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Cable connecting airplane electric brake controller and electromechanical actuator

A technology for electromechanical actuators and connecting cables, which is applied in the direction of power cables, power cables with shielding layers/conductive layers, cables, etc., which can solve problems such as electromagnetic interference, affecting system control accuracy, ignoring electromagnetic compatibility, etc., to reduce interference Quantity, improve control accuracy, improve the effect of anti-interference ability

Active Publication Date: 2014-08-13
东莞市三航军民融合创新研究院
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] At present, the research in the field of all-electric braking mainly focuses on the anti-skid control rate and motor control method, but ignores the discussion on electromagnetic compatibility. The aircraft all-electric braking system includes both the motor drive signal that generates strong interference and weak position feedback. Signals in one cable will inevitably cause serious electromagnetic interference problems, which will seriously affect the control accuracy of the system. However, domestic aircraft electric brakes are still in the development stage, and the connecting cables used have not been processed.

Method used

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  • Cable connecting airplane electric brake controller and electromechanical actuator
  • Cable connecting airplane electric brake controller and electromechanical actuator
  • Cable connecting airplane electric brake controller and electromechanical actuator

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Embodiment Construction

[0022] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:

[0023] Such as figure 1 , the aircraft electric brake controller and electromechanical actuator connecting cable to which the present invention belongs. The middle is the cable core, which includes the force sensor core cable, the Hall sensor core cable, and the motor three-phase core three sets of insulated core cables. The shielding layer 2 is set on the outside, and both ends are grounded, which can reduce the influence of external interference on the cable core, and reduce the internal interference signal from affecting other external circuits. An outer sheath 1 is provided on the outermost layer to prevent the shielding layer from contacting other conductors and increase the strength of the cable.

[0024] The middle of the force sensor wire core is a conductor 8, which is composed of a power supply wire conductor, a ground wire conductor and a signal wire...

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Abstract

The invention relates to a cable connecting an airplane electric brake controller and an electromechanical actuator. A cable core is arranged in the center and composed of three sets of wires which are three force sensor wire cores, five Hall sensor wire cores and three motor three-phase wire cores respectively, wherein the force sensor wire cores are composed of the supply wire, the ground wire and the signal wire, the Hall sensor wire cores are composed of the supply wire, the ground wire and the three Hall signal wires, and the motor three-phase wire cores are composed of the motor three-phase voltage wires. According to the cable connecting the airplane electric brake controller and the electromechanical actuator, the problem of electromagnetism compatibility of the cable in an airplane electric brake system is solved, the disturbance-resistant capacity of the system is improved, the disturbance variable overlaid on a force sensor feedback signal is greatly reduced through a test, and the control accuracy of an airplane electric brake is improved.

Description

technical field [0001] The invention relates to a connecting cable between an aircraft electric brake controller and an electromechanical actuator. Background technique [0002] The aircraft braking system is a subsystem with relatively independent functions on the aircraft. Its function is to absorb the kinetic energy of the aircraft during landing and taxiing, so as to make the aircraft brake quickly. The all-electric braking system is to use the electronic drive device to drive the brake actuator, and use the electronic transmission line to replace the original oil pipeline to realize the braking and control functions of the brake. [0003] The all-electric braking system has better safety, reliability, maintainability and potentially better braking performance and can greatly reduce the weight of the system. However, it also brings many problems, among which the problem of electromagnetic interference is one of them. [0004] Brushless DC motor (BLDCM, Brushless DC Mot...

Claims

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Application Information

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IPC IPC(8): H01B9/02H01B9/00
Inventor 马瑞卿相里康韩伟健张庆超刘青
Owner 东莞市三航军民融合创新研究院
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