High-stable and semi-flexible supporting structure for secondary lens of space camera
A support structure and space camera technology, applied in the field of aerospace optical remote sensing cameras, can solve the problems of poor static performance, large acceleration response multiple, low stiffness, etc., achieve high stiffness and small mass, eliminate influence, and ensure stability.
Active Publication Date: 2015-02-25
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
View PDF5 Cites 11 Cited by
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
[0003] The traditional rigid connection structure has high rigidity and good static performance. However, due to the small damping, this structure has a large acceleration response multiple and a large force on the installation point of the secondary mirror assembly, which makes it difficult to wi
Method used
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View moreImage
Smart Image Click on the blue labels to locate them in the text.
Smart ImageViewing Examples
Examples
Experimental program
Comparison scheme
Effect test
Example Embodiment
[0020] The high-stability semi-flexible support structure for the secondary mirror of a space camera according to the present invention will be described in further detail below with reference to the accompanying drawings and specific embodiments.
[0021] Such as Figure 1-Figure 7c As shown, the high-stability semi-flexible support structure for the secondary lens of a space camera according to the present invention includes a secondary lens holder frame 2, three supporting rods 3, and three supporting seats 4. Among them, the secondary lens holder frame 2 is a ring frame, and the secondary lens 1 is glued and fixed on the secondary lens holder frame 2. The three supporting rods 3 are evenly distributed on the secondary lens holder frame 2, the first end of each supporting rod 3 is fixed on the secondary lens holder frame 2 along the tangent direction of the secondary lens 1, and the three supporting rods 3 are located on the secondary lens holder. 1 The back of the reflective ...
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more PUM
Login to view more Abstract
A high-stable and semi-flexible supporting structure for a secondary lens of a space camera comprises a secondary lens bearing frame, three supporting rods and three supporting bases. The secondary lens is fixed to the secondary lens bearing frame in an adhesive connection mode. The three supporting rods are uniformly distributed on the secondary lens bearing frame and located on the back side of the reflecting surface of the secondary lens, the first end of each supporting rod is fixed to the secondary lens bearing frame in the tangential direction of the secondary lens, and the second end of each supporting rod is connected to one corresponding supporting base. The supporting bases are connected to a front lens tube through screws. According to the high-stable and semi-flexible supporting structure, bolt rigid connection is adopted for the front segments of the connecting parts of the supporting bases and the supporting rods, structural adhesive and damping adhesive flexible connection is adopted for the rear segments of the connecting parts of the supporting bases and the supporting rods, and semi-flexible spring structures are arranged between the supporting bases and the supporting rods. Compared with a full-rigid connection structure or a full-flexible connection structure, the high-stable and semi-flexible supporting structure has high dynamic rigidity, static rigidity, damping properties and stability and meets the space environment use requirement of a secondary lens assembly of the large-aperture coaxial three-lens camera.
Description
technical field [0001] The invention belongs to the technical field of aerospace optical remote-sensing cameras, and in particular relates to a supporting structure for supporting secondary mirrors of large-caliber optical coaxial three-mirror cameras in aerospace. Background technique [0002] The secondary mirror assembly of the aerospace large-aperture optical coaxial three-mirror camera is suspended on the front lens barrel by a rod support, and because it is farthest from the installation base of the camera and the satellite, the secondary mirror and its supporting structure are subjected to the worst mechanical environment , in order to ensure that the secondary mirror can experience the emission vibration environment and is stable and reliable, the connection structure between the secondary mirror assembly and the installation interface must have good dynamic performance and high stability at the same time. [0003] The traditional rigid connection structure has high ...
Claims
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more Application Information
Patent Timeline
Login to view more IPC IPC(8): G03B17/12G02B7/00G02B7/02
CPCG02B7/00G02B7/022G03B17/12
Inventor 罗世魁陈芳曹东晶潘宁贤史娇红吴杰宗肖颖张建国
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
Who we serve
- R&D Engineer
- R&D Manager
- IP Professional
Why Eureka
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Social media
Try Eureka
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap