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Built-in missile cabin mechanism containing soft oil tank and stealth aircraft with built-in missile cabin mechanism

A technology of soft fuel tank and bomb bay

Pending Publication Date: 2022-04-12
HIWING AVIATION GENERAL EQUIP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0008] The invention provides a built-in bomb bay mechanism containing a soft fuel tank and a stealth aircraft with it, which can solve the problem of complex structure and heavy weight of the built-in bomb bay mechanism of stealth aircraft in the prior art, which leads to the bomb load, stealth and combat effectiveness of combat aircraft. The technical problem that the radius cannot be taken into account at the same time

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  • Built-in missile cabin mechanism containing soft oil tank and stealth aircraft with built-in missile cabin mechanism
  • Built-in missile cabin mechanism containing soft oil tank and stealth aircraft with built-in missile cabin mechanism
  • Built-in missile cabin mechanism containing soft oil tank and stealth aircraft with built-in missile cabin mechanism

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Embodiment Construction

[0030] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. 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. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0031] It should be noted that the terminology used here is only for describing specific implementations, and is not intended to limit t...

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Abstract

The invention provides a built-in missile cabin mechanism containing a soft oil tank and a stealth aircraft with the built-in missile cabin mechanism. The built-in missile cabin mechanism comprises a built-in missile cabin shell, a soft oil tank and a stealth aircraft, a soft oil tank hydraulic device; the soft oil tank is located between the soft oil tank hydraulic device and the third side wall, and the soft oil tank can be compressed under the action of the soft oil tank hydraulic device; and the missile built-in rotating device and the missile built-in rotating mechanism are connected with the second side wall and the missile correspondingly, and the missile built-in rotating mechanism is used for being matched with the rotatable cabin door so that the missile can be externally hung outside the built-in missile cabin shell or arranged in the containing space of the built-in missile cabin shell. According to the technical scheme, the technical problem that in the prior art, a stealth aircraft built-in missile cabin mechanism is complex in structure and large in weight, and consequently the missile loading amount, invisibility and combat radius of a combat aircraft cannot be considered at the same time can be solved.

Description

technical field [0001] The invention relates to the technical field of stealth aircraft, in particular to a built-in bomb bay mechanism with a soft fuel tank and a stealth aircraft with the same. Background technique [0002] With the successful development and equipment of American F22, Russian T50 and Chinese J20, it marks that the world's major powers have entered the era of "fourth generation aircraft". An important criterion for judging whether a combat aircraft is a "fourth-generation aircraft" is the so-called "4S" standard - stealth (Stealth), supersonic cruise (Supersonic), over-the-horizon attack (Superior-sensor) and super Mobility (Super-agility). Among them, the purpose of supersonic cruise is to increase the range and shorten the intervention time; and stealth is the key to achieve combat effectiveness. [0003] With the rapid development of aviation science and technology, the idea of ​​aircraft structure design is constantly updated, and the requirements of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D7/00B64D37/04B64D37/06
Inventor 李东伟许聪颖杨鹏
Owner HIWING AVIATION GENERAL EQUIP
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