Aviation high-power composite brushless starting power generation system and control method thereof

A technology for starting power generation and high power, which is used in the direction of controlling generators through magnetic field changes, and can solve problems such as inability to meet AC and DC power consumption, unbalance between starting power supply voltage and generator output voltage, and restricting starting load capacity.

Pending Publication Date: 2021-03-19
BEIJING SHUGUANG AERO ELECTRICAL
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Problems solved by technology

Patent CN106357164A discloses a doubly salient pole high-voltage DC starter power generation system and its control method. The armature windings of the two-stage electrically excited doubly salient pole motor are connected in parallel with the bridge type uncontrolled rectifier circuit respectively, and are used as the power generation output end of the starter power generation system. , in which the three-phase armature windings of the first electrically excited doubly salient motor are respectively connected to the three-phase full-bridge inverter

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  • Aviation high-power composite brushless starting power generation system and control method thereof
  • Aviation high-power composite brushless starting power generation system and control method thereof
  • Aviation high-power composite brushless starting power generation system and control method thereof

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[0069] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Apparently, the described embodiments are some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0070] The features of various aspects of the embodiments of the present invention will be described in detail below. In the following detailed description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. It will be apparent, however, to one skilled in the art that the present invention may be pra...

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Abstract

The invention discloses an aviation high-power composite brushless starting power generation system and a control method thereof and belongs to the technical field of aviation starting and power supply systems. The starting power generation system comprises a starting generator, a power generation controller, a multiplexing starting controller, an AC/DC rectifier, an AC/AC converter, a current detection unit, a first conversion contactor, a second conversion contactor, a DC contactor, an AC contactor, a starting contactor, a first multiplexing contactor and a second multiplexing contactor. Theinvention further discloses a control method of the starting power generation system. A multi-winding, AC/DC dual-output and multiplexing control system configuration is provided, the system weight is reduced, the impact of starting and power generation on components is solved, and system efficiency, reliability and safety are improved.

Description

technical field [0001] The invention discloses an aviation high-power composite brushless starting power generation system and a control method thereof, belonging to the technical field of aviation starting and power supply systems. Background technique [0002] Aviation starter power generation technology is an integrated design that uses the reversible principle of the motor to realize the conversion of electrical energy into mechanical energy and mechanical energy into electrical energy. When the aircraft is started, the electrical energy is converted into mechanical energy by converting the power supply to drive the motor to work in an electric state, driving the engine to rotate to meet the speed requirement, and the engine is ignited. After the engine completes the starting process, the engine drives the motor, and the system converts the mechanical energy into the electrical energy required by the aircraft, and supplies power to the electrical equipment of the aircraf...

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Application Information

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IPC IPC(8): H02P9/36
CPCH02P9/36
Inventor 赵雅周袁静兰冷博阳李洋王华超
Owner BEIJING SHUGUANG AERO ELECTRICAL
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