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Multi-star distributor force bearing structure

A distributor and load-bearing tube technology, applied in the field of aircraft, can solve the problems of structural design, complex manufacturing, and high weight of multi-satellite distributor load-bearing tubes, and achieve simple structure manufacturing and assembly, good product consistency, and reduced weight Effect

Active Publication Date: 2020-08-14
TIANJIN ISTAR-SPACE TECH CO LTD +2
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The traditional multi-satellite distributor load-bearing cylinder is generally designed as a ring frame + skin stringer structure, an overall honeycomb sandwich structure, etc. The disadvantage is that in order to ensure the rigidity of the overall structure, the weight of the multi-satellite distributor load-bearing cylinder is generally high, and the structural design , manufacturing is more complicated

Method used

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  • Multi-star distributor force bearing structure
  • Multi-star distributor force bearing structure
  • Multi-star distributor force bearing structure

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Embodiment Construction

[0051] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art.

[0052] Such as Figure 1 to Figure 12 As shown, the embodiment of the present invention proposes a load-bearing structure of a multi-star distributor, including: a load-bearing cylinder 1 with a grid structure; the grid structure is a grid structure without skin; the load-bearing cylinder The first end 11 of 1 is provided with a first inner reinforcing frame 21, and the second end 12 of the bearing cylinder 1 is provided with a sec...

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Abstract

The embodiment of the invention provides a multi-star distributor force bearing structure which comprises a force bearing cylinder with a grid structure. The grid structure is a skin-free grid structure. A first inner reinforced n-shaped frame is arranged at a first end of the force bearing cylinder, and a second inner reinforced n-shaped frame is arranged at a second end of the force bearing cylinder; and at least one first satellite supporting table is arranged on an outer side arc surface of the first end of the force bearing cylinder, and at least one second satellite supporting table is arranged on the outer side arc surface of the second end of the force bearing cylinder. According to the scheme, use requirements of carrying and releasing a plurality of satellites at the same time can be met, rigidity is high, weight is light, the structure is integrally manufactured, assembly is simple, reliability is high, manufacturability is good, and product consistency is good too.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a load-bearing structure of a multi-satellite distributor. Background technique [0002] The load-bearing cylinder of the multi-satellite distributor is mainly used for launching multiple satellites with one arrow. The load-bearing cylinder of the multi-satellite distributor can generally arrange 2 or 4 satellites according to its own ring direction, and the connection point is generally located in the load-bearing cylinder of the multi-satellite distributor. Each satellite is generally connected to the load-bearing cylinder of the multi-satellite distributor through four connection points, and the four points also have the functions of separation and pop-up release. The weight efficiency of the load-bearing cylinder of the multi-satellite distributor is exactly the same as that of the satellite. At the same time, the load-bearing cylinder must also meet the overall stiffness re...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/00
CPCB64G1/002
Inventor 季宝锋王志勇刘含洋唐占文刘千金一王非刘发杰张鹏李世伟
Owner TIANJIN ISTAR-SPACE TECH CO LTD