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Aero-engine power extraction system with on-off function and debugging method thereof

An aero-engine and extraction system technology, applied in the field of aero-engine power extraction system and its debugging, to achieve the effects of improving operating performance, reducing performance deterioration, and expanding power extraction capability

Active Publication Date: 2022-05-13
AECC SHENYANG ENGINE RES INST
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] The purpose of this application is to provide an aeroengine power extraction system with on-off function and its debugging method, so as to solve at least one problem existing in the prior art

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  • Aero-engine power extraction system with on-off function and debugging method thereof
  • Aero-engine power extraction system with on-off function and debugging method thereof

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Embodiment Construction

[0052]In order to make the purpose, technical solution and advantages of the application more clear, the technical solution in the embodiment of the application will be described in more detail below in conjunction with the drawings in the embodiment of the application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the application. The embodiments described below by referring to the figures are exemplary, and are intended to explain the present application, and should not be construed as limiting the present application. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this application. Embodiments of the present application will be described in detail below in conjunction with the...

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Abstract

The invention belongs to the field of aero-engines, and particularly relates to an aero-engine power extraction system with an on-off function and a debugging method thereof. Comprising a high-pressure shaft power extraction module arranged on a turbofan engine system; the low-voltage shaft power extraction module is arranged on the turbofan engine system, and the low-voltage shaft power extraction module comprises a power output shaft and a clutch device, and the power output shaft is arranged at the front end of a low-voltage shaft fan and used for driving a load system; according to the clutch device, connection and disconnection of the load system and the turbofan engine system are achieved through relative movement of a built-in active friction plate and a built-in passive friction plate. According to the invention, power extraction of a larger quantity level can be realized, the operation performance of the engine is improved, the increasing requirements of airplanes are met, and the increase of the design difficulty of parts and the deterioration of the performance caused by a single power source are reduced.

Description

technical field [0001] The application belongs to the field of aero-engines, and in particular relates to an aero-engine power extraction system with an on-off function and a debugging method thereof. Background technique [0002] As the power source of the aviation platform, the aero engine not only provides the flight platform with the power required for air flight, but also provides the required electrical energy for various electrical equipment and systems on the aircraft. Since the development of aero-engines, most conventional twin-rotor turbofan engines have a high-pressure shaft that drives the central transmission unit to output power, and is connected to a generator to realize the conversion of energy from mechanical energy to electrical energy. With the development of aviation technology, airborne avionics equipment is developing towards high power and high energy consumption. At the same time, it must meet higher technical indicators such as low noise and low emi...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/36F02C9/00
CPCF02C7/36F02C9/00
Inventor 袁长龙芮长胜苏桂英郝燕平
Owner AECC SHENYANG ENGINE RES INST
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