toshiba Corp | Mirror device |
| CN1560660A (en) * | 2004-02-16 | 2005-01-05 | �й���ѧԺ�Ϻ���ѧ���ܻ�е�о��� | Large caliber standard plate precison regulation stand |
| CN102981244A (en) * | 2012-12-25 | 2013-03-20 | 中国科学院长春光学精密机械与物理研究所 | Two-dimensional large-diameter transmission-type quick reflecting mirror |
| CN103149662A (en) * | 2013-02-28 | 2013-06-12 | 海信集团有限公司 | Reflecting-mirror bonding method and reflecting-mirror bonding device |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2407369Y (en) * | 1999-12-23 | 2000-11-22 | 中国科学院光电技术研究所 | Two dimension angular trimming regulator for large diameter reflective mirror |
| US20030234991A1 (en) * | 2002-06-20 | 2003-12-25 | Alan Adler | Optical mirror flexing structure and assembly |
-
2013
- 2013-06-28 CN CN201310269966.0A patent/CN103345041B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05157957A (en) * | 1991-12-06 | 1993-06-25 | Toshiba Corp | Mirror device |
| CN1560660A (en) * | 2004-02-16 | 2005-01-05 | �й���ѧԺ�Ϻ���ѧ���ܻ�е�о��� | Large caliber standard plate precison regulation stand |
| CN102981244A (en) * | 2012-12-25 | 2013-03-20 | 中国科学院长春光学精密机械与物理研究所 | Two-dimensional large-diameter transmission-type quick reflecting mirror |
| CN103149662A (en) * | 2013-02-28 | 2013-06-12 | 海信集团有限公司 | Reflecting-mirror bonding method and reflecting-mirror bonding device |
Non-Patent Citations (1)
| Title |
|---|
| 空间遥感器反射镜组件的微应力装配技术;谭进国，何欣，刘强;《红外》;20120731;第33卷(第7期);第18-19页第3部分 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103345041A (en) | 2013-10-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104259720B (en) | For the tailor-welding tool of the supporting rack of torque arm car | |
| CN201892545U (en) | Sensor holder | |
| CN106323980A (en) | Small annular workpiece inner wall panoramic imaging apparatus and method | |
| CN102798510A (en) | Supporting device for automotive wind tunnel experiment model | |
| CN201342647Y (en) | Spherical clamping device | |
| CN103345041B (en) | Space camera mirror assembly dress school position conversion device | |
| CN103669873B (en) | A kind of vibration of arm control appliance, method, system and engineering machinery | |
| CN104787308B (en) | Aircraft foot rest drive arrangement, aircraft undercarriage and aircraft | |
| CN104142235A (en) | Engine suspension rigidity testing tool | |
| CN204024090U (en) | A kind of stiffness post is proofreaied and correct assembly | |
| CN103706987B (en) | A kind of aluminum alloy thick wall reducing cylinder related subgroup location and deformation control method | |
| CN215148293U (en) | Special auxiliary device | |
| CN211980595U (en) | Fixing device for wafer production | |
| CN204789367U (en) | Inner wall panorama image device of small -size cyclic annular work piece | |
| CN205121069U (en) | Manual initiative alignment equipment | |
| CN203202524U (en) | Flat quick-release frame | |
| CN204883067U (en) | 45 light filter assembly device | |
| CN203615000U (en) | Height-adjustable supporting device | |
| CN204075601U (en) | For the tailor-welding tool of the supporting rack of torque arm car | |
| CN207171256U (en) | A kind of coaxial CCD lens regulating structures of laser-beam welding machine | |
| CN204235102U (en) | Alignment device in a kind of large-scale drive apparatus axle | |
| CN103235394A (en) | Squirrel-cage high-precision four-dimensional adjusting mechanism and four-degree-of-freedom adjusting method thereof | |
| CN203679694U (en) | Adjustable elevator counter-weight frame assembly fixture | |
| CN108247555B (en) | Flexural pivot clamping and stress monitor device and method based on big component flexible docking | |
| CN104701632A (en) | Assembly adjusting method and device of panel sub-unit of radio telescope reflective face unit |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160302 Termination date: 20170628 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |