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Recyclable and deformable launching nacelle

A variable form and pod technology, applied to rigid spacecraft, lighter-than-air aircraft, aircraft, etc., can solve the problem of difficulty in achieving synchronous buffering, less research on aerostat launch pods, and deformable aerostat launch pods There are no precedents and other problems, and the effect of large launch window, stealth shielding, recycling and delivery is achieved

Active Publication Date: 2021-04-09
INST OF MECHANICS - CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, there are few researches on aerostat launch pods in the world, especially there is no precedent for aerostat launch pods with deformable bodies
[0004] There are a few aerostat launching pods that can only realize the function of launching the aircraft, and cannot realize the functions of floating flight suspension, air launch and delivery, safe buffer landing, stealth shielding, and repeatable multiple recovery and delivery through the whole body deformation. integrated
[0005] At the same time, it is difficult for the buffering and shock absorbing devices of various landers to achieve synchronous buffering.

Method used

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  • Recyclable and deformable launching nacelle
  • Recyclable and deformable launching nacelle
  • Recyclable and deformable launching nacelle

Examples

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Effect test

Embodiment 1

[0041] Embodiments of the present invention relate to a recyclable launch pod in variable form, such as figure 1 , figure 2 , image 3 , Figure 8 and Figure 9 As shown, a recyclable and variable launch pod includes an electrical load compartment 1, an upper deformation frame 2, a conformal fixed frame 3, a bottom frame 4, a lower deformation frame 5, a synchronous shock absorber 6, and a suspension aircraft 7 And rope drive system 22 eight parts are made up of. 16 hinged lugs c29 are installed on the electrical load compartment 1, and 16 hinged lugs c30 of the 8 upper deformation frames 2 are hingedly installed on the 16 hinged lugs c29 on the electrical load compartment 1 through pin shafts and sliding bearings 37 , the 16 hinge lugs a32 of the 8 lower deformation frames 5 are hingedly installed on the 16 hinge lugs a31 of the 8 upper deformation frames 2 through pin shafts and sliding bearings 37, between the hinge lugs a32 and the hinge lugs a31 Connected through th...

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PUM

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Abstract

The invention belongs to the technical field of nacelle equipment, and provides a recyclable and deformable launching nacelle based on the defects of an existing aerostat nacelle. A hanging aircraft is hung on a lifting hook of an electrical load cabin, and a shape follow-up fixing frame is fixed to the bottom of the electrical load cabin through a center fixing frame and two side fixing frames. The hanging aircraft is arranged in a shape follow-up supporting hole of the shape follow-up fixing frame, the synchronous shock absorber is installed at the corresponding position of the bottom of the electrical load cabin, the rope driving system is installed in the electrical load cabin, and four steel wire ropes of the rope driving system are guided into the synchronous shock absorber through a plurality of sets of fixed pulleys and fixed to the corresponding positions of the bottom frame, and four steel wire ropes are used for winding and unwinding. The nacelle can realize integration of functions such as floating flight hanging, near-air launching and launching, safe buffer landing, invisible shielding and repeatable multi-time recycling and launching by utilizing deformation of the aircraft body. And meanwhile, the plurality of buffers can realize synchronous buffering.

Description

technical field [0001] The invention belongs to the technical field of pod equipment, and in particular relates to a recyclable launch pod in a variable form. Background technique [0002] The pod refers to a streamlined nacelle section that is installed with certain airborne equipment or weapons and hangs under the fuselage or wing. With the development of aviation technology, airborne pod technology has also made great progress. Generally speaking, airborne pods can be divided into: weapon pods (including aircraft gun pods, aviation rocket pods), reconnaissance pods, fire control pods, and logistics auxiliary pods (refueling pods). [0003] At present, there are few studies on aerostat launch pods in the world, especially there is no precedent for aerostat launch pods with deformable bodies. [0004] There are a few aerostat launching pods that can only realize the function of launching the aircraft, and cannot realize the functions of floating flight suspension, air lau...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64B1/22B64B1/00
CPCB64B1/22B64B1/00
Inventor 王福德李文皓张陈安吴臣武彭青
Owner INST OF MECHANICS - CHINESE ACAD OF SCI
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