Whole machine test run method of turboprop engine and engine test run device
An engine and turboprop technology, which is applied in the field of a turboprop engine test run method and an engine test run device, can solve the problems of complex structure, lack, high performance and functional requirements of the turboprop engine, and achieves satisfactory performance parameters, rapid response, and high performance. The smooth effect of each parameter
Active Publication Date: 2020-02-04
AECC HUNAN AVIATION POWERPLANT RES INST
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Problems solved by technology
[0002] Due to the complex structure of the turboprop engine, high performance and functional requirements, the test operation and control are all new methods, and there is relatively little experience that can be used for reference.
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[0038] Typical embodiments embodying the features and advantages of the present invention will be described in detail in the following description. It should be understood that the present invention can have various changes in different embodiments without departing from the scope of the present invention, and that the description and drawings therein are illustrative in nature and not intended to limit the present invention. invention.
[0039] In the following description of various exemplary embodiments of the invention, reference is made to the accompanying drawings, which form a part hereof, and in which are shown by way of example different exemplary structures, systems, and embodiments in which aspects of the invention may be implemented and steps. It is to be understood that other specific arrangements of components, structures, exemplary means, systems and steps may be utilized and structural and functional modifications may be made without departing from the scope o...
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The invention discloses a turbo engine complete machine test run method and an engine test run device. The engine test run device comprises a vehicle station, a torsion measuring device, a dynamometer, a flywheel, an operating system, a PEC simulator and a controller. The vehicle station is provided with a turbo engine. The torsion measuring device is connected with the power output shaft of the turbo engine to measure the torque of the turbo engine. The dynamometer is connected with the torsion measuring device to measure the power of the turbo engine. The flywheel is connected with the dynamometer to simulate the rotational inertia of a propeller. The operating system issues an operating signal. The PEC simulator is electrically connected with the dynamometer and the operating system to convert the operating signal into corresponding rotation speed and torque information and transmit the rotation speed and the torque information to the dynamometer. The controller is electrically connected with the turbo engine and the operating system to issue a corresponding control command to the turbo engine according to the operating signal. According to the invention, test run control and test run measuring of the turbo engine are realized.
Description
technical field [0001] The invention relates to the technical field of aeroengines, in particular to a method for testing a complete turboprop engine and an engine testing device. Background technique [0002] Due to the complex structure of the turboprop engine, high performance and functional requirements, the test operation and control are all new methods, and there is relatively little experience that can be used for reference. Therefore, when the complete machine test run of the turboprop engine is realized on the test bench, it is very difficult to ensure the safe and stable operation of the engine. At the same time, the "General Specifications for Aviation Turboprop and Turboshaft Engines" (GJB242) requires aviation turboprop engines to determine the performance characteristics of the complete engine equipped with power absorption devices, and to verify manual feathering, reverse propeller work, stability. [0003] Therefore, it has become a major technical problem ...
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IPC IPC(8): G01M15/14
CPCG01M15/14
Inventor 张永飞魏秀利杨飞邹植伟贾宗芸刘秀国
Owner AECC HUNAN AVIATION POWERPLANT RES INST