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

Space expandable exposure experiment platform based on Mard mechanism

An exposure experiment and space technology, applied in the field of space expandable exposure experiment platform, can solve the problems of low structural strength, structural failure, inconvenient transportation, etc.

Active Publication Date: 2022-06-03
TECH & ENG CENT FOR SPACE UTILIZATION CHINESE ACAD OF SCI
View PDF6 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The current exposure test platform hardly has the function of folding and unfolding, and most of them are truss structures or the outer surface of the cabin, which are limited by factors such as the position and area of ​​the load hanging point, and the rocket launch envelope.
Large-scale exposure experiment platforms are mostly rigid box-shaped structures, which are bulky and inconvenient for transportation. They require multiple launches for on-orbit modular assembly before they can be used, requiring high launch costs.
[0004] Some existing foldable space exposure platforms use memory alloys or cams to drive and unfold, which have low structural strength and cannot form effective restraint supports. For long-term exposure tests, it is easy to cause structural failure and lose support. cause test failure etc.

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
  • Space expandable exposure experiment platform based on Mard mechanism
  • Space expandable exposure experiment platform based on Mard mechanism
  • Space expandable exposure experiment platform based on Mard mechanism

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0036] The principles and features of the present invention will be described below with reference to the accompanying drawings. The examples are only used to explain the present invention, but not to limit the scope of the present invention.

[0037] like Figure 1 to Figure 7 As shown, the space deployable exposure experimental platform based on the Myard mechanism of this embodiment includes a central module 1, a lead screw nut transmission mechanism 3, a connecting rod assembly 5, a Myard mechanism 6, a driving mechanism 7 and a deployment block 21. A plurality of unfolding blocks 21 are hinged on the peripheral side edge of the module 1, a Myard mechanism 6 is hinged between two adjacent unfolding blocks 21, and at least one set of the connecting rods is connected to the inner side of each unfolding block 21. Assembly 5, the drive mechanism 7 is connected and drives the screw nut transmission mechanism 3 to drive each group of connecting rod assemblies 5 to move, and uses...

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

The invention relates to a Mard mechanism-based space expandable exposure experiment platform, which comprises a central module, a lead screw nut transmission mechanism, a connecting rod assembly, Mard mechanisms, a driving mechanism and expansion blocks, and is characterized in that a plurality of expansion blocks are hinged to the peripheral edge of the central module, and a Mard mechanism is hinged between every two adjacent expansion blocks; the inner side face of each unfolding block is connected with at least one connecting rod assembly, the driving mechanism is connected with the lead screw nut transmission mechanism and drives the lead screw nut transmission mechanism to drive the connecting rod assemblies to move, and the unfolding blocks and the Myard mechanisms are driven by the connecting rod assemblies to be folded and unfolded synchronously. According to the exposure experiment platform, the unfolding block and the Myard mechanism are folded and unfolded through cooperation of the lead screw nut transmission mechanism and the connecting rod assembly, the exposure experiment platform is folded towards the center when folded, smaller launching space is occupied, the surface area for exposure experiments can be effectively increased when the exposure experiment platform is unfolded, the number of exposure experiments can be increased, and the development efficiency is improved. And a relatively large folding and unfolding ratio is realized.

Description

technical field [0001] The invention relates to the technical field of space exposure, in particular to a space deployable exposure experiment platform based on a Myard mechanism. Background technique [0002] The demand for space missions is gradually increasing, and the structure size of the corresponding spacecraft is getting larger and larger, but this contradicts the carrying space and capability of the rocket. The deployable mechanism can complete the transformation from the folded state to the unfolded state under the control of the command, and After deployment, it has a large envelope size and a certain stiffness, and can carry a specified load mechanism. Therefore, a deployable mechanism with a folding and unfolding function can be selected to solve this problem. [0003] Space exposure experiment is an important way to explore space science. The premise of conducting extravehicular exposure experiment is that the spacecraft must provide an exposure experiment plat...

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
IPC IPC(8): B64G1/22B64G1/66
CPCB64G1/222B64G1/66
Inventor 赵冲孙惠泽赵海峰王珂张璐洪逸伦
Owner TECH & ENG CENT FOR SPACE UTILIZATION CHINESE ACAD OF SCI
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