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

On-orbit monitoring device of rope tension for spacecraft

A rope tension and monitoring device technology, applied in the direction of tension measurement, etc., can solve the problems of large weight and volume, complex conditioning circuit, heavy weight and resources, etc., and achieve the effect of simple interface, broad application prospect and strong scalability

Active Publication Date: 2015-11-18
SHANGHAI SATELLITE ENG INST
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The general general commercial force sensors at home and abroad mainly have the following problems: 1) Most of the force sensors require relatively complicated conditioning circuits, and the weight and volume are large;
[0003] 2) It is generally used as the ground, and the reliability of space use and the impact of the environment on it need special test verification;
[0004] These problems limit the use of rope tension monitoring technology on spacecraft such as spacecraft, and even limit the use of related moving parts on spacecraft
With the development trend of lightweight spacecraft, the weight of each load on the spacecraft is required to be smaller and smaller. Therefore, the general force measurement technology uses a large weight and resources.

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
  • On-orbit monitoring device of rope tension for spacecraft
  • On-orbit monitoring device of rope tension for spacecraft
  • On-orbit monitoring device of rope tension for spacecraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0026] The embodiments of the present invention are described in detail below: this embodiment is implemented under the premise of the technical solution of the present invention, and detailed implementation methods and specific operating procedures are provided. It should be noted that those skilled in the art can make some modifications and improvements without departing from the concept of the present invention, and these all belong to the protection scope of the present invention.

[0027] Such as figure 1 As shown, this embodiment provides a cable tension on-orbit monitoring device for a spacecraft, including an angular position sensor, a rack and pinion transmission assembly, a micro switch, a mounting sleeve, a compression spring, a push rod, and a roller assembly, Wherein, the rope rotates around the roller assembly, and the roller assembly is compressed by the compression spring through the push rod, the compression spring is arranged in the installation sleeve, the f...

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 discloses an on-track monitoring device for tension of a spacecraft rope. The device comprises an angular position sensor, a gear rack transmission assembly, a microswitch, an installation sleeve, a compression spring, a push rod and a roller assembly, wherein the rope rotates around the roller assembly; the roller assembly is tightly pressed by the compression spring through the push rod; the compression spring is mounted in the installation sleeve; a first end of the push rod slides inside the installation sleeve; an end part of a second end of the push rod is connected with the roller assembly; the roller assembly performs translational motion due to the change of the tension on the rope; the gear rack transmission assembly changes the translational motion of the roller assembly into rotation; the angular position sensor measures the rotation angle of the gear rack transmission assembly; and the microswitch triggers limit signals. According to the device, the problem that the tension of a rope part on the spacecraft requires to be monitored accurately is solved. At the same time, the device has the advantages of light mass, simple adjustment, small size, high security, low power consumption and the like, and the reliability and the applicability of on-track monitoring of rope tension are effectively guaranteed.

Description

technical field [0001] The invention relates to the technical field of rope mechanisms used for spacecraft movement, in particular to a rope tension on-orbit monitoring device for spacecraft. Background technique [0002] With the development of spacecraft technology, the application of moving rope components on spacecraft is becoming more and more extensive, and devices with the requirement of accurately monitoring the tension of ropes are also produced. The general general commercial force sensors at home and abroad mainly have the following problems: 1) Most of the force sensors require relatively complicated conditioning circuits, and the weight and volume are large; [0003] 2) It is generally used as the ground, and the reliability of space use and the impact of the environment on it need special test verification; [0004] These problems limit the use of rope tension monitoring technology on spacecraft such as spacecraft, and even limit the use of related moving part...

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): G01L5/10
Inventor 周徐斌薛景赛王智磊王萌杜三虎
Owner SHANGHAI SATELLITE ENG INST
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