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Minitype turbo-jet fuel oil control method and device and storage medium

A jet engine and micro-turbine technology, which is used in the fuel control of turbo/propulsion devices, engine components, turbo/propulsion fuel delivery systems, etc., and can solve problems such as the inability to reliably control the fuel of micro-turbo jet engines.

Active Publication Date: 2018-04-13
北京航天宏恩动力技术有限公司
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  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

[0006] In view of this, the technical problem to be solved by the present invention is to provide a micro-turbojet engine fuel control method, device, and storage medium, which solves the problem that the prior art cannot reliably control the fuel oil of a micro-turbojet engine

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  • Minitype turbo-jet fuel oil control method and device and storage medium

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Embodiment Construction

[0021] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the spirit of the disclosure of the present invention will be clearly described below with the accompanying drawings and detailed descriptions. Any person skilled in the art will understand the embodiments of the present invention. , when it can be changed and modified by the technology taught in the content of the present invention, it does not depart from the spirit and scope of the content of the present invention.

[0022] The exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not to limit the present invention. In addition, elements / members with the same or similar numbers used in the drawings and embodiments are used to represent the same or similar parts.

[0023] As used herein, "first", "second", ... etc. do not refer to a particular sequence or order, nor are they used to limit the pre...

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Abstract

The invention provides a minitype turbo-jet fuel oil control method and device and a storage medium, wherein, the control method includes the steps that present rotating speed of a minitype turbo-jetis collected; and the fuel oil supply of the minitype turbo-jet is controlled according to the present rotating speed and a given rotating speed. The minitype turbo-jet fuel oil control method and device and the storage medium can accurately control the minitype turbo-jet to realize the requirements of stability, speediness and accuracy, do not cause overheat or flameout of the minitype turbo-jet,and are safe and reliable.

Description

technical field [0001] The invention relates to the technical field of turbojet engines, in particular to the fuel control technology of micro turbojet engines, specifically a fuel control method and device for micro turbojet engines, and a storage medium. Background technique [0002] Turbojet engine is a kind of turbine engine, which is characterized by completely relying on gas flow to generate thrust, and is usually used as the power of high-speed aircraft. Compared with ordinary turbojet engines, micro turbojet engines have the characteristics of small size and light weight. Therefore, micro turbojet engines have the advantages of precise structure, small size, light weight, and large thrust-to-weight ratio. They are very suitable for target aircraft, reconnaissance , attack, aerial survey and other small UAVs. [0003] In the prior art, the turbojet engine provides thrust for the aircraft, and the requirement of the aircraft to the turbojet engine is to ensure that th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C9/30
CPCF02C9/30
Inventor 姚翠荣熊石仑
Owner 北京航天宏恩动力技术有限公司
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