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A return cargo aircraft

An aircraft, return-type technology, applied in the aerospace field, to achieve the effects of high safety, improved structural utilization, and reduced launch costs

Active Publication Date: 2022-01-18
航天科工空间工程发展有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It effectively solves the problems of compact layout, high safety, and excellent carrying capacity, and meets the needs of the space station for fast, flexible, and low-cost downlink transportation of daily cargo

Method used

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  • A return cargo aircraft
  • A return cargo aircraft
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Examples

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Embodiment Construction

[0062] Various exemplary embodiments of the present invention will now be described in detail with reference to the accompanying drawings. It should be noted that the relative arrangements of components and steps, numerical expressions and numerical values ​​set forth in these embodiments do not limit the scope of the present invention unless specifically stated otherwise.

[0063] The following description of at least one exemplary embodiment is merely illustrative in nature and in no way taken as limiting the invention, its application or uses.

[0064] Techniques and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, such techniques and devices should be considered part of the description.

[0065] In all examples shown and discussed herein, any specific values ​​should be construed as exemplary only, and not as limitations. Therefore, other instances of the exemplary embodiment may have different values.

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Abstract

The invention discloses a return-type cargo aircraft, comprising: a power cabin at the bottom; the power cabin includes a propeller that provides the aircraft with power required for on-orbit flight; an airbag compartment; an airbag and a buffer assembly are included in the airbag compartment; an equipment compartment located above the airbag compartment and fixed in combination with the airbag compartment; and a cargo compartment located above the equipment compartment and fixed in combination with the equipment compartment; the power compartment is configured as It is used to carry the propeller to provide on-orbit power for the aircraft; the air bag compartment is configured to carry the storage air bag and the buffer assembly and to serve as the main load-bearing structure of the ascending section of the aircraft; the equipment bay is configured to carry and fix the electronic control equipment of the aircraft; The cargo compartment is configured to carry cargo to be carried by the aircraft. In the present invention, a load-bearing system is formed by connecting the cabin sections in series, and sufficient layout space can be provided in the interior to maximize the utilization rate of the cargo space.

Description

technical field [0001] The invention relates to the field of aerospace technology. More specifically, it relates to a returnable cargo aircraft. Background technique [0002] In the past few decades, my country's space recovery technology has always used parachutes to assist in the recovery process with buffer reverse rockets and positioning devices. The improvement and development of corresponding recovery technologies are also carried out on this basis. At present, space return technology is mainly used in the field of manned spaceflight. The technical solution adopts a manned return capsule, and the space cargo is transported down with the return capsule. The rate is lower. With the gradual development of my country's space station program, the fast, flexible, and low-cost downlink transportation technology solutions for daily cargo on the space station in the future will surely become a hot research field, which can be extended to commercial activities on the Internati...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/22B64G1/52
CPCB64G1/22B64G1/52
Inventor 李枫李毅
Owner 航天科工空间工程发展有限公司
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