An aircraft power generation control device

A technology for power generation control and aircraft, which is applied in the fuel control of turbine/propulsion device, charging system, engine components, etc. It can solve the problem of reducing the control accuracy of the system, unable to automatically correct the PID controller, and difficult to meet the high control accuracy of aircraft. requirements, etc., to achieve the effect of strong adaptive ability and good dynamic and static characteristics

Inactive Publication Date: 2011-11-30
UNIV OF ELECTRONICS SCI & TECH OF CHINA
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AI Technical Summary

Problems solved by technology

Since aircraft generator sets are often used in very harsh industrial environments, they are often in variable working conditions. At this time, when ordinary PID control methods are applied to aircraft power generation control devices, the PID control parameters are fixed, and PID cannot be controlled in a random environment. The controller performs automatic correction, which reduces the control accuracy of the system, and it is difficult to meet the high control accuracy requirements of the aircraft

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  • An aircraft power generation control device
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  • An aircraft power generation control device

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Embodiment Construction

[0021] 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.

[0022] figure 1 It is a structural block diagram of a specific embodiment of the aircraft power generation control device of the present invention

[0023] In this example, if figure 1 As shown, the aircraft power generation control device includes an input module 1, an output module 2, and a core processing module 3. The input module 1 sends the collected operating parameters of the aircraft generator set to the core processing module 3, and the core processing module 3 according to The operating parameters output the control quantity to the corresponding actuator to perform the corresponding operation.

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Abstract

The invention discloses an aircraft power generation control device. The high-speed digital input module is used to collect the rotational speed of the driving shaft of the aircraft generator set, and can collect pulse signals with a frequency higher than 100KHz; the high-precision analog input module is used to collect the aircraft generator set. The power generation power and the valve position displacement of the fuel regulating valve, the acquisition accuracy is higher than one ten-thousandth; the PWM output module is used to use the algorithm of PWM current control to output the control amount to the fuel regulating valve to realize the control of the valve opening; The core control module includes an adaptive fuzzy PID control module to control the speed, power and valve position displacement. The invention adopts the self-adaptive fuzzy PID module to control the speed, power and valve position displacement, has strong self-adaptability to environmental changes, and can automatically correct the controller in a random environment, so that the system characteristic changes or is disturbed. , the aircraft power generation system has good dynamic and static characteristics, which meets the control requirements of the aircraft power generation system.

Description

technical field [0001] The invention relates to the technical field of power generation control, in particular to the control of a power generation system using an aero-engine as the driving power of a generator. Background technique [0002] Aircraft power generation technology has been developed in recent years. It is an efficient, energy-saving and environmentally friendly power generation technology that applies a series of transformations to aero-engines (aircraft for short) for ground power generation. The aircraft power generation system includes the aircraft generator set and the aircraft power generation control system. Among them, the aircraft power generation control system is a comprehensive control system that takes the aircraft generator set as the object and involves many disciplines such as control, computer, communication, power, and electric power. , is one of the key technologies of aircraft power generation, in which the aircraft power generation control ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C9/32
Inventor 郑宏徐红兵邹见效李凯
Owner UNIV OF ELECTRONICS SCI & TECH OF CHINA
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