CN102705657A - Flexible support frame for small high-stability multifunctional optical reflector - Google Patents

Flexible support frame for small high-stability multifunctional optical reflector Download PDF

Info

Publication number
CN102705657A
CN102705657A CN2012101994551A CN201210199455A CN102705657A CN 102705657 A CN102705657 A CN 102705657A CN 2012101994551 A CN2012101994551 A CN 2012101994551A CN 201210199455 A CN201210199455 A CN 201210199455A CN 102705657 A CN102705657 A CN 102705657A
Authority
CN
China
Prior art keywords
platform
ray machine
supporting frame
flexible supporting
flexible support
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.)
Granted
Application number
CN2012101994551A
Other languages
Chinese (zh)
Other versions
CN102705657B (en
Inventor
闫勇
金光
安源
姚劲松
贾学志
张雷
王栋
谷松
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.)
Chang Guang Satellite Technology Co Ltd
Original Assignee
Changchun Institute of Optics Fine Mechanics and Physics of CAS
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 Changchun Institute of Optics Fine Mechanics and Physics of CAS filed Critical Changchun Institute of Optics Fine Mechanics and Physics of CAS
Priority to CN201210199455.1A priority Critical patent/CN102705657B/en
Publication of CN102705657A publication Critical patent/CN102705657A/en
Application granted granted Critical
Publication of CN102705657B publication Critical patent/CN102705657B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention relates to a flexible support frame for a small high-stability multifunctional optical reflector, and belongs to the technical field of space optics. The problems that the conventional supporting mechanism is only applicable to reflectors made of the same material, and the purposes and the size of the conventional supporting mechanism are limited are solved. The flexible support frame has a rectangular structure comprising a hollow circle, mechanical connecting platforms which are equal in width and have rectangular bump structures are processed on two sides of the flexible support frame, two mechanical connectors are respectively processed at two ends of each mechanical connecting platform, an optical machine connecting platform which has an annular bump structure is processed along the hollow circle, a recess structure is processed at the bottom of the optical machine connecting platform, an unloading base plate which has a sinking structure is processed between each mechanical connecting platform and the optical machine connecting platform, and an unloading slit which has a circular topological structure is processed on each unloading base plate. The flexible support frame is designed integrally, and is wide in application range and high in applicability, and the safety and the reliability of the flexible support can be increased.

