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A turbofan engine control system and method based on rapid prototype

A turbofan engine and control system technology, applied in machine/engine, gas turbine engine testing, engine ignition, etc., can solve the problems of unsatisfactory rapid engine development, high cost of electronic controller, poor versatility, etc., and shorten the development cycle , low cost, and the effect of reducing development costs

Active Publication Date: 2020-07-21
BEIJING POWER MACHINERY INST
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  • Abstract
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  • Claims
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Problems solved by technology

The traditional turbofan engine control system is developed with the electronic controller as the core, but the development of a dedicated engine electronic controller is costly, long-term, and poor in versatility, which cannot meet the needs of rapid engine development

Method used

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  • A turbofan engine control system and method based on rapid prototype
  • A turbofan engine control system and method based on rapid prototype
  • A turbofan engine control system and method based on rapid prototype

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Embodiment Construction

[0038] In order to make the purpose, content, and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0039] figure 1 It is a schematic diagram of a turbofan engine control system based on a rapid prototype, and its system consists of a rapid prototype 1, an electric pump 2, an electrical control box 3, a speed sensor 4, a total incoming flow temperature Tt2 sensor 5, and an exhaust temperature Tt6 Sensor 6, electric ignition 7, gunpowder starter 8, igniter 9, engine 10, host computer 11.

[0040] Wherein, the rotational speed sensor 4, the Tt2 sensor 5, and the Tt6 sensor 6 are respectively used to measure the physical rotational speed N of the engine 10, the total incoming flow temperature Tt1 and the exhaust gas temperature Tt6;

[0041] The electrical control box 3 includes an F / V conversion module and a signal am...

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Abstract

The invention relates to a turbofan engine control system and method based on a rapid prototype, and belongs to the technical field of engines. By means of the turbofan engine control system and method, the turbofan engine control system is established by using the universal rapid prototype, and various control functions such as engine oil supply, ignition and protection are achieved. Meanwhile, the system has good versatility, strong expandability, the short development cycle and low cost, is suitable for the rapid development of engine control systems in the early development stage, can greatly reduce the development cost and can shorten the development cycle.

Description

technical field [0001] The invention belongs to the technical field of engines, and in particular relates to a rapid prototype-based turbofan engine control system and method. Background technique [0002] The engine control system is the core component of the turbofan engine, which is used to realize engine control law calculation, fuel control, ignition control and other functions. The traditional turbofan engine control system is developed with the electronic controller as the core, but the development of a dedicated engine electronic controller is costly, long-term, and poor in versatility, which cannot meet the needs of rapid engine development. Contents of the invention [0003] (1) Technical problems to be solved [0004] The technical problem to be solved by the present invention is: how to design a turbofan engine control system and method that can satisfy multiple control functions of the engine. [0005] (2) Technical solutions [0006] In order to solve the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C9/48F02C7/26F02C7/266F02C7/272G01M15/02G01M15/14
CPCF02C7/26F02C7/266F02C7/272F02C9/48G01M15/02G01M15/14
Inventor 卢彬唐玉臣
Owner BEIJING POWER MACHINERY INST
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