Aircraft test comprehensive climate environment simulation system and simulation method
A climate environment and simulation system technology, which is applied in the direction of aircraft component testing, etc., can solve problems such as large resource consumption, long test cycle, and difficult organization and coordination, and achieve low investment and operation costs, flexible system use, and good scalability Effect
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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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