Deflection warhead

A warhead and shell technology, applied in the field of deformation aircraft, can solve the problems of low control efficiency of the warhead and tail, and achieve the effects of simple structure, high control precision and fast response

Inactive Publication Date: 2016-02-10
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a deflected warhead, which is used to solve the problem of low control efficiency of the wings and tail, so as to achieve the purpose of high-efficiency flight control

Method used

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Embodiment Construction

[0019] The implementation will be described in detail below in conjunction with the description of the accompanying drawings

[0020] to combine Figure 1 ~ Figure 4 , a deflecting warhead, including a swing cone, a spherical sub-shell 3, a bullet shell 4 and a driving mechanism; the bullet shell 4 is a circular platform, and the circular platform is provided with a cavity that runs through its bottom and top surfaces.

[0021] Described swinging cone comprises cone 1, rotating spheroid 2 and square shaft 17, has a plane on the outer surface of rotating spheroid 2, by this plane, rotating spheroid 2 is fixed on the bottom surface center of cone 1, and this plane The opposite spherical surface cooperates with the spherical secondary casing 3 to form a spherical pair, and the diameter of the rotating sphere 2 equals the inner diameter of the spherical secondary casing 3; one end of the spherical secondary casing 3 is connected to the small end of the bullet casing 4 bottom area,...

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Abstract

The invention discloses a deflection warhead. The deflection warhead comprises a swinging cone, a spherical surface pair shell, a warhead shell and a driving mechanism, wherein the warhead shell is a circular platform and is provided with a cavity penetrating through the bottom surface and the top surface of the warhead shell; the swinging cone comprises a cone, a rotary sphere body and a square shaft; a plane is turned on the outer surface of the rotary sphere body; the rotary sphere body is fixed at the center of the bottom surface of the cone through the plane; a spherical surface opposite to the plane is matched with the spherical surface pair shell to form a spherical surface pair; the other end of the spherical surface pair shell is connected with one end, with the small bottom area, of the warhead shell; one end of the square shaft is fixed on the rotary sphere body and the other end of the square shaft is located in the warhead shell; the driving mechanism is located in the warhead shell. According to the deflection warhead, the aim that the swinging cone swings in a relatively large range can be realized and the deflection warhead has the advantages of high control precision and rapid response.

Description

technical field [0001] The invention belongs to the field of deformable aircraft, and in particular relates to a deflected warhead. Background technique [0002] As early as 1946, the engineering community proposed the concept of a "movable nose cone", which was the prototype of a deflecting warhead. Regarding the research on deflected warheads, NASA has conducted a series of theoretical analysis and experimental research. Among them, Lander proved through wind tunnel tests that the aerodynamic characteristics of the deflected warhead are superior to those of the duck-type projectile. Domestic researchers such as Wang Ju also proved through experiments that the aerodynamic characteristics of the deflected warhead are superior to those of the canard rudder. In addition, the wings and empennage can also control the flight, but the disadvantages of the wings and the empennage are that the area of ​​the wings is larger, the required control force is larger, and the correction e...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B12/02
Inventor 李恒郭锐刘荣忠吕胜涛
Owner NANJING UNIV OF SCI & TECH
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