Control method of airplane starting and generating integrated motor

A control method and aircraft technology, applied in aircraft-related fields, can solve problems such as harsh working conditions, aircraft starting, transition conversion, strategy research on power generation control, complex electromagnetic environment, etc., to achieve the effect of ensuring safety

Active Publication Date: 2020-11-06
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The aircraft environment has a more complex electromagnetic environment and harsher working conditions than ground vehicles, and it is impossible to directly learn from the research results of the starter motor in the automotive field
At present, there are many researches on the structure, materials and semiconductor devices of SG motors in the aviation field at home and abroad, but there is no research on the strategy of starting, transition conversion and power generation control of the whole aircraft.

Method used

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  • Control method of airplane starting and generating integrated motor
  • Control method of airplane starting and generating integrated motor
  • Control method of airplane starting and generating integrated motor

Examples

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Embodiment Construction

[0043] A method for controlling an aircraft starter motor, specifically comprising the following steps:

[0044] S1, start mode control

[0045] In the starting mode, the coordinate change of the current needs to be carried out first. The current waveform in the natural coordinate system (abc) is converted into a synchronous rotating axis (dq), and at this time the measured value is compared with the reference value and can be adjusted without error through the PI controller. figure 1 Shown is the relationship between the static abc coordinate system, the static αβ coordinate system and the rotating dq coordinate system.

[0046] In order to get the variables in the dq coordinate system. Firstly, the variable x in the stationary abc coordinate system is transformed by Clarke transformation of equal power abc Transform to the static αβ coordinate system, and then use the Park transformation to transform the variables in the static αβ coordinate system to the rotating dq coor...

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PUM

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Abstract

The invention belongs to the related technical field of airplanes, and particularly relates to a control method of an airplane starting and generating integrated motor, which comprises the following steps that S1, in a starting mode, firstly, coordinate change needs to be carried out on current; a current waveform under a natural coordinate system is converted into a synchronous rotating shaft, and error-free adjustment can be realized through a PI controller after a measured value is compared with a reference value; S2, SG transition control comprises control of connection and disconnection of a ground power supply, conversion of a closed-loop control strategy and connection and disconnection of an equipment load switch; and S3, in the generating mode, the maximum direct-current voltage output by the SG is limited by the bus voltage. The invention provides a set of complete control strategy of the airplane starting and generating integrated motor. Therefore, the SG can provide enoughkinetic energy when the airplane engine is started, the safety of transition conversion can be guaranteed, the generating mode can be smoothly switched to, high-quality electric energy is provided forthe whole airplane, and technical support is provided for the application of the starting and generating integrated motor to a multi-electric airplane and a full-electric airplane.

Description

technical field [0001] The present application belongs to the technical field related to aircraft, and in particular relates to a method for controlling an aircraft starter motor. Background technique [0002] In order to meet the increasing demand of electric load, reduce aircraft emissions, improve fuel economy, reduce the total system cost, and adapt to the development of aerospace industry, the concept of More Electronic Aircraft (MEA) has been proposed at home and abroad. The starter-generator system (starter-generator, SG) is one of the key subsystems of the MEA. In the starting mode, the SG can be used to start the engine or the auxiliary power unit. In the generating mode, the SG operates as a generator to provide electrical energy for the whole machine. In the past ten years, the continuous increase in the capacity of power generation subsystems and power conversion electronic equipment has provided conditions for the electric starting of engines. [0003] As an in...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02P21/22H02P9/02H02P9/30H02P101/30
CPCH02P9/02H02P9/30H02P2101/30H02P21/22
Inventor 李红邓乐武莫文静罗强张永强徐龙
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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