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Horizontal tail front edge for bird strike-resisting airplane

A technology for the leading edge and leading edge of a wing, applied in aircraft parts, wings, multi-layer structures, etc., can solve the problems of high cost, breakdown, deformation, etc., and achieve the effect of simple production and low cost

Active Publication Date: 2011-04-27
西测翱翔(太仓)航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to overcome the defects in the prior art that the structure produced after a bird strike is either broken down, or greatly deformed, and the cost is high, the present invention proposes a flat tail leading edge of an anti-bird strike aircraft

Method used

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  • Horizontal tail front edge for bird strike-resisting airplane
  • Horizontal tail front edge for bird strike-resisting airplane
  • Horizontal tail front edge for bird strike-resisting airplane

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0027] The present embodiment is used for the leading edge of the horizontal tail of an anti-bird strike aircraft of a certain type.

[0028] Such as figure 1 As shown, this embodiment includes a leading edge skin 1, an upper honeycomb core layer 2 and a lower honeycomb core layer 5, a leading edge reinforcement 3 and a wing liner 4, an upper honeycomb core layer 2 and a lower honeycomb core layer 5, a front The edge reinforcement 3 and the wing liner 4 are all arranged between the spans in the leading edge of the wing along the horizontal tail span; wherein the leading edge reinforcement 3 is a triangular prism, and one corner of the leading edge reinforcement is located At the front end of the leading edge of the wing; the upper honeycomb core layer 2 and the lower honeycomb core layer 5 that are parallelograms are respectively fixed on the upper and lower inner surfaces of the leading edge skin 1, and one of the upper honeycomb core layer 2 and the lower honeycomb core lay...

Embodiment 2

[0035] The present embodiment is used for the leading edge of the horizontal tail of an anti-bird strike aircraft of a certain type.

[0036] Such as figure 1As shown, the present embodiment comprises flat tail skin 1, upper honeycomb core layer 2 and lower honeycomb core layer 5, leading edge stiffener 3 and wing liner 4, upper honeycomb core layer 2 and lower honeycomb core layer 5, leading edge The reinforcement 3 and the wing liner 4 are all arranged between the spans in the leading edge of the wing along the span direction of the horizontal tail of the aircraft; At the front end of the leading edge of the wing; the upper honeycomb core layer 2 and the lower honeycomb core layer 5 that are parallelograms are respectively fixed on the upper and lower inner surfaces of the leading edge skin 1, and an oblique of the upper honeycomb core layer 2 and the lower honeycomb core layer 5 The edges are all matched with one side surface of the leading edge reinforcement 3; the wing ...

Embodiment 3

[0043] The present embodiment is used for the leading edge of the horizontal tail of an anti-bird strike aircraft of a certain type.

[0044] Such as figure 1 As shown, the present embodiment comprises flat tail skin 1, upper honeycomb core layer 2 and lower honeycomb core layer 5, leading edge stiffener 3 and wing liner 4, upper honeycomb core layer 2 and lower honeycomb core layer 5, leading edge The reinforcement 3 and the wing liner 4 are all arranged between the spans in the leading edge of the wing along the span direction of the horizontal tail of the aircraft; At the front end of the leading edge of the wing; the upper honeycomb core layer 2 and the lower honeycomb core layer 5 that are parallelograms are respectively fixed on the upper and lower inner surfaces of the leading edge skin 1, and an oblique of the upper honeycomb core layer 2 and the lower honeycomb core layer 5 The edges are all matched with one side surface of the leading edge reinforcement 3; the wing...

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Abstract

The invention relates to a horizontal tail front edge for a bird strike-resisting airplane. An upper honeycomb sandwich layer, a lower honeycomb sandwich layer, a front edge reinforcing member and an aerofoil lining layer are arranged among spans on the horizontal tail front edge in a spanwise mode along a horizontal tail of the airplane; one angle of the front edge reinforcing member is positioned at the front end of the horizontal tail front edge; the upper honeycomb sandwich layer and the lower honeycomb sandwich layer which are in a shape of a parallelogram are fixed on upper and lower internal surfaces of a horizontal tail skin respectively, the edge of one vertex angle of each honeycomb sandwich layer is fixed with surfaces of the front edge reinforcing member and the horizontal tail skin respectively, and the edge of the other vertex angle is fixed with the surfaces of the horizontal tail skin and the aerofoil lining layer; and the honeycomb sandwich layers and the front edge reinforcing member are coated between the aerofoil lining layer and the internal surfaces of the horizontal tail skin by the aerofoil lining layer. In the horizontal tail front edge, birds are cut by the front edge reinforcing member, the impact force of the birds is absorbed by the honeycomb sandwich layers, and an internal structure of the horizontal tail front edge is protected against damage bythe aerofoil lining layer. The horizontal tail front edge is also suitable for vertical tails, aerofoil front edges and all beam edges which are likely to be subjected to bird strike on the airplane.

Description

technical field [0001] The invention relates to the field of civil aircraft structure design, in particular to a flat tail leading edge structure. Background technique [0002] A bird strike accident refers to an accident in which an aircraft such as an airplane flying in the air collides with a flying bird. With the rapid development of the civil aviation industry, civil aircraft bird strikes have become one of the most serious safety threats to civil aviation. According to relevant reports of United Airlines, from 1990 to 2008, American civil aviation reported 89,727 collisions between animals and civil aviation aircraft, 97.4% of which were caused by birds. Relevant data show that the windward side of the aircraft, including the windshield, radome, engine, wing leading edge and tail leading edge, is the most vulnerable to bird strikes. There are often oil circuit systems or control lines inside the leading edge structure. Once these internal facilities are damaged by bi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/20B64C3/26
Inventor 李玉龙石霄鹏索涛刘军
Owner 西测翱翔(太仓)航空科技有限公司
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