Dual-active bridge-based starting power generation system

A technology of starting power generation and dual active bridges, applied in the field of aviation power supply, can solve the problems of reducing the reliability of aircraft operation, the complexity of control network, communication network, the weight and volume of airborne equipment, etc., to improve system capacity and electric energy. Quality, light weight and long life effect

Inactive Publication Date: 2018-04-17
SHAANXI AVIATION ELECTRICAL
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional starter generator system uses the starter controller to drive the starter generator to start the engine. After the start is completed, the starter controller is disengaged, and the generator controller controls the starter generator to generate electricity. The on-board actuation system needs to be equipped with an additional motor controller. It causes the complexity of the control network and communication network, and makes the weight and volume of the aircraft on-board equipment larger, reducing the reliability of the aircraft operation

Method used

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  • Dual-active bridge-based starting power generation system
  • Dual-active bridge-based starting power generation system

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Embodiment Construction

[0017] The present invention is described in detail below in conjunction with accompanying drawing:

[0018] attached figure 1 A block diagram of a 270V high voltage DC starter generator system is described. The system includes engine, high-speed permanent magnet synchronous motor, starter generator controller, starter power supply, electric load, etc.

[0019] The system first works in the starting running state, and the engine acts as the mechanical load of the permanent magnet synchronous motor. Turn on the 270V DC starting power supply, perform power conversion through the starter generator controller, provide three-phase AC power to the three-phase armature winding of the high-speed permanent magnet synchronous motor, generate electromagnetic torque, and start the engine to the disengagement speed.

[0020] After the starting process is over, disconnect the ground power supply and connect the electrical load. At this time, the engine starts to serve as the driving ener...

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Abstract

The invention belongs to the technical field of an aviation power supply, and relates to a dual-active bridge-based starting power generation system. A 270V high-voltage direct current is used as a power supply mechanism of the starting power generation system, a starting power generator of the starting power generation system employs a high-speed permanent-magnet synchronous motor, and the starting and power generation functions can be achieved by a bidirectional running principle of the motor. A rare-earth permanent-magnet material employed by the permanent-magnet motor has high magnetic energy product, the weight of the motor can be obviously reduced, the volume of the motor is reduced, and meanwhile, the motor is long in service lifetime and high in reliability and maintenance. A high-speed permanent-magnet synchronous motor is mature in technology, digital control is employed, and output torque control of the motor can be achieved; and the starting power generation system has theadvantages of large capacity, high power generation efficiency, small size, light weight, high reliability, low life cycle cost and the like.

Description

technical field [0001] The invention belongs to the technical field of aviation power supplies, and relates to a starting power generation system based on dual active bridges. Background technique [0002] At present, in the aviation power system at home and abroad, the application of 28V low-voltage DC power system is relatively mature, while the AC power system and high-voltage DC system are mostly in the research stage. The traditional starter generator system uses the starter controller to drive the starter generator to start the engine. After the start is completed, the starter controller is disengaged, and the generator controller controls the starter generator to generate electricity. The on-board actuation system needs to be equipped with an additional motor controller. It causes the complexity of the control network and the communication network, and makes the weight and volume of the airborne equipment of the aircraft larger, reducing the reliability of the aircraf...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02P6/20H02P6/28H02P21/22H02P25/022H02P27/08H02K7/20H02K7/18
CPCH02K7/1807H02K7/20H02P6/20H02P6/28H02P21/22H02P25/024H02P27/08
Inventor 赵勇陈亚平姜宇侯艳雪李真贵
Owner SHAANXI AVIATION ELECTRICAL
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