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Aero-engine salt mist sensitivity test device

An aero-engine and test device technology, which is applied in engine testing, jet engine testing, gas turbine engine testing, etc., can solve problems such as low safety factor, high cost, and inability to meet the needs of naval engine development, and achieve faster fouling. Effect

Active Publication Date: 2019-07-26
BEIJING INST OF STRUCTURE & ENVIRONMENT ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The salt spray test in the salt spray test chamber is a "static" salt spray test to investigate the effect of salt spray settlement on the corrosion of static products, which can only simulate the corrosion resistance of components and cannot meet the development needs of naval engines
[0004] Due to the lack of corresponding engine salt spray sensitivity test equipment, the comprehensive performance of the engine affected by the marine environment can only rely on numerical simulation and flight tests, and numerical simulation must rely on experimental verification to ensure its accuracy. Flight tests are subject to real climate conditions. The impact of the change is too large to conduct a repeatable test, and the cost is high and the safety factor is low

Method used

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  • Aero-engine salt mist sensitivity test device
  • Aero-engine salt mist sensitivity test device
  • Aero-engine salt mist sensitivity test device

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Embodiment Construction

[0031] See Figure 1-2 , An aeroengine salt spray sensitivity test device of the present invention includes an air supply unit, a temperature adjustment unit, a humidity adjustment unit, a salt spray mixing adjustment unit, a dynamic salt spray sampling unit, a salt spray protection cabin unit, Exhaust unit; each unit is respectively connected to the measurement and control unit; the air supply unit supplies air for the aero engine to be tested to meet the air intake of the aero engine to be tested during operation; in the air supply unit, air is sent to the air supply through the air supply pipeline The fan unit 1 is pressurized, and the pressurized compressed air enters the air filter device 2 for filtration and then is sent to the temperature adjustment unit through the main pipe; the air supply pipe has a thermal insulation structure, the inner layer is made of non-metallic materials, and the middle layer is polyurethane foam Heat insulation, the outer layer is wrapped with...

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Abstract

The invention provides an aero-engine salt mist sensitivity test device. The test device comprises an air supply unit, a temperature regulation unit, a humidity regulation unit, a salt mist mixed regulation unit, a dynamic salt mist sampling unit, a salt mist protective cabin unit and an exhaust unit, wherein all the units are sequentially connected and are connected to a measurement and control unit respectively. The test device simulates typical marine environmental climates, such as temperature, humidity and salt mist, which a whole aero-engine undergoes during operation in a marine environment, and therefore performance testing and assessment of the aero-engine under the influence of the integrated environment are realized. Besides, the test device also can perform precise control andfree combination on the temperature, humidity and salt content of the simulated environment, and therefore testing on multiple environmental profiles of the aero-engine is realized.

Description

Technical field [0001] The invention relates to an aeroengine salt spray sensitivity test device, which belongs to the field of engine test. Background technique [0002] When flying in a coastal environment, aero engines will be severely affected by the marine climate environment and the induced environment. The main influencing factors include temperature, humidity, salt spray, rain, acidic atmosphere, etc. The most prominent ones are temperature, humidity, and salt. Foggy environment. The harsh and changeable climatic environment such as high temperature, damp heat and salt spray in the ocean and coastal areas will cause severe corrosion to the flow components of the engine, which will cause the deterioration of the aerodynamic performance of the engine and affect the structural strength and fatigue life of the engine; On the other hand, higher salt content will be absorbed by the liquid film on the engine surface when the engine is working, which will cause fouling on the en...

Claims

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Application Information

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IPC IPC(8): G01M15/14G01M15/02
CPCG01M15/02G01M15/14
Inventor 马平昌刘玥高飞李红李亚男芮鹏
Owner BEIJING INST OF STRUCTURE & ENVIRONMENT ENG
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