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

A space load assembly mechanism and a space load unfolding and retracting device

An assembly mechanism and load technology, applied to fixed devices, motor vehicles, mechanical equipment, etc., can solve the problems of unsatisfactory long-term scalability, replaceable load, and difficult replacement, and achieve good maintainability, convenient replacement, and environmental adaptability strong effect

Active Publication Date: 2022-04-19
TECH & ENG CENT FOR SPACE UTILIZATION CHINESE ACAD OF SCI
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] At present, space science experiment loads are generally installed directly on the ground on the launch platform, and are fastened by bolts, which are not easy to replace in orbit, and do not meet the needs of long-term expandable and replaceable loads.

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 space load assembly mechanism and a space load unfolding and retracting device
  • A space load assembly mechanism and a space load unfolding and retracting device
  • A space load assembly mechanism and a space load unfolding and retracting device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0045] Such as Figure 1 to Figure 7 As shown, a load assembly mechanism of this embodiment includes a load body 200 and an unfolding platform 100, one side of the unfolding platform 100 is provided with a first stepped structure 124, and the horizontal stepped surface 130 of the first stepped structure 124 There is a guide post on it, and one end of the unfolding platform 100 is provided with a limit wall 128, and the limit wall 128 is provided with a captive screw 129, and the limit wall 128 is provided with an elastic limit piece 145; The bottom side of the load body 200 is provided with a second stepped structure 201 adapted to the first stepped structure 124, and the horizontal stepped surface 130 of the second stepped structure 201 is provided with a guide adapted to the guide column. hole, the bottom end surface of the load body 200 is provided with a second limiting groove 140 and a screw hole adapted to the elastic limiting member 145 .

[0046] Such as Figure 6 an...

Embodiment 2

[0055] Such as Figure 8 ~ Figure 11 As shown, a space load deployment device of this embodiment includes the load assembly mechanism described in Embodiment 1, and also includes a deployment drive mechanism and a locking mechanism, and at least two of the deployment platforms 100 are hinged sequentially through hinges 122 The power part of the unfolding drive mechanism is installed on one of the two adjacent unfolding platforms 100, and the transmission gear 104 of the unfolding drive mechanism is rotatably connected to the hinges 122 of the two adjacent unfolding platforms 100. and connected with another deployment platform 100; the locking mechanism includes a latch 125 and a locking assembly 126, and the latch 125 and locking assembly 126 are respectively installed on two adjacent deployment platforms 100 The upper end face of the limiting wall 128; the power part of the unfolding drive mechanism is connected with the transmission gear 104 and drives the transmission gear ...

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 load assembly mechanism and a space load unfolding and retracting device. The load assembly mechanism includes a load body and an unfolding platform. One side of the unfolding platform is provided with a first stepped structure, and a guide column is arranged on the horizontal stepped surface of the first stepped structure. , one end of the unfolding platform is provided with a limit wall, the limit wall is provided with a captive screw, and the limit wall is provided with an elastic limit piece; the bottom side of the load body is provided with a second ladder adapted to the first ladder structure structure, the horizontal step surface of the second ladder structure is provided with a guide hole adapted to the guide column, and the end surface of the bottom end of the load body is provided with a limit groove and a screw hole adapted to the elastic limiter. The assembly of the load body and the unfolding platform is stable and reliable. The guide column is used for guidance and positioning, and the elastic limiter is used to limit the position. Finally, the captive screw is used for locking and positioning. The disassembly and installation of the load body are convenient and reliable. The need for long-term scalability and replaceable payloads.

Description

technical field [0001] The invention relates to the related technical field of space load assembly, in particular to a space load assembly mechanism and a space load unfolding and retracting device. Background technique [0002] With the development of space science and space technology and the continuous exploration of space by human beings, more and more space experiments need to be carried out. Especially with the completion of the space station and the explosive growth of the number of satellite launches, the types of space motion devices that space science experiment loads need to rely on are developing in the direction of diversification, basicity, long life, and scalability. Space launch missions have the characteristics of shortage of launch volume, launch weight, power supply, and communication resources. The space environment has environmental characteristics such as high and low temperature alternating, high vacuum, strong radiation, and space debris impact. The ...

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): B64G1/22F16B1/02F16C11/04F16C11/10
CPCB64G1/222F16C11/04F16C11/10F16B1/02
Inventor 刘立坤王珂张璐张聚乐王绍坤盛强乔志宏吕从民
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

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com