Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Leading edge capable of improving bird impact resistance of airplane

A technology for wing leading edge and bird strike, applied in wings, aircraft parts, motor vehicles, etc., can solve problems such as skin tearing, wing leading edge deformation, front beam structure damage, etc., and achieve bird strike resistance. Improve, increase the structural rigidity, protect the effect of the beam web

Active Publication Date: 2017-05-24
NORTHWESTERN POLYTECHNICAL UNIV
View PDF5 Cites 6 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to overcome the problems that the leading edge of the wing undergoes severe deformation or even the skin is torn and the front beam structure is greatly damaged after the bird strikes, the present invention proposes a leading edge of the wing that can improve the anti-bird strike performance of the aircraft.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Leading edge capable of improving bird impact resistance of airplane
  • Leading edge capable of improving bird impact resistance of airplane
  • Leading edge capable of improving bird impact resistance of airplane

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0030] This embodiment is a bird strike-resistant wing front edge for a certain type of aircraft, including the wing leading edge skin 4, additional skin 5, front beam 3, small front beam 2, multiple front ribs 6, multiple rear Rib 7 and two side ribs 2. among them:

[0031] The two side ribs 1 are respectively fixed on the upper surface of the two ends of the front beam 3. The small front beam 2 is located above the two side ribs, and the two ends of the small front beam are riveted to the inner surfaces of the two side ribs respectively. The rear ribs 7 are arranged between the upper surface of the front beam 3 and the lower surface of the small front beam 2, and the rear ribs are inclined to form a "V" or inverted shape between two adjacent rear ribs. "V"-shaped included angle; the angles of the included angles are all 60°. A plurality of front ribs 6 are uniformly distributed on the upper surface of the small front beam 2. The vertex of each front rib 6 and the vertex of ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention relates to a leading edge capable of improving bird impact resistance of an airplane. A small front beam is added into the leading edge, front ribs are distributed on the small front beam, and an additional skin is tightly attached; when the leading edge meets bird impact, a stronger support effect on a front edge skin and the additional skin is achieved; thus, structural rigidity is improved, and structural appearance is kept as far as possible; in a deforming process, the additional skin can drive the front ribs to generate plastic deformation, so that more energy is absorbed. Rear ribs with an inclined angle can improve structural rigidity and are beneficial to buffering bird impact and protecting web plates. According to the leading edge disclosed by the invention, a requirement of an airplane structure on weight is fully taken into consideration, and structural weight is reasonably distributed; compared with an original structure, the thickness of the front edge skin and the thicknesses of the ribs are reduced by half to be used for adding the small front beam and the additional skin to design wing ribs again; structural weight is reduced by 3% compared with the original structure, so that the bird impact resistance of the leading edge is effectively improved.

Description

Technical field [0001] The invention relates to the field of civil aircraft structure design, in particular to a wing leading edge capable of improving the bird strike resistance of the aircraft. Background technique [0002] A bird strike refers to an accident that occurs when an aircraft or other aircraft flying in the air collides with flying birds. With the rapid development of the civil aviation industry, bird strikes of civil aircraft have become one of the most serious security threats to civil aviation. According to a United Airlines report, between 1990 and 2008, American civil aviation reported 89,727 collisions between animals and civilian aircraft, 97.4% of which were caused by flying birds. Relevant data show that the windward side of the aircraft, including the aircraft windshield, radome, engine, leading edge of the wing and the leading edge of the tail, are the most vulnerable parts to bird strikes. There are often oil systems or control lines inside the front e...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): B64C3/18B64C3/26
CPCB64C3/18B64C3/26B64U30/10
Inventor 索涛李玉龙王振郝鑫刘军汤忠斌
Owner NORTHWESTERN POLYTECHNICAL UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products