Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

A variable frequency damping support device for a space camera

A space camera and support device technology, applied in the field of aerospace optical remote sensors, can solve problems such as system complexity, uneconomical use, image distortion, etc., and achieve the effect of small size, strong adaptability, and light weight

Active Publication Date: 2019-03-12
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The first form is adaptable to the unevenness of the camera assembly surface, but it cannot suppress the micro-vibration within 60Hz in orbit, and even the suppression effect is not obvious at around 100Hz, and it will cause obvious image distortion during the whole-satellite mobile imaging. The second form has higher requirements on the camera assembly surface, the system is relatively complicated, and needs to introduce pyrotechnics, which is not economical in use

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 more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • A variable frequency damping support device for a space camera
  • A variable frequency damping support device for a space camera
  • A variable frequency damping support device for a space camera

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0026] A variable frequency damping support device for a space camera such as Figure 1 ~ Figure 2 As shown, it includes upper hinge plate 1, outer connecting rod, steel wire retaining ring for hole 4, joint bearing 5, pin shaft 6, inner connecting rod 7, damping rubber layer 8, partition plate 9, lower hinge plate 10, rigidity rubber layer 11, steel wire retaining ring 12 for shaft. Among them, the outer connecting rod, the joint bearing 5, the inner connecting rod 7, the damping rubber layer 8, the partition plate 9, and the rigidity rubber layer 11 are its core components.

[0027] Such as image 3 (a), image 3 As shown in (b), the outer connecting rod includes an outer connecting rod one 2 and an outer connecting rod two 3; the outer connecting rod one 2 is cylindrical, and the end of the cylinder has an installation ring that cooperates with the joint bearing 5 and the pin shaft 6; The connecting rod 2 3 is cylindrical, and the end of the cylinder has two parallel mou...

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

No PUM Login to View More

Abstract

A frequency-variable damping support device for a space camera, comprising an upper hinge plate (1) and the like. The upper hinge (1) and the lower hinge (10) are respectively connected to the outer connecting rods (outer connecting rod one (2), outer connecting rod two (3)) and inner connecting rods through joint bearings (5) and pin shafts (6). The rods (7) are connected, and the damping rubber layer (8) is filled between the outer connecting rod one (2), the outer connecting rod two (3) and the inner connecting rod (7). ) to create a controllable structural gap between the first outer link (2), the second outer link (3) and the inner link (7), finally realizing the support for the camera. Through the design of the gap, the present invention enables the camera to exhibit frequency conversion characteristics of three different frequencies under small-scale vibration, launch section vibration, and on-orbit weightlessness, which not only ensures the effect of large damping and vibration reduction, but also solves the problem of satellite structure on-orbit microscopic The impact of vibration on camera imaging.

Description

technical field [0001] The invention belongs to the technical field of aerospace optical remote sensors, and relates to a space camera support device, in particular to a frequency-variable damping support device. Background technique [0002] With the development of aerospace remote sensing technology, remote sensing cameras are constantly becoming larger and lighter, and the technical indicators of cameras are constantly improving, and the requirements for satellite platforms are becoming more and more stringent. Limited by processing technology, the flatness of the camera assembly surface on the satellite platform can no longer meet the requirements of the current camera. When the satellite is in orbit, the problem of camera image distortion caused by dynamic flutter of moving parts is also becoming more and more prominent. With the weight of the camera With the improvement of the camera, the tolerance of the camera to the vibration environment of the transmission section ...

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
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): F16M11/06F16F15/08F16F3/093G03B17/56
CPCG03B17/56F16F3/093F16F15/08F16M11/06F16F2224/025F16F2232/08F16M2200/04
Inventor 罗世魁高超史姣红王先炉邱军晖刘子嘉董科
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products