Description

The flexible supporting frame of small-sized high stable multifunctional optical reflector
Technical field
The invention belongs to the flexible supporting frame of a kind of small-sized high stable multifunctional optical reflector that relates in the space optics technical field.
Background technique
Flexible supporting frame is to be out of shape a kind of passive regulation structure of isolating or reducing because of factors such as operating ambient temperature variation, erection stresses optical reflecting mirror shape precision to be had a negative impact through flexible link.That this class formation has is simple in structure, it is sluggish not have, do not have the advantage of the influence of the various rugged environment of creeping, can stand the space, is widely used at present in the supporting structure of reflective optic reflector in the space optics load.
Current, space reflection formula optical mirror all adopts flexible structure to realize the supported design of highi degree of accuracy, high stable.The prior art the most approaching with the present invention; Be U.S. Paul R.Yoder, Jr. work Opto-Mechanical Systems Design (optical-mechanical system design, the third edition; Zhou Haixian, Cheng Yunfang translates) the flexible support device of metallic mirror shown in the 604th page of Figure 13-55.The maximum shortcoming of this flexible structure is that it is only applicable to reflector and supporting structure is the integrated design of metallic material of the same race; The purposes of flexible structure and size are seriously limited; And this kind flexible structure complicacy; Difficulty of processing is big, cost is high, the cycle is long, is unfavorable on a large scale, large batch of use.
Summary of the invention
Be only applicable to the same material reflector in order to solve above-mentioned supporting mechanism; Purposes and size-constrained problem the invention provides the flexible supporting frame of a kind of small-sized high stable multifunctional optical reflector, comprising: flexible supporting frame; Flexible supporting frame is the rectangular configuration that contains the hollow circle; The rectangular boss construction machine that both sides process equal width connects platform, and the two ends of mechanical connection platform respectively process two mechanical interfaces, connects platform along hollow circle processing annular boss structure ray machine; Ray machine connect platform bottom surface processing concave volume structure; Processing concave volume structure is unloaded carried base board between mechanical connection platform and the ray machine connection platform, unloads the unloading slit of processing circular topology structure on the carried base board, the topological structure axes O 1O 1' being connected the platform axis coaxle with ray machine, the unloading slit is divided into internal layer and outer two-part, and internal layer is connected platform and connects with ray machine, and skin is connected with the mechanical connection platform, the line O of center of arc everywhere of outer unloading slot ends 2O 2' and O 3O 3' be mutually 90 ° of angles and hand in the ray machine connection platform O of center of arc 0, the ray machine interface is positioned at ray machine with pin hole and is connected on the platform, and the ray machine interface is 90 ° of distributions, the pin hole line of centres and axes O 2O 245 ° of angles of ' one-tenth; Internal layer unloading slit is divided into five groups, and to be mutually 180 ° of angles unloading slit at interval be one group, and its terminal line of center of arc everywhere all intersects at ray machine and connects the platform O of center of arc 0
Good effect of the present invention:
1. the integrated form design that adopts of this flexible supporting frame metallic absorption supporting structure different from the past; This flexible supporting frame is the split type design that is connected with mirror body; Applicable to the support requirement of material space reflectors such as metal, glass, SiC, Applicable scope is wider, and adaptability is stronger;
2. the selection of this flexible supporting frame material therefor is more versatile and flexible; Can be according to what of the quality of the difference of mirror base, Environmental Conditions, processing cost; Select heat to mate the structural material better, that intensity is better, workability is good, the more convenient and saving of feasible design and course of working;
3. this flexible support frame structure is simple; It is extremely easy to process, and has avoided the caused manufacturing difficult problem of integrated structure, can significantly reduce the structural member processing cost; Shorten the process-cycle; The processing mode of this supporting frame flexible structure simplicity can improve its Security and reliability greatly simultaneously, and this is an extremely important performance assessment criteria in the development of space item;
4. this flexible support frame structure and size are not limited by reflector; The design variable simple controllable; Especially the design of axial dimension is comparatively flexible; Can be suitable for the supported design requirement of the more harsh optical mirror of axial carrying requirement, also can satisfy the usage requirement of optical mirror bearing of optical axis high stability simultaneously;
5. this flexible supporting frame has adopted split type plane structure; Under the prerequisite that satisfies the usage requirement of optical mirror supporting structure high stability; The structure axial dimension is shortened, reduced the axial dimension constraint restriction of optical system, be very suitable for the small light designing requirement of structure.
Description of drawings
Fig. 1 is the structural representation of the flexible supporting frame of small-sized high stable multifunctional optical reflector;
Fig. 2 is the sectional view of the flexible supporting frame of small-sized high stable multifunctional optical reflector;
Fig. 3 is that the flexible supporting frame of small-sized high stable multifunctional optical reflector is connected schematic representation with metallic absorption/SiC reflector screw;
Fig. 4 is that the flexible supporting frame of small-sized high stable multifunctional optical reflector is connected schematic representation with the glass reflector gummed;
Fig. 5 is small-sized flexible supporting frame of high stable multifunctional optical reflector and glass reflector cemented surface sectional view;
Embodiment
Below in conjunction with accompanying drawing the present invention is further described:
Embodiment one
Shown in Fig. 1-2, the flexible supporting frame of small-sized high stable multifunctional optical reflector comprises: flexible supporting frame 8; Flexible supporting frame 8 is for containing the rectangular configuration of hollow circle; The rectangular boss construction machine that both sides process equal width connects platform 5, and the two ends of mechanical connection platform 5 respectively process two mechanical interfaces 1, connects platform 7 along hollow circle processing annular boss structure ray machine; Ray machine connects 7 bottom surface processing concave volume structure of platform; Processing concave volume structure is unloaded carried base board 6 between mechanical connection platform 5 and the ray machine connection platform 7, unloads the unloading slit 3 of processing circular topology structure on the carried base board 6, the topological structure axes O 1O 1' being connected platform 7 axis coaxles with ray machine, unloading slit 3 is divided into internal layer and outer two-part, and internal layer is connected platform 7 and connects with ray machine, and skin is connected with mechanical connection platform 5, the line O of center of arc everywhere of outer unloading slot ends 2O 2' and O 3O 3' be mutually 90 ° of angles and hand in ray machine connection platform 7 O of center of arc 0, ray machine interface 2 is positioned at ray machine with pin hole 4 and is connected on the platform 7, and ray machine interface 2 is 90 ° of distributions, pin hole 4 lines of centres and axes O 2O 245 ° of angles of ' one-tenth; Internal layer unloading slit is divided into five groups, and to be mutually 180 ° of angles unloading slit at interval be one group, and its terminal line of center of arc everywhere all intersects at ray machine and connects platform 7 O of center of arc 0 Mechanical connection platform 5 is connected platform 7 with ray machine convex surface is in the same plane, and the concave volume structure that ray machine connects the processing of platform 7 bottom surfaces is identical with the recessed height that unloads carried base board 6.
As shown in Figure 3, flexible supporting frame 8 and optical mirror 9 are connected through screw, and optical mirror 9 is metallic absorption or SiC reflector.
As shown in Figure 4, flexible supporting frame 8 is connected through gummed with optical mirror 9, and optical mirror 9 is a glass mirror.
As shown in Figure 5, when optical mirror 9 is glass mirror, the sectional view that flexible supporting frame 8 is connected with optical mirror 9 gummeds.
Embodiment two
Flexible supporting frame 8 adopts with optical mirror 9 and divides body structure; Workability and versatility have been increased; When optical mirror is metal or SiC material, is connected between flexible supporting frame and the optical mirror 9 and is connected platform 7 with ray machine through ray machine interface 2, pin hole 4 and connects, what pin hole 4 guaranteed that ray machines connect platforms 7 and optical mirror 9 is connected Location accuracy and repetition installing and locating precision; Unloading 6 pairs of mechanical connection platforms 5 of carried base board is connected erection stress and the thermal stress that platform 7 produces and has carried out even distribution with ray machine; Prevent concentrating of stress, and be divided into internal layer and outer two-part that internal layer is connected platform 7 and connects with ray machine at the unloading slit 3 that unloads on the carried base board 6; Skin is connected with mechanical connection platform 5; The big flexible deformation of these two-part zone can prevent that its mechanical connection platform 5 is connected the direct transmission of 7 stress abilities of platform with ray machine with intercepting at non-key position than macrostructure internal stress or thermal stress on the one hand, avoids the big stress can be to the influence of reflector precision stability as far as possible; Flexible deformation that on the other hand can be through self structure connects structural stress residual between the platform 7 or thermal stress with mechanical connection platform 5 and ray machine and changes structural energy into and store; Increased the adaptability and the stability of reflector, simultaneously because unloading slit 3 is the circular topology structure, its topological structure axes O 1O 1' be connected platform 7 axis coaxles with ray machine, so connecting platform 7, the ray machine that is connected with internal layer unloading slit has around unloading slit 3 central axis O 1O 1' rotating micro-displacement can carry out the micrometric displacement compensation to the torsional moment that is caused by mechanical connection platform 5, and the antitorque adaptability of this supporting frame is strengthened, and has improved the stability of reflector.This supporting frame ray machine connects platform 7 and has designability along axial direction thickness; Selection through to its thickness can provide suitable axial rigidity; Satisfy the rigidity requirement vertically of this flexible supporting frame, and its rigidity perpendicular to axial direction can obtain equally through suitable selection unloading slit 3 is connected platform 7 with ray machine connection section area, this structure can satisfy big rigidity requirement; General its single order resonant frequency can be higher than 300Hz, and the acclimation to heat scope can reach ± and 15 ℃.
When optical mirror is glass material; The cylinder of hollow circle contacts the cylndrical surface and carries out size and join car on the flexible supporting frame 8 with optical mirror 9; Matching gap is between 0.01 ~ 0.015mm, flexible then supporting frame 8 and optical element contact position facing-up, guarantee both area of contact>85% after; After evenly being coated with optics epoxy glue GHJ-01 (Z) on both contact position, be adhesively fixed, the thermal expansion coefficient of flexible supporting frame 8 needs to be complementary with the thermal expansion coefficient of optical mirror 9.
Embodiment three
Flexible supporting frame 8 material therefors can be selected invar (Invar) material that is complementary with optical mirror 9 material therefor thermal expansion coefficient for use; Reduce heat to greatest extent and does not match, or select that tensile strength is higher, the better titanium alloy material of processibility for use the influence of optical mirror minute surface face shape.
It is the structural member material that this flexible supporting frame is selected the invar (Invar) of Beijing material development in science and technology Co., Ltd of the aerospace Yin Dynasty or the titanium alloy (TC4) of Shenyang Inst. of Metals, Chinese Academy of Sciences for use; In concrete course of working, carrying out repeatedly vacuum aging handles; Two-layer unloading slit 3 all adopts the mode of the silk of being careful to carry out the line cutting process inside and outside this flexible supporting frame, strict control surface quality of workpieces, claimed structure spare smooth surface, no tool marks; The cross-section that particularly unloads slit requires its surface finishment at 0.6-0.9; Do not have the processing tool marks, with the transition of fillet nature, avoid forming stress and concentrate in structural member corner.
Mechanical connection platform 5 is connected platform 7 with ray machine connection face is in the same plane, plane working surface shape required precision≤0.003mm, the optical axis verticality≤0.01mm of plane and optical mirror.Unload carried base board 6 and the ray machine of flexible supporting frame connect platform 7 and adopt the staggered floor design in the axial direction, and the structure axial dimension is shortened, and have increased the parameter of design, select suitable axial parameter can obtain different axial rigidities and axial micrometric displacement benefit RepayEffect under the prerequisite that satisfies the usage requirement of optical mirror supporting structure high stability, has reduced the axial dimension constraint restriction of optical system, is very suitable for the small light designing requirement of structure.

