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Comprehensive control method for alternating-current electric pump

A comprehensive control and electric pump technology, applied in the direction of pump control, machine/engine, liquid variable capacity machinery, etc., can solve the problems of small available power, long duration, easy overheating and burning, etc. powerful effect

Inactive Publication Date: 2010-07-28
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to solve the problems of the existing AC electric pumps, such as large starting impact current, long duration, low probability of successful starting, easy overheating and burning, small available power, and lack of fault detection means.

Method used

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  • Comprehensive control method for alternating-current electric pump
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  • Comprehensive control method for alternating-current electric pump

Examples

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Embodiment Construction

[0015] The present invention will be described in further detail below through specific examples.

[0016] A hydraulic pump assembly driven by an 18kW motor is controlled as follows: reduce the starting impulse current by switching stages, shorten the starting time and increase the probability of successful starting by unloading starting, and realize fault self-detection by over-temperature detection.

[0017] When starting, the control signal (5V DC) enters the control box of the AC electric pump to drive the main contactor, so that the induction motor in the AC electric pump is connected to the power supply; at the same time, the control signal passes through a 1.5s delay relay to drive the step-change contactor, The three-phase coil of the induction motor is connected to the power supply in a star connection, and the induction motor starts to rotate.

[0018] At the same time, the control signal drives the unloading valve on the hydraulic pump through a 1.5s delay relay to ...

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PUM

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Abstract

The invention discloses a comprehensive control method for an alternating-current electric pump. The method comprises the following steps: arranging an alternating-current electric pump control box (1) in a system, wherein when the alternating-current electric pump is started, the control box (1) automatically converts the wire connection mode of the three-phase winding of an induction motor (2) in the alternating-current electric pump from delta connection into star connection, thereby realizing reduced voltage starting and reducing the starting current; arranging an electromagnetic unloading valve (3), thereby enhancing the probability of starting success of the alternating-current electric pump and shortening the starting time; and arranging a pump overtemperature switch (5) and a motor overtemperature switch (6), wherein when the pump or a motor is too hot, the overtemperature switches (5, 6) automatically transmit a message to an aircraft control system, thereby realizing automatic fault detection. Compared with the prior art, the method has the advantages of high available power, low starting impulse current, quick starting, high probability of starting success, and capability of realizing automatic fault diagnosis and the like.

Description

technical field [0001] The invention belongs to the design technology of a hydraulic energy system, in particular to a novel comprehensive control method for an AC electric pump. Background technique [0002] When the aircraft AC electric pump source is started, it is generally directly controlled by a contactor. This method is simple in configuration and light in weight, but has the disadvantages of large inrush current amplitude and long duration. When the power of the AC electric pump is large It is easy to cause power failure, which endangers the safety of the aircraft. Therefore, the power of the AC electric pump using this control method is limited; the probability of successful starting is low when starting with load, which will easily cause the pump to burn out and pollute the entire system; when the power supply capacity is limited, The above problems result in the low available power of the AC electric pump, which cannot meet the power demand of the hydraulic syste...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F04B49/06
Inventor 李巍刘红秦成王剑
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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