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Structure, design method and application of deformable aircraft product

A technology of aircraft and internal structure, which is applied in the field of self-defense of various aircraft, and can solve the problem that there are no similar products on the aircraft platform

Pending Publication Date: 2021-05-25
陈红明 +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] There is no similar product in the field of self-defense for existing aircraft platforms (including various surface ships and ground mobile platforms)

Method used

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  • Structure, design method and application of deformable aircraft product
  • Structure, design method and application of deformable aircraft product
  • Structure, design method and application of deformable aircraft product

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Embodiment Construction

[0050] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments, where the schematic embodiments and descriptions of the present invention are used to explain the present invention, but not to limit the present invention.

[0051] The following is attached figure 2 ~ attached Figure 7 Embodiment The above-mentioned technical solution item (1) of the present invention, the retractable mechanism (1) is further described in detail.

[0052] Such as figure 2 As shown, the implementation strategy of item (1) of the technical solution: the telescopic mechanism is composed of a proximal rod, a connecting component and a distal rod.

[0053] Such as Figure 3 ~ Figure 4 As shown, the implementation strategy of the technical scheme (1) clause: the proximal rod is made up of two mutually perpendicular cylinders, wherein one section of the cylinder is a cylinder or a sphere (the present invention is illustrated w...

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Abstract

The invention relates to a deformable aircraft, as well as a use field and the application thereof, and provides a structural design scheme, a structural design method and the application of a novel deformable aircraft. According to the scheme and the method, a telescopic mechanism and a rotatable mechanism are spatially arranged and combined; a radar reflector is applied to a mechanism; a fuel gas power device is applied to the mechanism; and a foldable high-temperature-gas-resistant special textile fabric is applied to the mechanism. After the aircraft is unfolded, the aircraft can generate an infrared characteristic and has an appearance characteristic of an aircraft body; the product produces a flight accompanying product with the same size as an aircraft platform, can be used for protecting the platform, and can also be used for specific performance purposes; the method is used for a specific product which needs to simulate the same characteristics of medium and remote monitoring and display of an original aircraft platform. The structural design scheme and the method of the deformable aircraft are mainly applied to all aircraft platforms (including various water surface ships and boats and ground mobile platforms), including unmanned or manned aviation aircrafts, such as transport aircrafts, helicopters, fighters, bombers, aerospace crafts, manned spacecrafts and the like.

Description

technical field [0001] The present invention provides a structure, design method and application of a deformable aircraft product, and particularly relates to a structure and design method of an aircraft product with the same characteristics near the aircraft platform after being ejected from the aircraft platform. It is used in the field of self-defense of various aircraft. Background technique [0002] There is no similar product in the field of self-defense for existing aircraft platforms (including various surface ships and ground mobile platforms). Contents of the invention [0003] In view of this, the present invention provides a self-defense product, design method and application method for various aircraft platforms. [0004] The technical scheme adopted in the present invention is: [0005] (1) Design a telescopic mechanism. In the service state, the internal telescopic mechanism of the deformable aircraft is retracted and locked. In the combat state, the inter...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/30
CPCB64C1/30
Inventor 陈红明唐林
Owner 陈红明
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