A variable camber wing based on composite material corrugated sheet flexible skin

A composite material and plate flexibility technology, applied in the directions of wings, wing adjustment, aircraft parts, etc., can solve the problems of small out-of-plane stiffness and damage to the aerodynamic shape of the wing.

Active Publication Date: 2021-08-27
BEIHANG UNIV
View PDF6 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In addition, the out-of-plane stiffness of the composite corrugated sheet flexible skin is small. When aerodynamic load is applied, or when the bending deformation of the wing causes a certain side of the skin to be compressed, the composite corrugated sheet flexible skin will have a large out-of-plane stiffness. Deformation, resulting in destruction of the aerodynamic shape of the wing

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
  • A variable camber wing based on composite material corrugated sheet flexible skin
  • A variable camber wing based on composite material corrugated sheet flexible skin
  • A variable camber wing based on composite material corrugated sheet flexible skin

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0014] The present invention will be further described below in conjunction with the accompanying drawings and implementation examples.

[0015] The invention is a variant airfoil based on the flexible skin of corrugated board of composite material. Composite corrugated sheet flexible skin (such as figure 1 shown) is composed of continuous corrugated units connected smoothly, the central angle of each corrugated unit is θ, and the corrugated radius is R. Composite material corrugated plates have tensile and bending deformation capabilities in the corrugated direction, and in the direction perpendicular to the corrugated direction has greater rigidity. Among them, the composite material corrugated board is a unidirectional belt laminated corrugated board made of carbon fiber, glass fiber, Kevlar fiber and boron fiber, and a woven material corrugated board made of carbon fiber, glass fiber, Kevlar fiber and boron fiber. Variant wing structures (such as figure 2 shown) is com...

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

A variable-camber wing based on a flexible skin of a composite material corrugated plate is composed of a multi-section wing section, a rotating shaft, a hinge structure, a composite material corrugated plate and an elastic body layer. The connection relationship is as follows: each wing section is connected by the end of the rotating shaft, and the adjacent wing sections are covered with composite material corrugated plates. The composite material corrugated plates are respectively fixed on the platforms of the front wing section and the rear wing section. Each composite material corrugated plate A hinged structure is provided in the middle to connect with the corresponding wings, and the elastomer layer is bonded to the outer surface of the corrugated board made of composite material. The invention utilizes the characteristic that the flexible skin of the corrugated board of composite material has large deformation ability along the corrugation direction, designs a variable-camber wing structure, and uses a hinge structure to impose out-of-plane constraints on the flexible skin of the corrugated board of composite material. The wing can realize the function of variable camber, and the flexible skin of the composite corrugated board will not have out-of-plane deformation beyond the allowable range, and can maintain a good aerodynamic shape.

Description

technical field [0001] The invention provides a variable-camber wing based on a flexible skin of a composite corrugated board, which belongs to the field of structural design. Background technique [0002] In the field of aviation, "variant aircraft" is an aircraft that can enhance the performance of the mission profile by changing its geometric shape, and the most critical technology is the morphing wing. The variable camber wing is a kind of variant wing. Compared with the traditional wing, the variant wing with smooth and continuously variable camber has higher aerodynamic efficiency. Composite corrugated board has large tensile deformation capacity in the corrugation direction, good bending deformation capacity, and high stiffness in the direction perpendicular to the corrugation. Therefore, composite corrugated board is suitable as a flexible cover for variable camber wings. Skin. However, due to the unevenness of the composite corrugated board and the poor aerodynami...

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
Patent Type & Authority Patents(China)
IPC IPC(8): B64C3/26B64C3/44
CPCB64C3/26B64C3/44
Inventor 白江波杨光昊谢长川冒森
Owner BEIHANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products