Offset side hanging type rocket adapter structure

A side-mounted and adapter technology, applied in the field of aerospace, can solve the problems of large payload, unable to carry volume, unable to meet the requirements of payload carrying, etc., to achieve the effect of improving strength, low cost, and easy installation

Pending Publication Date: 2022-07-29
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, when the payload space of the launch vehicle is small, the use of symmetrical side-mounted rocket adapters may not be able to meet the loading requirements of the payload.
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Method used

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  • Offset side hanging type rocket adapter structure
  • Offset side hanging type rocket adapter structure

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Embodiment Construction

[0026] In order to make the purposes, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments These are some embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of the present invention.

[0027] refer to figure 1 , figure 2 The structure of the offset side-mounted rocket adapter shown includes: a bearing member, a bearing bottom plate 3 and a support connecting member 4 .

[0028] The load-bearing member includes a load-bearing cylinder 1, and the interior of the load-bearing cylinder 1 is a hollow structure. The c...

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Abstract

The invention relates to the field of space flight and aviation, and discloses an offset side hanging type rocket adapter structure, which comprises a force bearing part, a side hanging part, a side hanging part and a side hanging part, and is characterized in that the force bearing part is eccentrically arranged relative to a central shaft of a rocket fairing; the bearing bottom plate is arranged at one end of the force bearing piece; the supporting connecting piece is connected with the force bearing piece and the bearing bottom plate; wherein the force bearing piece, the bearing bottom plate, the supporting connecting piece and the fairing of the rocket are encircled to form an enveloping space used for arranging an effective load of the rocket, and a center shaft of the fairing of the rocket penetrates through the enveloping space. By eccentrically arranging the force bearing piece, under the condition that the size of the fairing is not changed, the effective enveloping space in the rocket can be expanded, and the effective load with the larger single size can be conveniently carried. Through the effect of the supporting connecting piece, the strength of the adapter structure can be improved, the situation that the force load borne by the force bearing piece exceeds the allowable range is avoided, and connection between the rocket adapter structure and other sections of the tail stage of a rocket can be achieved through the bearing bottom plate.

Description

technical field [0001] The invention relates to the field of aerospace, in particular to an offset side-mounted rocket adapter structure. Background technique [0002] According to the different installation methods of the payload on the rocket adapter, the rocket adapter structure currently used in the rocket field can be divided into a base structure and a side-mounted structure. The base-mounted rocket adapter and the payload are connected and separated along the rocket flight direction, while the side-mounted rocket adapter and the payload are connected and separated laterally. [0003] At present, the structure of the side-mounted rocket adapter is mainly a symmetrical structure, and the payload is distributed around the adapter and connected to the adapter sideways. When the load space of the launch vehicle is small, the use of symmetrical side-mounted rocket adapters may not meet the payload requirements. Therefore, an offset side-mounted rocket adapter structure is...

Claims

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Application Information

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IPC IPC(8): F42B15/00
CPCF42B15/00
Inventor 高旭信傲李智朱璇鲍永定胡驰谭友德彭威曹丽方
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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