Aircraft engine compartment fire experiment equipment

A technology for engine compartment and experimental equipment, which is used in engine testing, machine/structural component testing, measuring devices, etc., can solve the problem of not being able to verify the effectiveness of fire extinguishing systems at the same time, and achieve the effect of saving equipment investment.

Pending Publication Date: 2018-06-15
UNIV OF SCI & TECH OF CHINA +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The present invention can solve the problem that the fire extinguishing system effectiveness verification cannot be carried out at the same time on the existing power cabin fire prevention system test bench, the fire extinguishing effectiveness verification experiment of the new halon substitute fire extingu...

Method used

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  • Aircraft engine compartment fire experiment equipment
  • Aircraft engine compartment fire experiment equipment
  • Aircraft engine compartment fire experiment equipment

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Embodiment Construction

[0033] The present invention will be further described below through implementation examples in conjunction with the accompanying drawings, but the implementation scope of the present invention is not limited to this arrangement.

[0034] Such as figure 1 As shown, a kind of aircraft engine compartment fire experiment equipment of the present invention comprises air inlet, cabin body, exhaust port, observation window, engine dummy, heating assembly, engine compartment congestion simulation device, fire extinguishing agent concentration test interface, Oil pool fire module, spray fire simulator interface, temperature measurement module, air velocity measurement module, pressure measurement module, laser flow field measurement module and cabin support, the above parts are composed of mechanical connections, electrical cables and process gas path connections an experimental device.

[0035] In this embodiment, the maximum dimensions of the length×width×height of the experimental...

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Abstract

The invention discloses a piece of aircraft engine compartment fire experiment equipment which can be used to carry out an experiment for engine compartment fire dynamics research and carry out experimental verification of an aircraft fire prevention system. The equipment comprises an air inlet, a compartment body, an air outlet, an observation window, fake engine parts, a heating component, an engine compartment congestion part simulation device, a fire extinguishing agent concentration test interface, an oil pool fire module, a spray fire simulator interface, a temperature measurement module, an airflow velocity measurement module, a pressure measurement module, a laser flow field measurement module and a compartment body bracket. Compared with the prior art, the aircraft engine compartment fire experiment equipment can be used to carry out an experiment for aircraft engine compartment fire dynamics research and simulate the influence of the engine surface temperature on the experimental boundary conditions in the compartment.

Description

technical field [0001] The invention relates to the technical field of test and verification of an aircraft fire protection system, in particular to an aircraft engine compartment fire test equipment. Background technique [0002] With the continuous development of the aviation industry and the advancement of science and technology, more and more attention has been paid to the safety of aircraft, especially the safety and airworthiness of aircraft are very important. Aircraft engine compartment fire protection is an important part of the aircraft fire protection system, and the scientific research and effectiveness of the aircraft engine compartment fire protection system need to be verified through experiments. [0003] Existing aircraft engine compartment fire protection system experimental equipment, such as the test cabin described in the Chinese patent "A Fire Extinguishing Test Assembly for Aircraft Engines" (CN105865797A), can only carry out the test of fire extinguis...

Claims

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Application Information

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IPC IPC(8): G01M15/00
CPCG01M15/00
Inventor 陆松刘长城张和平赵军超陈龙杨维华
Owner UNIV OF SCI & TECH OF CHINA
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