Claims (3)

1. the flexible supporting frame of small-sized high stable multifunctional optical reflector; Comprise: flexible supporting frame (8); It is characterized in that flexible supporting frame (8) is for containing the rectangular configuration of hollow circle, both sides process the mechanical connection platform (5) of the rectangular boss structure of equal width; The two ends of mechanical connection platform (5) respectively process two mechanical interfaces (1); Ray machine along hollow circle processing annular boss structure connects platform (7), and ray machine connects the bottom surface processing concave volume structure of (7) of platform, mechanical connection platform (5) and ray machine connect process the concave volume structure between the platform (7) unload carried base board (6); Unload carried base board (6) and go up the unloading slit (3) of processing circular topology structure, topological structure axes O 1O 1' being connected platform (7) axis coaxle with ray machine, unloading slit (3) is divided into internal layer and outer two-part, and internal layer is connected platform (7) and connects with ray machine, and skin is connected with mechanical connection platform (5), the line O of center of arc everywhere of outer unloading slot ends 2O 2' and O 3O 3' be mutually 90 ° of angles and intersect at ray machine connection platform (7) O of center of arc 0, ray machine interface (2) is positioned at ray machine with pin hole (4) and is connected on the platform (7), and ray machine interface (2) is 90 ° of distributions, pin hole (4) line of centres and axes O 2O 245 ° of angles of ' one-tenth; Internal layer unloading slit is divided into five groups, and to be mutually 180 ° of angles unloading slit at interval be one group, and its terminal line of center of arc everywhere all intersects at ray machine and connects platform (7) O of center of arc 0, five groups of internal layer slits are in the O with center of arc 0On the circumference of concentric.
2. according to the flexible supporting frame of the said small-sized high stable multifunctional optical reflector of claim 1, it is characterized in that mechanical connection platform (5) is connected platform (7) with ray machine convex surface is in the same plane.
3. according to the flexible supporting frame of the said small-sized high stable multifunctional optical reflector of claim 1, it is characterized in that the concave volume structure that ray machine connects the processing of platform (7) bottom surface is identical with the recessed height that unloads carried base board (6).
CN201210199455.1A 2012-06-15 2012-06-15 Flexible support frame for small high-stability multifunctional optical reflector Active CN102705657B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210199455.1A CN102705657B (en) 2012-06-15 2012-06-15 Flexible support frame for small high-stability multifunctional optical reflector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210199455.1A CN102705657B (en) 2012-06-15 2012-06-15 Flexible support frame for small high-stability multifunctional optical reflector

Publications (2)

Publication Number Publication Date
CN102705657A true CN102705657A (en) 2012-10-03
CN102705657B CN102705657B (en) 2014-10-15

Family

ID=46898632

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210199455.1A Active CN102705657B (en) 2012-06-15 2012-06-15 Flexible support frame for small high-stability multifunctional optical reflector

Country Status (1)

