Airplane cockpit windshield structure with sun shading function

A cockpit and windshield technology, which is applied in the field of aircraft cockpit windshield structure design, can solve the problems of increased daily workload, loose and sagging sunshade devices, and increased aircraft weight, so as to improve economic performance, facilitate operation, and reduce weight.

Inactive Publication Date: 2016-05-18
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
View PDF7 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the crew members need sunshade, they need to turn down and unfold the sunshade device to block the direct sunlight; The sunshade d

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
  • Airplane cockpit windshield structure with sun shading function
  • Airplane cockpit windshield structure with sun shading function

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0015] The present invention will be described in further detail below. see figure 1 , figure 2 , an aircraft cockpit windshield structure with sun-shading ability, is characterized in that it is based on the sandwich structure windshield of various transparent materials of the traditional aircraft cockpit, and is determined according to the design eye position 1 of the aircraft cockpit. The windshield area above the horizontal line or the smaller windshield area is a sunshade area. In this area, a transparent ITO conductive heating film 3 is coated on the interlayer surface of the transparent ITO conductive heating film 2 adjacent to the outer layer of the windshield in this area, and two layers of ITO conductive heating film are coated. Between 2 and 3, a transparent nano-electrochromic sunshade film 4 is set, and a conductive bus bar 7 is set on the upper and lower edges of the outer ITO conductive heating film 2, and a similar conductive bus bar is set on the upper edge ...

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 an airplane cockpit windshield structure with a sun shading function. Based on a windshield structure of a traditional airplane cockpit, a sun shading region is determined according to a designed eye position 1 of the airplane cockpit, and in other words, a windshield region above the visual horizontal line of the designed eye position 1 of the airplane cockpit serves as the sun shading region; the outer surface of a transparent interlayer 6 adjacent to a transparent ITO conductive heating film 2 on the outer layer of a windshield is coated with a transparent second ITO conductive heating film 3; a transparent electrochromic sun shading rubber film 4 is inserted in the position between the ITO conductive heating film 2 and the ITO conductive heating film 3; and under the powering-on condition, a certain potential difference is formed between the two ITO conductive heating films, the color and light transmittance of the transparent electrochromic sun shading rubber film are changed, and therefore the shading function of the windshield of the airplane cockpit is achieved. By the adoption of the airplane cockpit windshield structure, the weight of an airplane is reduced and the economic performance of the airplane is improved; and the sun shading function is electrically controlled, the color and light transmittance of the windscreen in the sun shading region can be reversibly adjusted, and operation carried out by crew is facilitated.

Description

technical field [0001] The invention belongs to the design technology of windshield structure of aircraft cockpit. Background technique [0002] Conventional aircraft cockpit windshield adopts multi-layer inorganic tempered glass or plexiglass, PU layer, ITO conductive heating film and other materials to form a curved or flat laminated structure, and is sealed by a rubber ring to form an overall windshield, which has anti-bird impact, anti- It has functions such as ice defogging, but does not have sunshade function. In order to meet the shading needs of the crew, a mechanical shading device is often installed at an appropriate position on the upper part of the cockpit windshield. When the crew members need sunshade, they need to turn down and unfold the sunshade device to block the direct sunlight; The sunshade device may loosen and sag during long-term use, which interferes with the normal work of the crew and increases the weight of the aircraft. Contents of the invent...

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): B64C1/14B64C1/40
Inventor 何启国王雯
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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