An aircraft test comprehensive climate environment simulation system and simulation method

A climate environment and simulation method technology, applied in the direction of aircraft component testing, can solve the problems of high resource consumption, difficult organization and coordination, long test cycle, etc., and achieve low investment and operating costs, good scalability, and flexible system use. Effect

Active Publication Date: 2022-04-12
CHINA AIRPLANT STRENGTH RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, my country is still blank in the design and construction of climate environment simulation facilities suitable for aircraft and other large equipment
In terms of climate and environment tests for these large-scale equipment, it is only possible to follow the clouds day by day to carry out outdoor natural climate tests, facing problems such as difficult to capture climatic conditions, long test periods, difficult organization and coordination, and high resource consumption.

Method used

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  • An aircraft test comprehensive climate environment simulation system and simulation method
  • An aircraft test comprehensive climate environment simulation system and simulation method
  • An aircraft test comprehensive climate environment simulation system and simulation method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0106] This embodiment is a kind of aircraft test comprehensive climate environment simulation system, such as figure 1 shown, including:

[0107] Test machine 1, test machine 1 is an airplane,

[0108] The laboratory structure system for carrying the testing machine 1, the laboratory structure system includes: a sealed insulation cabin 3, a building structure 2 for fixing the insulation cabin 3 and serving as the laboratory skeleton, the insulation cabin 3 adopts a thickness of 200mm Made of polyurethane sandwich panels, such as figure 2 As shown, the building structure 2 includes from the inside to the outside: a steel structure 22, an outer wall surface 21, a hoisting module 23 on the inner top of the steel structure 22, a bearing ground 25 on the inner bottom of the steel structure 22, and a ground on the bearing ground 25. Drainage 26 and ground mooring 27, the side of building structure 2 is also provided with gate 24,

[0109] The environment simulation system used ...

Embodiment 2

[0118] The present embodiment is the simulation method of a kind of aircraft test comprehensive climate environment simulation system based on embodiment 1, such as Figure 5 shown, including the following steps:

[0119] S1. Low temperature environment simulation

[0120] S1-1. Start the cooling water module 61, the steam boiler 64, and the air supply module 62. The cooling water module 61 is used for heat dissipation of the refrigeration module 41 and the air supply module 62. The steam boiler 64 provides a heat source for the regeneration of the dehumidification and fresh air module 44 of the runner. The air supply module 62 provides high-pressure air for the pneumatic actuator;

[0121] S1-2. Start the air circulation processing module 43, the wheel dehumidification fresh air module 44, the micro positive pressure device 45, the cooling and heating module 42 and the refrigeration module 41 in sequence;

[0122] S1-3. The refrigeration module 41 provides a cold source, an...

Embodiment 3

[0187] The difference between this embodiment and embodiment 1 is:

[0188] The insulation cabin body 3 adopts the polyurethane sandwich panel that thickness is 240mm to make.

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Abstract

The invention provides an aircraft test comprehensive climate environment simulation system and a simulation method, belonging to the technical field of aircraft testing. The simulation system includes: testing machine, laboratory structure system, and environment simulation system. The simulation method includes the following steps: S1, low temperature environment simulation; S2, high temperature environment simulation; S3, temperature daily cycle environment simulation; S4, humidity environment simulation; S5, Solar radiation environment simulation; S6, rain / wind-blown rain environment simulation; S7, snowfall / wind-blown snow environment simulation; S8, fog environment simulation; S9, ice accumulation / freezing rain environment simulation. The invention solves the problem that the existing experimental facilities are generally small in size and relatively single in function, and has the advantages of complete functions, various modules cooperating with each other, and saving the number of equipment.

Description

technical field [0001] The invention relates to the technical field of aircraft testing, in particular to an aircraft testing comprehensive climate environment simulation system and a simulation method. Background technique [0002] Aircraft climatic environment adaptability refers to the ability of an aircraft to realize all its predetermined functions, performance and non-destructive capabilities under the influence of various climatic environments that it is expected to encounter during its lifespan. It is one of the important quality characteristic indicators of an aircraft. The quality characteristics of an aircraft is a comprehensive concept, which includes function, performance, safety, environmental adaptability, reliability, testability, maintainability and support, etc. The climate environment adaptability of an aircraft is one of the quality characteristics of an aircraft. A very important factor, it must rely on experiments and management to ensure. [0003] Air...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 王彬文吴敬涛成竹任战鹏马建军
Owner CHINA AIRPLANT STRENGTH RES INST
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