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Hovering type folding wing lifting body aircraft based on variable centroid technology

A wing lift and variable center of mass technology, which is applied in the field of aviation aircraft, can solve problems such as difficult maneuvering and control, decreased aircraft stability, and large wing size, so as to facilitate transportation and delivery, improve flight performance and stability, and reduce weight. The effect of small storage space

Active Publication Date: 2014-08-06
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, vertical / short take-off and landing fixed-wing aircraft emerged as the times require, but the wings of this type of aircraft are relatively large, and they need to occupy a large space when hovering in the air, and cannot hover and fly in a small space
Although another type of tilt-rotor aircraft can realize vertical take-off and landing and high-speed cruise at the same time, it also has serious defects. The propellers rotate synchronously, which is quite difficult to maneuver and control
In order to overcome these "quality" defects, "Osprey" had to adopt many complicated and unconventional technical measures, which affected the weight, performance and production cost of the whole machine
In addition, the aerodynamic performance of fixed-wing aircraft capable of vertical / short take-off and landing is different when flying in different attitudes such as takeoff and cruise. The irregular transformation of the distance between the aerodynamic center and the center of mass reduces the stability of the aircraft, making it unable to take into account different attitudes. flight mission

Method used

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  • Hovering type folding wing lifting body aircraft based on variable centroid technology
  • Hovering type folding wing lifting body aircraft based on variable centroid technology
  • Hovering type folding wing lifting body aircraft based on variable centroid technology

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Embodiment Construction

[0018] See attached figure 1 , 3 , a hoverable folding wing lifting body aircraft based on variable center of mass technology, which includes: a lifting body fuselage 1, two front wings 41 connected to the lifting body fuselage 1, and two rear wings 42 adopt wing bodies Fused tandem wing layout, the aircraft also includes: variable center mechanism 2, vector thrust mechanism 3 and wing rotation and folding mechanism 4;

[0019] The lifting body fuselage 1 is a fuselage that can provide lift for the aircraft as a whole during flight, so that the wing area can be effectively reduced, and the aircraft still has superior air cruise capability;

[0020] Two front wings 41 and two rear wings 42 adopt the wing-body fusion type tandem wing layout, which is: the front wing 41 and the wing 42 are arranged in pairs before and after and share the aerodynamic layout of the lift; this layout can Reduce the wingspan of the wing, making the aircraft more compact and flexible;

[0021] The ...

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Abstract

The invention relates to an aviation aircraft, and in particular relates to a hovering type folding wing lifting body aircraft based on a variable centroid technology. According to the technical scheme, the hovering type folding wing lifting body aircraft based on the variable centroid technology comprises a lifting body airframe (1), a variable centroid mechanism (2), a vectored thrust mechanism (3) and a wing rotation folding mechanism (4), wherein two front wings (41) and two rear wings (42) which are connected with the lifting body airframe (1) are in a wing combination type serial wing layout. By adopting the hovering type folding wing lifting body aircraft based on the variable centroid technology, the problems of take-off and landing performances and multi-attitude flight performance of a fixed wing aircraft are solved, and the functions of vertical / short-distance take-off and landing, thrust vectoring and small-space flight of the fixed wing aircraft are realized.

Description

technical field [0001] The invention relates to an aviation aircraft, in particular to a hoverable lifting body aircraft. Background technique [0002] At present, in the field of aviation in the world, aircraft are mainly divided into two types: fixed-wing aircraft and rotary-wing aircraft. Due to the single and fixed layout of these two aircrafts, they still have great limitations in various aspects. Conventional fixed-wing aircraft need to take off and land by taxiing, which has great limitations in the way of taking off and landing, and has strict requirements on the quality of the runway (length, width, hardness, flatness, material, maintenance level, etc.). Although the rotorcraft can reduce the requirements on the quality of the runway, its flight mode makes its flight speed low, the range is short, and the payload is low. Therefore, vertical / short take-off and landing fixed-wing aircraft have emerged as the times require. However, the wings of this type of aircraft...

Claims

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Application Information

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IPC IPC(8): B64C3/56B64C17/02B64C29/00
Inventor 唐胜景陈天悦李震周小陈刘真畅李博
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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