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

A test system and configuration method for aircraft climate environment test

A climate environment and test system technology, which is applied in aircraft component testing, climate sustainability, building types, etc., can solve the problems of resource waste experiments, errors, etc., and achieve the advantages of easy operation, small footprint, and convenient observation of test conditions Effect

Active Publication Date: 2022-04-12
CHINA AIRPLANT STRENGTH RES INST
View PDF8 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, when switching between aircrafts of different sizes, the simulated experimental cabin is likely to cause a certain waste of resources or experimental errors.

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 test system and configuration method for aircraft climate environment test
  • A test system and configuration method for aircraft climate environment test
  • A test system and configuration method for aircraft climate environment test

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0045] like figure 2 Shown, a kind of test system of aircraft climate environment test, comprises: the big environment cabin 1 and the small environment cabin 2 that are arranged side by side front and back, the first annex building 11 that is positioned at the big environment cabin 1 side and is positioned at the big environment cabin 1 another The second annex building 12 on the side, the third annex building 21 on one side of the small environment cabin 2, the power assembly 3 located at the rear of the small environment cabin 2, the power assembly 3 includes a warehouse 31, a boiler room 32, and a compressed air station arranged side by side. 33 and the circulating water pump room 34, the exhaust space of the exhaust pipe 22 is reserved between the boiler room 32 and the compressed air station 33, a circulating water pool 35 is arranged underground on one side of the circulating water pump room 34, and a There is a circulating cooling tower 36 connected to the circulating...

Embodiment 2

[0050] The difference between this embodiment and Embodiment 1 lies in that the thickness of the interlayer 4 is different, and the thickness of the interlayer 4 is 1 m.

Embodiment 3

[0052] The difference between this embodiment and Embodiment 1 lies in that the thickness of the interlayer 4 is different, and the thickness of the interlayer 4 is 2 m.

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 discloses a test system and a configuration method for aircraft climate and environment testing, belonging to the technical field of aircraft testing. The test system for aircraft climate and environment testing includes: a large environment cabin and a small environment cabin arranged side by side in front and behind, located in the large environment cabin The first annex on one side and the second annex on the other side of the large environmental chamber, the third annex on one side of the small environmental chamber, the power assembly behind the small environmental chamber, the inner walls of the large and small environmental chambers and the There are interlayers between the outer walls, an isolation door is provided at the junction of the large and small environmental chambers, a water collection tank is provided under the ground of the large and small environmental chambers, and a drainage assembly is arranged inside the water collection tank. The test system of the aircraft climate environment test of the present invention fully considers the functional requirements, building structure, environmental simulation system, power supply and other factors of the super-large climate environment laboratory, iteratively optimizes the layout of the laboratory, and forms a super-large comprehensive The overall layout of the climate-like environment laboratory.

Description

technical field [0001] The invention relates to the technical field of aircraft testing, in particular to a test system and a configuration method for aircraft climate environment testing. Background technique [0002] Aircraft flight test refers to various test experiments conducted by the aircraft under the real flight environment conditions. The design and test of the aircraft need to go through repeated all-round simulation tests before entering the flight test stage. Therefore, in order to complete the simulation tests under various conditions of the aircraft, a large-scale climate environment laboratory is needed. [0003] The climate and environment laboratory is used for climate and environment adaptability tests of large-scale equipment such as aviation aircraft. Snowfall, fog, wind, icing / freezing rain, wind blowing rain, wind blowing snow and other climate environments. The volume of the climate and environment laboratory, the scale and complexity of the environ...

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): B64F5/60E04H1/00
CPCB64F5/60E04H1/00Y02P70/50
Inventor 王彬文成竹吴敬涛任战鹏刘海燕
Owner CHINA AIRPLANT STRENGTH RES INST
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

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com