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Starting program control device and control method of turbofan

A technology for a turbofan engine and a starter, which is applied to the starting of the engine, the starting of the turbine/propulsion device, the ignition of the engine, etc., can solve the problems of high manufacturing cost, high weight, low timing accuracy, etc., and achieves low manufacturing cost and weight. Lightweight, high timing accuracy

Active Publication Date: 2018-10-26
CHINA HANGFA SOUTH IND CO LTD
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  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The invention provides a turbofan engine starting program control device and control method to solve the technical problems of the existing turbofan engine using a motor-type cam timing mechanism to realize the starting program control, resulting in heavy weight, high manufacturing cost, and low timing accuracy

Method used

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  • Starting program control device and control method of turbofan
  • Starting program control device and control method of turbofan
  • Starting program control device and control method of turbofan

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Embodiment Construction

[0039] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0040] refer to figure 1 , the preferred embodiment of the present invention provides a kind of starting procedure control device of turbofan engine, comprises power supply circuit, electromagnetic relay group and time relay group, and power circuit is connected with electromagnetic relay group and time relay group; Time relay group comprises multiple The time relay, the electromagnetic relay group includes a plurality of electromagnetic relays, and the plurality of time relays are connected to the plurality of electromagnetic relays correspondingly, and are used to control the on or off of the corresponding electromagnetic relays at the set time; the plurality of electromagnetic relays are res...

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Abstract

The invention discloses a starting program control device and a control method of a turbofan. The starting program control device comprises a power circuit, an electromagnetic relay set and a time relay set, wherein the power circuit is connected with the electromagnetic relay set and the time relay set; the time relay set comprises multiple time relays; the electromagnetic relay set comprises multiple electromagnetic relays; the multiple time relays are correspondingly connected with the multiple electromagnetic relays and used for controlling switch-on or switch-off of corresponding electromagnetic relays at set time; and the multiple electromagnetic relays are respectively used for being connected to corresponding starting accessories of the turbofan. The starting program control deviceis small in size, light and low in manufacturing cost, the timing accuracy of the time relays is high, and thus the whole control device and the control method are high in control precision and highin reset and response speeds, an engine can control starting, cold working and false starting of the turbofan according to set programs and logic, and performance indexes meet the requirements.

Description

technical field [0001] The invention relates to the technical field of turbofan engine startup control, in particular, to a turbofan engine startup program control device and control method. Background technique [0002] The turbofan engine is mainly used to generate pull or thrust to provide flight power for the flight of the aircraft. At the same time, it provides electricity for the electrical equipment on the aircraft and provides air source for air-conditioning equipment and other air-consuming equipment. It is the heart of the aircraft. [0003] The starting procedure control method is to control the work of the starting accessories of the engine according to the specified timing and logic, and at the end of the starting, the starting accessories will stop working, so as to ensure that the automatic starting (including air starting), cold running and false starting of the engine follow the established procedures Finish. Due to the harsh working environment of the star...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/26F02C7/266F02C9/00
CPCF02C7/26F02C7/266F02C9/00
Inventor 陈伦祥王山峰许丹张达方柳星剑任广华琚浩
Owner CHINA HANGFA SOUTH IND CO LTD
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