Self-energy feedback type brake apparatus-based airplane braking system and control method thereof

A brake device and brake system technology, applied in the direction of aircraft brake arrangement, weight reduction, etc., to achieve the effects of reducing the number of parts, improving safety, high reliability and maintainability

Inactive Publication Date: 2014-05-21
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] In fact, due to the particularity of the braking system, the existing research on all-electric and power-by-wire braking is not the only improvement idea

Method used

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  • Self-energy feedback type brake apparatus-based airplane braking system and control method thereof
  • Self-energy feedback type brake apparatus-based airplane braking system and control method thereof
  • Self-energy feedback type brake apparatus-based airplane braking system and control method thereof

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Effect test

Embodiment 1

[0031] The invention provides an aircraft brake system based on a self-feeding brake device, such as figure 1 Shown is a schematic structural diagram of the braking system, which includes: an aircraft braking system controller 11, an onboard power supply 12 and a plurality of self-feeding braking devices 13;

[0032] The onboard power supply 12 is respectively connected to each of the self-feeding braking devices 13 for providing electric energy for each of the self-feeding braking devices;

[0033] Each of the self-feeding brake devices 13 includes a transmission mechanism and a hydraulic pump, the transmission mechanism is used to obtain the mechanical energy of the movement of the aircraft wheel connected to the transmission mechanism and transmit it to the hydraulic pump, and the hydraulic pump uses To convert the mechanical energy obtained by the transmission mechanism into hydraulic energy to provide braking power for the brake actuator connected to the hydraulic pump; ...

Embodiment 2

[0053] The present invention also provides a control method for an aircraft braking system based on a self-feeding brake device, comprising: the onboard power supply 12 provides electric energy for each of the self-feeder brake devices 13;

[0054] When the aircraft braking system controller 11 receives the aircraft braking command, it controls each of the self-feeding braking devices 13 to provide braking power to the correspondingly connected braking actuators, wherein: each of the self-feeding braking devices The transmission mechanism obtains the mechanical energy of the movement of the aircraft wheel connected to the transmission mechanism and transmits it to the hydraulic pump of the self-feedback brake device, and each hydraulic pump of the self-feedback brake device makes the self-feedback brake device The mechanical energy obtained by the transmission mechanism is converted into hydraulic energy to provide braking power for the brake actuator connected to the hydraulic...

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PUM

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Abstract

The invention provides a self-energy feedback type brake apparatus-based airplane braking system and a control method of the self-energy feedback type brake apparatus-based airplane braking system. The method comprises the following steps: an airborne power source provides electric energy to each self-energy feedback type brake apparatus; an airplane braking system controller controls each self-energy feedback type brake apparatus and braking actuators which are connected with the corresponding self-energy feedback type brake apparatuses to provide braking power when receiving an airplane braking instruction. The system and the control method have the advantages that the braking system has an integrated structure, and the amount of parts can be reduced due to the high integration of the modules, thus the braking system is extremely high in reliability and maintainability; the braking system is independent of host computer energy sources, and the braking can be completed even when the host computer is under the normal state or the power-free emergency state; the braking system is encapsulated into an electro-hydraulic integrated device interface, a hydraulic pipeline of a pump resource in a resource self-cluster is cancelled, and the weight of the airplane is reduced, so that the safety of the airplane can be improved.

Description

technical field [0001] The invention relates to the field of aircraft braking systems, in particular to an aircraft braking system based on a self-feeding braking device and a control method thereof. Background technique [0002] The aircraft braking system is an important part of modern aircraft, mainly used to dissipate the kinetic energy of the aircraft when it is sliding on the ground, to ensure that the aircraft brakes to stop, to shorten the distance of the aircraft to run, to prevent excessive wear of the wheels, and to cooperate with other airborne The system realizes the turning and parking functions of the aircraft, and is an important system to ensure the safe take-off and landing of the aircraft. Therefore, whether the aircraft braking system can operate normally and reliably is very important. [0003] Whether the aircraft brake system is safe and reliable is directly related to the safety and reliability of the aircraft as a whole. Because the hydraulic brake ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/42
CPCY02T50/40
Inventor 尚耀星刘晓超焦宗夏黄澄
Owner BEIHANG UNIV
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