Country Link
CN (1) CN102705657B (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106324789A (en) * 2016-10-26 2017-01-11 中国科学院长春光学精密机械与物理研究所 Universal large-aperture rigid bearing-type quick reflecting mirror
CN106371190A (en) * 2015-07-23 2017-02-01 肖特股份有限公司 A monolithic support for overall supporting of a workpiece
CN106443959A (en) * 2016-12-07 2017-02-22 中国科学院长春光学精密机械与物理研究所 Split type bi-material flexible mechanism of space-based large-calibre high-facial-contour-precision reflector assembly
CN108227113A (en) * 2016-12-10 2018-06-29 中国科学院长春光学精密机械与物理研究所 For the adjustment of mirror optics element angle and the device and method of aberration compensation
KR20180106962A (en) * 2017-03-17 2018-10-01 루미리즈 홀딩 비.브이. Led lighting arrangement
CN109799594A (en) * 2019-03-21 2019-05-24 长光卫星技术有限公司 A kind of flexible mandrel for eliminating large caliber reflecting mirror adhesive stress
CN110087950A (en) * 2017-01-10 2019-08-02 金泰克斯公司 Ball-collecting rack component for vehicle
CN110231691A (en) * 2019-07-18 2019-09-13 长光卫星技术有限公司 A kind of intersection hinge type flexible support structure

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1243262A (en) * 1999-06-18 2000-02-02 中国科学院上海技术物理研究所 Support device for large-aperture optical main mirror for space use
JP2001133704A (en) * 1999-11-05 2001-05-18 Sony Corp Optical axis correcting device
CN101566718A (en) * 2009-06-05 2009-10-28 中国科学院长春光学精密机械与物理研究所 Flexible supporting structure for the back of reflecting mirror
CN102073123A (en) * 2010-12-27 2011-05-25 中国科学院长春光学精密机械与物理研究所 Single-point supporting flexible section for small-aperture reflecting mirror of space optical remote sensor
CN102262281A (en) * 2011-08-02 2011-11-30 中国科学院长春光学精密机械与物理研究所 Flexible supporting mechanism for space remote sensor reflector

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1243262A (en) * 1999-06-18 2000-02-02 中国科学院上海技术物理研究所 Support device for large-aperture optical main mirror for space use
JP2001133704A (en) * 1999-11-05 2001-05-18 Sony Corp Optical axis correcting device
CN101566718A (en) * 2009-06-05 2009-10-28 中国科学院长春光学精密机械与物理研究所 Flexible supporting structure for the back of reflecting mirror
CN102073123A (en) * 2010-12-27 2011-05-25 中国科学院长春光学精密机械与物理研究所 Single-point supporting flexible section for small-aperture reflecting mirror of space optical remote sensor
CN102262281A (en) * 2011-08-02 2011-11-30 中国科学院长春光学精密机械与物理研究所 Flexible supporting mechanism for space remote sensor reflector

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106371190A (en) * 2015-07-23 2017-02-01 肖特股份有限公司 A monolithic support for overall supporting of a workpiece
CN106324789A (en) * 2016-10-26 2017-01-11 中国科学院长春光学精密机械与物理研究所 Universal large-aperture rigid bearing-type quick reflecting mirror
CN106443959A (en) * 2016-12-07 2017-02-22 中国科学院长春光学精密机械与物理研究所 Split type bi-material flexible mechanism of space-based large-calibre high-facial-contour-precision reflector assembly
CN108227113A (en) * 2016-12-10 2018-06-29 中国科学院长春光学精密机械与物理研究所 For the adjustment of mirror optics element angle and the device and method of aberration compensation
CN110087950A (en) * 2017-01-10 2019-08-02 金泰克斯公司 Ball-collecting rack component for vehicle
CN110087950B (en) * 2017-01-10 2023-01-31 金泰克斯公司 Ball rack assembly for vehicle
KR20180106962A (en) * 2017-03-17 2018-10-01 루미리즈 홀딩 비.브이. Led lighting arrangement
CN108626586A (en) * 2017-03-17 2018-10-09 亮锐控股有限公司 LED light device
CN108626586B (en) * 2017-03-17 2021-11-23 亮锐控股有限公司 LED lighting device
KR102543885B1 (en) 2017-03-17 2023-06-16 루미리즈 홀딩 비.브이. Led lighting arrangement
CN109799594A (en) * 2019-03-21 2019-05-24 长光卫星技术有限公司 A kind of flexible mandrel for eliminating large caliber reflecting mirror adhesive stress
CN110231691A (en) * 2019-07-18 2019-09-13 长光卫星技术有限公司 A kind of intersection hinge type flexible support structure

