A simulation method and device for a common DC bus type aircraft starting and generating system

A technology of starting power generation and system simulation, which is applied in the field of aviation electrical systems, and can solve problems such as being unable to supply power from DC, failing to meet test requirements, and only being able to simulate motor loads.

Active Publication Date: 2020-07-10
HUAZHONG UNIV OF SCI & TECH
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  • Description
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Problems solved by technology

[0007] Aiming at the above defects or improvement needs of the prior art, the present invention provides a method and device for simulating a common DC bus type aircraft start-up power generation system, thereby solving the problems in the prior art that cannot be powered by DC and can only simulate without a motor driver. Motor load, technical problems that cannot meet the test requirements

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  • A simulation method and device for a common DC bus type aircraft starting and generating system
  • A simulation method and device for a common DC bus type aircraft starting and generating system
  • A simulation method and device for a common DC bus type aircraft starting and generating system

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[0035]In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0036] figure 1 It is a structural diagram of an aircraft starting and generating system simulation device according to an embodiment of the present invention. Such as figure 1 As shown, the aircraft starter generator system simulation device includes a DC power supply 1 , a starter generator control converter 2 , a starter generator simulator 3 , a circulating current suppression reactor 4 , a...

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Abstract

The invention discloses a common direct current bus type aircraft starting power generation system simulating method and device. The simulating device is used for simulating the starting and power generation processes of an aircraft starting and power generation system, and testing the aircraft starting and power generation system during research, development and testing phases. The simulating device comprises a direct current power supply, a starting generator control converter, a starting generator simulator, a circulating current suppression reactor, a starting generator simulator control system and a host computer. The invention further discloses the simulating method of the common direct current bus type aircraft starting power generation system simulating device. According to the invention, the simulating method and device simulate the starting and power generation processes of an aircraft; the parameters of the device can be flexibly modified; the power energy loss is small; a huge cooling device is omitted; and the lead time and the development cost are shortened.

Description

technical field [0001] The invention belongs to the field of aviation electrical systems, and more specifically relates to a method and device for simulating a common DC bus type aircraft starting and generating system. Background technique [0002] With the rapid development of the aviation industry, the aircraft is developing in the direction of multi-electricity and full-electricity, and the aircraft starter power generation system is one of the key equipment for multi-electricity and full-electricity. At this stage, the test of the aircraft starter generator system mainly uses the actual starter generator for testing. During the starting process, the mechanical load carried by the starter is usually a synchronous generator, and the load torque required by the starter is generated by controlling the output power of the synchronous generator. Such a test system has complex system, poor reliability, high hardware cost, The characteristics of low power utilization. In the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01R31/34
CPCG01R31/34
Inventor 蒋栋朱磊莱昂·托尔伯特曲荣海
Owner HUAZHONG UNIV OF SCI & TECH
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