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A supersonic vehicle with low resistance and low sonic boom layout

A technology of aircraft and supersonic speed, which is applied in canard aircraft, aircraft parts, transportation and packaging, etc. It can solve the problems of low wave resistance and low wave resistance, and achieve the effects of reducing the impact of sonic boom, increasing the curvature of the wing, and reducing wave resistance

Active Publication Date: 2017-03-08
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the current aerodynamic layout of supersonic vehicles, there is a certain contradiction between the wing area and the cruise angle of attack, and it is impossible to take into account the requirements of low wave resistance and low sound explosion for small wing area and small flight angle of attack

Method used

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  • A supersonic vehicle with low resistance and low sonic boom layout
  • A supersonic vehicle with low resistance and low sonic boom layout
  • A supersonic vehicle with low resistance and low sonic boom layout

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Embodiment Construction

[0021] In order to better understand the low-resistance and low-sonic-burst supersonic vehicle according to the scheme of the present invention, a preferred embodiment of the low-resistance and low-sonic-burst supersonic vehicle of the present invention will be further described below in conjunction with the accompanying drawings.

[0022] Such as Figure 1-Figure 5 As shown, the supersonic aircraft with low-resistance and low-sound-burst layout provided by the present invention adopts a canard layout and a fuselage with a large slenderness ratio. The front landing gear is forwardly received in the front landing gear compartment at the bottom of the nose 1; behind the nose 1, the front part of the middle front fuselage 11 of the circular cross-section is arranged with a full-motion trapezoidal canard 2 with a medium sweep angle; Fuselage 11 back, before wing 4 is the air inlet 3 of power system; Middle rear fuselage 7 adopts the design of bee waist, and the width of bee waist ...

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Abstract

The invention provides a low resistance and low sonic boom layout supersonic aircraft, and relates to the technical field of supersonic aircraft design. According to the low resistance and low sonic boom layout supersonic aircraft, the canard configuration and the large slenderness ratio aircraft body are used, the aircraft head completely droops, the lower edge of the tip portion upturns, the front undercarriage is forward received into the front undercarriage cabin of the aircraft head, the front portion of the middle-front aircraft body is provided with a full-motion trapezoidal canard having a middle sweepback, the back portion of the middle-front aircraft body and the position in front of the wing are the gas inlet channel of the power system, the middle-rear aircraft body adopts the wasp waist design so as to connect the root portions of the upper wing and the lower wing of the aircraft wings, two jet engines are vertically arranged on the rear aircraft body in a side-by-side manner, the trapezoidal vertical tail having a large sweepback is arranged on the upper portion of the rear aircraft body, and the tip portions of the upper wing and the lower wing of the aircraft wings are connected through the end plate. According to the low resistance and low sonic boom layout supersonic aircraft of the present invention, the shock wave generated due to the wing attack angle is weakened, the sonic boom influence of the shock wave on the ground is reduced, the stability is strong, and safety and reliability are provided.

Description

technical field [0001] The invention relates to the technical field of supersonic aircraft design, in particular to a supersonic aircraft with low-resistance and low-sonic-explosion layout. Background technique [0002] For an aircraft that cruises at high speed in the atmosphere, the aerodynamic layout with minimum drag and maximum lift-to-drag ratio at supersonic speed is its main design goal. However, supersonic cruising flight will generate shock waves. The economical problems caused by wave resistance and the noise pollution caused by sonic explosions have always been the fetters of the development of supersonic aircraft. Especially for supersonic commercial aircraft, how to weaken the impact of the shock wave is always the focus of its layout design. [0003] The shock wave intensity of a supersonic vehicle depends on its own layout and volume. Therefore, the fuselage and wings become the main parts of the aircraft that generate shock waves. A fuselage with a large ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/12B64C3/10B64C3/28
Inventor 郭润兆曲浩谭玉婷
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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