Aeroengine generating system

A technology for power generation systems and aircraft, which is applied in the direction of charging systems, turbine/propellant fuel delivery systems, and control of generators through magnetic field changes. It can solve problems such as unfavorable control system expansion, heavy computer load, and system inoperability. High control accuracy, improved reliability, and reduced maintenance costs

Inactive Publication Date: 2010-06-16
UNIV OF ELECTRONIC SCI & TECH OF CHINA
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AI Technical Summary

Problems solved by technology

[0005] There are many shortcomings in the centralized control system currently used for aircraft power generation, among which there are three main shortcomings: 1. Reduced reliability
The full authority digital electronic controller (FADEC) in the control system not only needs to realize all the main functions such as signal acquisition, processing, control calculation and control signal output,

Method used

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Embodiment Construction

[0015] In order to better understand the present invention, the present invention will be described in more detail below in conjunction with the accompanying drawings and specific embodiments. In the following description, when detailed descriptions of existing prior art may obscure the subject matter of the present invention, such descriptions will be omitted here.

[0016] figure 1 It is a structural block diagram of a specific embodiment of the aircraft power generation system of the present invention

[0017] In this example, if figure 1 As shown, the aircraft power generation system includes two parts: the aircraft generator set I and the aircraft power generation control system II.

[0018] The aircraft generating set 1 includes an aircraft 101, a generator 102, an electric / exciter 103 and a fuel regulating valve 104, and the electric / exciter 103 is coaxially connected with the generator 102 and the aircraft 101. The aircraft 101 mainly includes a compressor C, a comb...

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Abstract

The invention discloses an aeroengine generating system. An aeroengine generating set comprises an electric motor/exciter which is coaxially connected with a generator and an aircraft in the aeroengine power generating set; an aeroengine generating control system comprises a main controller, a starting excitation controller and a fuel adjusting controller which form a distributed bus control network in a mode of a bus; each controller is an independent node on the bus; and the main controller is a main node, and the fuel adjusting controller and the starting excitation controller are slave nodes. Each control part is designed in a modularizing mode and controlled in a distributed mode, so that the individual and general safe, economic, stable and reliable operation is realized in the aeroengine generating system, and the aeroengine generating set has the advantages of fast starting, smooth transition, high control precision, simple operation, strong adaptability and high reliability. Compared with a centralized control system in the prior art, each controller has the control function, and a universal standard device can be adopted, so that the aeroengine generating system is easy to expand and the maintenance cost is greatly reduced.

Description

technical field [0001] The invention relates to a power generation system, in particular to an aircraft power generation system using an aeroengine as the driving power of a generator. Background technique [0002] The aircraft power generation system is a high-efficiency, energy-saving and environmentally friendly power generation device that adapts the aeroengine (aircraft for short) to power generation on the ground after a series of modifications, including the aircraft generator set and the aircraft power generation control system. Among them, the aircraft The power generation control system is an integrated control system that takes aircraft generator sets as the object and involves control, computer, communication, power, electric power and many other disciplines. It is one of the key technologies and an important part of aircraft power generation. [0003] The development of aircraft power generation control technology has gone through stages of hydraulic mechanical ...

Claims

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Application Information

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IPC IPC(8): F02C9/32H02P9/14H02H7/06
Inventor 郑宏徐红兵李凯
Owner UNIV OF ELECTRONIC SCI & TECH OF CHINA
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