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Morphing nose cone of aircraft based on multi-ring closed-chain space-deployable mechanism

A technology for deploying mechanisms and aircraft, which is applied in the field of aerospace vehicles, can solve problems such as the complexity of the aerodynamic characteristics of aircraft, and achieve the effects of large deformation, strong controllability, and flexible movement

Active Publication Date: 2018-11-09
TSINGHUA UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The structural variation of the variant aircraft in the related art is mainly the deformation of the wing, but the deformation of the wing will complicate the aerodynamic characteristics of the aircraft. The nose cone is an important part of the design of the variant aircraft. Different flight environments need to choose different The shape of the nose cone, so the deformable nose cone is of great significance for the optimization of the aerodynamic shape of the aircraft

Method used

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  • Morphing nose cone of aircraft based on multi-ring closed-chain space-deployable mechanism
  • Morphing nose cone of aircraft based on multi-ring closed-chain space-deployable mechanism
  • Morphing nose cone of aircraft based on multi-ring closed-chain space-deployable mechanism

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Embodiment Construction

[0027] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0028] Such as Figure 1-Figure 6 As shown, the aircraft variant nose cone 1 based on the multi-loop closed-chain space expandable mechanism according to the embodiment of the present invention includes a plurality of conical body segments 100, a plurality of secondary scissor mechanisms 200, a plurality of drive assemblies 300 and a Cone head 400.

[0029] A plurality of conical body segments 100 are arranged at intervals along the front-to-back direction (the front-to-back direction is as Figure 1-Figure 6 As indicated by the arrow A in), each conical body segment 100 includes a housing, a fixing groove 110 and a sliding groove 120 .

[0030] The secondary scissor mechanism 200 is located between two adjacent cone segments 100, and there are four secondary scissor mechanisms 200 between the adjacent two cone segments 100, and the secondary scissor mechan...

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Abstract

The invention provides a morphing nose cone of an aircraft based on a multi-ring closed-chain space-deployable mechanism. The morphing nose cone comprises a plurality of conical body segments, a driving part and a conical head, wherein the first conical body segment and the last conical body segment are respectively provided with a group of hold-down groove and sliding groove, and the rest conicalbody segments are respectively provided with two groups of hold-down groove and sliding groove; a secondary scissors type mechanism with both telescoping and bending functions is arranged between twoadjacent body segments; one end of each secondary scissors type mechanism is cooperated with the hold-down groove or the sliding groove on one body segment, and the other end of each secondary scissors type mechanism is connected with a next-stage scissors type mechanism through a telescoping rod equipped with a spherical hinge; the driving part is composed of a push rod, a cross bar, connectingrods and connection shafts in parallel connection and carries out distributed driving; and the conical head is located at the forefront of the plurality of conical body segments. The morphing nose cone of the invention can realize complex morphing and has the advantages of flexible movement, great morphing amount, strong controllability, etc.

Description

technical field [0001] The invention relates to the technical field of aerospace vehicles, in particular to an aircraft variant nose cone based on a multi-loop closed-chain space expandable mechanism. Background technique [0002] The flight performance of the aircraft can be improved by proper deformation of the aircraft in different flight environments. The structural variation of the variant aircraft in the related art is mainly the deformation of the wing, but the deformation of the wing will complicate the aerodynamic characteristics of the aircraft. The nose cone is an important part of the design of the variant aircraft. Different flight environments need to choose different The shape of the nose cone, so the deformable nose cone is of great significance for the optimization of the aerodynamic shape of the aircraft. Contents of the invention [0003] In order to overcome the deficiencies of the above-mentioned prior art, the purpose of the present invention is to p...

Claims

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Application Information

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IPC IPC(8): B64C1/00B64C1/06
CPCB64C1/0009B64C1/068
Inventor 阎绍泽梁友鉴张玉玲赵杰亮卢晟昊
Owner TSINGHUA UNIV
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