Also Published As

Publication number Publication date
CN102705657B (en) 2014-10-15

Similar Documents

Publication Publication Date Title
CN102705657A (en) Flexible support frame for small high-stability multifunctional optical reflector
US20220049959A1 (en) Micro hemispherical resonator gyroscope, and an assembly method and wafer fixture
CN102200623B (en) Micro-stress assembly flexible supporting method of small-calibre micro-crystal glass material reflector
CN203551874U (en) Fast reflecting mirror system based on flexible support
US8864324B2 (en) Substrate with lightweight structure
CN103576283A (en) Rapid reflective mirror system based on flexible supports
CN101949700B (en) Laser gyro cavity length control reflecting mirror assembly
CN101566718A (en) Flexible supporting structure for the back of reflecting mirror
CN105445894A (en) Secondary mirror supporting structure
CN111045186A (en) SIC reflector with supporting reference structure
CN110187467A (en) A kind of reflecting mirror of drum structure
CN114562989B (en) Hemispherical resonant gyroscope based on optical cement connection mode
CN106019529A (en) Space aluminium-based reflector assembly
US8950879B2 (en) Laser projection module with conical reflector supported by thin walls
CN111488000B (en) Cascade amplification two-dimensional pointing adjustment device and method with embedded deflection angle sensing unit
CN103758244B (en) Inclined paralled plates buckling restrained brace
CN204086654U (en) A kind of ray machine integration silicon carbide mirror and system
CN203007132U (en) Support mechanism for double-sided ITO glass processing
CN207636831U (en) A kind of lens barrel
CN105911644B (en) A kind of optical fiber collimating apparatus and its assembly method
CN110361827B (en) Control method for reducing coupling of X axis and Y axis in two-axis quick reflector
CN209895070U (en) Reflecting mirror with I-shaped structure
CN114355554A (en) Aerospace lightweight reflector assembly and assembling method
CN104701632A (en) Assembly adjusting method and device of panel sub-unit of radio telescope reflective face unit
CN201072458Y (en) High-precision saddle type optical fiber bracket

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
C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20161201

Address after: 130000 Mingxi high tech Zone, Jilin, North Road, No. 1759, No.

Patentee after: CHANGGUANG SATELLITE TECHNOLOGY CO., LTD.

Address before: 130033 southeast Lake Road, Jilin, Changchun, No. 3888

Patentee before: Changchun Inst. of Optics and Fine Mechanics and Physics, Chinese Academy of Sci

PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: Flexible support frame for small high-stability multifunctional optical reflector

Effective date of registration: 20170718

Granted publication date: 20141015

Pledgee: Jilin nine rural commercial bank, Limited by Share Ltd Changchun branch

Pledgor: CHANGGUANG SATELLITE TECHNOLOGY CO., LTD.

Registration number: 2017220000004

PE01 Entry into force of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20210818

Granted publication date: 20141015

Pledgee: Jilin nine rural commercial bank Limited by Share Ltd. Changchun branch

Pledgor: CHANG GUANG SATELLITE TECHNOLOGY Co.,Ltd.

Registration number: 2017220000004

PC01 Cancellation of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: Flexible support frame for small high stability multifunctional optical mirror

Effective date of registration: 20211125

Granted publication date: 20141015

Pledgee: Agricultural Bank of China Limited Changchun Development Zone sub branch

Pledgor: CHANG GUANG SATELLITE TECHNOLOGY Co.,Ltd.

Registration number: Y2021220000105

PE01 Entry into force of the registration of the contract for pledge of patent right
CP03 Change of name, title or address

Address after: No. 1299, Mingxi Road, Beihu science and Technology Development Zone, Changchun City, Jilin Province

Patentee after: Changguang Satellite Technology Co.,Ltd.

Address before: No.1759 Mingxi Road, Gaoxin North District, Changchun City, Jilin Province

Patentee before: CHANG GUANG SATELLITE TECHNOLOGY Co.,Ltd.

CP03 Change of name, title or address