Variable-camber deformable wing based on connecting rod driving

A connecting rod drive and wing technology, applied in the direction of wing adjustment, etc., can solve the problems of large-scale camber deformation of the wing, low efficiency of the drive mechanism, etc., to improve the efficiency of drive deformation, simple and reliable principle, and strong practicability Effect

Active Publication Date: 2021-03-19
中国空气动力研究与发展中心设备设计及测试技术研究所
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0005] Aiming at the problems in the prior art that the wing is difficult to deform in a large range of camber and the efficiency of the driving mechanism is low, the purpose of the present invention is to provide a deformed wing with v

Method used

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  • Variable-camber deformable wing based on connecting rod driving
  • Variable-camber deformable wing based on connecting rod driving

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Embodiment Construction

[0021] The technical solutions of the various embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0022] In this embodiment, a deformed wing with variable camber driven by a connecting rod such as figure 1 As shown, it includes the wing body, the connecting rod drive assembly and the shaft connection assembly.

[0023] The wing body includes wing module I1, wing module II2, wing module III3 and wing module IV4, and wing module I1 is a fixed section.

[0024] The connecting rod driving assembly is arranged inside the wing body, including a slider 5, a driving connecting rod 6, a...

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Abstract

The invention discloses a variable-camber deformable wing based on the connecting rod driving. The deformable wing comprises a wing body, a connecting rod driving assembly and a rotating shaft connecting assembly, the wing body is composed of multiple sections of wing modules, the wing modules are rotationally connected through the rotating shaft connecting assembly at a time, and the connecting rod driving assembly organically combines all the wing modules; all the wing modules can be driven by linear motion to form knuckle type bending deformation, the adopted connecting rod driving assemblyis high in driving efficiency, and large-range bending deformation of wings can be achieved.

Description

technical field [0001] The invention belongs to the technical field of aerospace equipment and relates to a wing structure, in particular to a deformed wing with variable camber driven by a connecting rod. Background technique [0002] The wing is a key component that determines the overall aerodynamics of the aircraft, and its shape has an important impact on the overall performance of the aircraft. Under different flight environments and missions, changing the aerodynamic shape of the wing itself according to the actual situation can change the performance parameters of the aircraft such as lift-to-drag ratio, take-off and landing distance, fuel consumption, range, maneuverability and stealth, so that the aircraft can fly in the air. Maintain the best overall performance in the process. [0003] Due to the various advantages of the deformed wing, a large amount of research work has been carried out abroad since the last century. Since the end of World War II, the United ...

Claims

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Application Information

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IPC IPC(8): B64C3/48
CPCB64C3/48
Inventor 高鑫宇蔡清青聂旭涛张伟唐萍
Owner 中国空气动力研究与发展中心设备设计及测试技术研究所
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