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Torque test system of analogue simulation of VBV fuel oil driving motor of civil aircraft

A technology for driving motor and torque testing, which is applied in the field of testing systems for civil aircraft components to ensure safety, reliability and stability.

Active Publication Date: 2014-01-08
GUANGZHOU AIRCRAFT MAINTENANCE ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in view of the fact that the original equipment manufacturer has imposed a technical blockade on the production and testing process of VBV fuel-driven motors; how to establish a test platform by itself highlights its significance

Method used

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  • Torque test system of analogue simulation of VBV fuel oil driving motor of civil aircraft

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Experimental program
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Embodiment Construction

[0017] Such as figure 1 A civil aircraft VBV fuel-driven motor simulation torque test system is shown, the torque test system includes a dynamometer 6, a dynamometer control system 5, a torque speed sensor 9, a torque speed parameter acquisition system 10, a VBV fuel drive The motor 12 and the power test bench 13, the dynamometer 6, the torque speed sensor 9, the torque speed parameter acquisition system 10, and the dynamometer control system 5 are respectively electrically connected to the power supply, and the dynamometer control system 5 and the dynamometer 6 are connected through cables. connected, the dynamometer control system 5 is used to control the dynamometer 6 to provide load to the fuel-driven motor 12, and the dynamometer 6 is externally connected with a cooling air source 7, which is used for air cooling and heat dissipation, and improves the load control of the dynamometer 6 stability, the torque speed sensor 9 has two connecting shafts, one of which is connecte...

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Abstract

The invention discloses a torque test system of analogue simulation of a VBV fuel oil driving motor of a civil aircraft. The torque test system comprises a dynamometer machine, a dynamometer machine control system, a torque rotating speed sensor, a torque rotating speed parameter collecting system, the VBV fuel oil driving motor and a power test platform, wherein the dynamometer machine control system is connected with the dynamometer machine through a cable, one connection shaft of the torque rotating speed sensor is connected with the dynamometer machine, the other connection shaft of the torque rotating speed sensor is connected with the VBV fuel oil driving motor, the torque rotating speed sensor is further connected with the external torque rotating speed parameter collecting system, and the VBV fuel oil driving motor is further connected with the power test platform. The torque test system can test torque of the VBV fuel oil driving motor under set pressure difference and rotating speed, the torque is compared with a relative torque reference value, whether the VBV fuel oil driving motor reaches the standard is judged, and therefore whether the VBV fuel oil driving motor is safe and reliable is judged.

Description

technical field [0001] The invention relates to a test system for civil aircraft components, in particular to a torque test system for simulating a VBV fuel-driven motor of a civil aircraft. Background technique [0002] The VBV system plays a vital role in engine operation: during constant engine speed and acceleration, it is directly controlled by the angular adjustment point of the adjustable compressor stator vane VSV: at low speed, the low pressure compressor provides The compressed air flow greatly exceeds the air flow required by the core machine. At this time, the VBV valve opens to release the excess compressed air out of the core machine. engine running needs. When the thrust of the engine is reduced, the VBV valve opens, and when the thrust is rapidly reduced, the VBV valve is fully opened, and the compressed air of the low-pressure compressor LPC is discharged from the core engine. At this time, the VBV plays the role of increasing the air flow in the LPC and im...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01L5/00G01M15/04
Inventor 密世乾刘明德李辉宪郎建军黄华王光宇陈斌黄焯荣王健何志坚钟锦锋丛海峰郑惠忠陈培华
Owner GUANGZHOU AIRCRAFT MAINTENANCE ENG