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

Stationary orbit ultra-large type assemblable satellite platform configuration and on-orbit assembly method

A geostationary orbit and satellite platform technology, applied in the field of spacecraft, can solve the problems of inapplicable assembleable satellite platforms, limited on-orbit scale, and inability to assemble on-orbit, achieving high energy utilization efficiency, open platform configuration space, and favorable The effect of satellite attitude control

Active Publication Date: 2020-07-17
SHANGHAI SATELLITE ENG INST
View PDF10 Cites 9 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] After searching the existing technology, the patent document CN103863577A discloses a frame-plate satellite configuration and a modular satellite. The platform adopts a modular design, but this patent can only meet the configuration design of a single satellite platform and cannot be assembled in orbit; Another example is the patent document CN105501471A which discloses a satellite configuration loaded with a large-scale deployable antenna with double reflectors. The platform is designed for large-scale application satellites. Assemblable satellite platform applicable to the present invention

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
  • Stationary orbit ultra-large type assemblable satellite platform configuration and on-orbit assembly method
  • Stationary orbit ultra-large type assemblable satellite platform configuration and on-orbit assembly method
  • Stationary orbit ultra-large type assemblable satellite platform configuration and on-orbit assembly method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0052] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0053] The invention provides a geostationary orbit ultra-large assembling satellite platform configuration, such as figure 1As shown, including the mother platform 1, which is the control center of the whole star, the mother platform is responsible for the resource and task management and control of the whole star, and is the core part of the platform; the transition sub-platform Ⅰ and transition sub-platform Ⅱ are respectively connected to the mother platform 1 through the connecting device Connection...

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 provides a stationary orbit ultra-large type assemblable satellite platform configuration, which belongs to the technical field of spacecrafts, and comprises a mother platform, a transition sub-platform I and a transition sub-platform II, a functional sub-platform I and a functional sub-platform II, a functional sub-platform III and a functional sub-platform IV, an energy module I and an energy module II, and a mechanical arm I and a mechanical arm II, wherein the mother platform is a control center of a whole satellite; the transition sub-platform I and the transition sub-platform II are respectively connected with the mother platform through connecting devices; the functional sub-platform I and the functional sub-platform II are respectively connected with the transition sub-platform I through connecting devices; the functional sub-platform III and the functional sub-platform IV are respectively connected with the transition sub-platform II through connecting devices; the energy module I and the energy module II are respectively connected with the transition sub-platform I and the transition sub-platform II through connecting devices to supply power; the mechanicalarm I and the mechanical arm II are installed on the transition sub-platform I and the transition sub-platform II correspondingly to execute an on-orbit assembling task. The platform configuration issuitable for expansion, can adapt to on-orbit construction of large satellites with the on-orbit flight weight of 10-20 t, is applied to various types of satellites and service stations, and is wide in application range.

Description

technical field [0001] The invention relates to the technical field of spacecraft, in particular to a geostationary orbit ultra-large assembleable satellite platform configuration and an on-orbit assembly method. Background technique [0002] With the development of satellite application level, the importance of satellite to national defense technology and national economy and people's livelihood is increasing day by day. In recent years, major aerospace countries have continued to increase their investment in the aerospace industry, and the number of satellite launches has been increasing year by year, with an average annual increase of more than 20% in the number of global satellite launches. Geostationary orbit satellites cause the particularity of the orbit, and play an extremely important role in the fields of global communication, relay, and earth observation. However, geostationary orbit resources are very scarce, and my country's high-orbit satellites will face incr...

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 Applications(China)
IPC IPC(8): B64G1/10B64G1/22
CPCB64G1/10B64G1/1007B64G1/22
Inventor 李文龙孔祥龙杨丽丽许浩钱勇陈昌亚王智磊
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