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Aviation fuel adjusting and testing system

A technology for aviation fuel and testing system, applied in the field of aviation testing, can solve the problems of low efficiency, loss of service life of fuel adjustment system, long detection time and so on

Inactive Publication Date: 2016-01-20
CHINA AIRCRAFT MAINTENANCE & ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Low efficiency: the detection process is complicated, there are many test personnel, labor intensity is high, the detection time is long, fuel consumption is serious, and the efficiency is low. Repeated operations caused by misjudgment and missed detection also consume the service life of the fuel adjustment system

Method used

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  • Aviation fuel adjusting and testing system

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Embodiment Construction

[0013] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.

[0014] The invention provides an aviation fuel adjustment test system, such as figure 1 As shown, it includes a fuel tank 1, an oil pressure regulating unit, an air pressure regulating unit, a fuel regulating unit 6 and a pressure display unit; the fuel tank 1 is connected to the oil pump 3 through a pipeline through the oil filter 2, and the oil pump 3 is connected to the inlet of the one-way valve 4, The outlet of the check valve 4 is connected to the oil pressure regulating unit, the oil pressure regulating unit is connected to the fuel regulating unit 6 , the fuel regulating unit 6 is connected to the air pressure regulating unit, and the air pressure regulating unit is connected to the air source 5 .

[0015] The fuel adjustment unit 6 includes a first port 10, a second port 11, a third port 12, a fourth port 13, a fifth port 14 ...

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Abstract

The invention provides an aviation fuel adjusting and testing system, which comprises a fuel tank, a fuel pressure adjusting unit, a gas pressure adjusting unit, a fuel adjusting unit and a pressure display unit, wherein the fuel tank is connected with a fuel pump through a fuel filter via a pipeline, the fuel pump is connected with an inlet of a one-way valve, an outlet of the one-way valve is connected with the fuel pressure adjusting unit, the fuel pressure adjusting unit is connected with the fuel adjusting unit, the fuel adjusting unit is connected with the gas pressure adjusting unit, and the gas pressure adjusting unit is connected with a gas source. By utilizing the aviation fuel adjusting and testing system, manpower cost can be greatly reduced, the aviation fuel adjusting and testing system is high in accuracy rate and convenient to move, is suitable for tests in various places, has the advantages of rapid connection, high-speed data acquisition, small occupied space and convenient moving, is suitable for texting an aviation aircraft fuel adjusting system, practically increases testing efficiency of the aviation aircraft fuel adjusting system, and ensures accuracy of tests.

Description

technical field [0001] The invention relates to the field of aviation testing, in particular to an aviation fuel adjustment testing system. Background technique [0002] The fuel regulation system is an important part of the aircraft engine control system. With the improvement of aero-engine control accuracy requirements, the performance of the fuel regulation system is particularly important. In addition, the performance failures that are often encountered in practice, such as over-temperature, over-rotation, speed swing, etc., are often caused by regulator failures. Therefore, the research on the detection of aero-engine fuel control system has very important engineering significance. In view of the intricate characteristics of the working mechanism of the aero-engine fuel control system, it is impossible to realize the detection and diagnosis of corresponding faults without a thorough understanding and study of the engine. [0003] The aviation fuel adjustment test sys...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M15/00
Inventor 何丹陈怀宇申炳龙汪建民孟文辉刘珏伶
Owner CHINA AIRCRAFT MAINTENANCE & ENG