Double-switch-valve-based self-powdering brake apparatus and system

A braking device and braking system technology, which is applied in the field of self-feeding braking devices and systems, can solve problems such as the inability to continue to complete the braking function and the failure of self-feeding braking devices, so as to avoid poor pollution resistance and reduce the flow required for braking , the effect of reducing the volume

Active Publication Date: 2016-03-02
北京航辰机载智能系统科技有限公司
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AI Technical Summary

Problems solved by technology

When the taxiing speed of the aircraft drops to a certain level, even the entire self-feeding braking device fails, and the braking function cannot be continued.

Method used

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  • Double-switch-valve-based self-powdering brake apparatus and system
  • Double-switch-valve-based self-powdering brake apparatus and system
  • Double-switch-valve-based self-powdering brake apparatus and system

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Embodiment Construction

[0027] The embodiments of the present application are described below with reference to the drawings. The elements and features described in one drawing or one embodiment of this application may be combined with the elements and features shown in one or more other drawings or embodiments. It should be noted that, for the purpose of clarity, representations and descriptions of components and processes that are not related to the present application and known to those of ordinary skill in the art are omitted from the drawings and descriptions.

[0028] See figure 1 As shown, this is a schematic structural diagram 100 of a self-powered braking device based on a dual on-off valve according to a first embodiment of the application.

[0029] In this embodiment, the self-feeding brake device based on dual on-off valves includes a transmission mechanism 110, a hydraulic pump 120, a first on-off valve 131, a second on-off valve 132, and a brake assembly 140.

[0030] The transmission mechani...

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Abstract

The present application relates to a double-switch-valve-based self-powdering brake apparatus and a system. The apparatus comprises a drive mechanism, a hydraulic pump, a first switch valve, a second switch valve and a brake assembly; the oil inlet port of the first switch valve is connected with the oil outlet port of the hydraulic pump, a control end of the first switch valve opens or closes the oil outlet port of the first switch valve on the basis of a first control instruction received by the control end; the oil inlet port of the second switch valve is connected with the oil outlet port of the first switch valve, the oil outlet port of the second switch valve is connected with the oil inlet port of the hydraulic pump, the second switch valve opens or closes the oil outlet port of the second switch valve on the basis of a second control instruction received by the control end; the brake assembly is connected with the oil outlet port of the first switch valve for generating a brake actuation signal on the basis of the flow rate of the oil outlet port of the first switch valve. The double switch valve-based self-powdering brake apparatus and system can avoid the problems of poor contamination resistance and serious oil leakage of the self-powdering brake device in the prior art.

Description

Technical field [0001] This application relates to the technical field of aircraft brake systems, in particular to a self-feeding energy brake device and system based on dual on-off valves. Background technique [0002] Aircraft brake system is an important system to ensure aircraft safety. It is mainly used to dissipate the kinetic energy of the aircraft when taxiing on the ground, to ensure that the aircraft brakes to stop, shorten the taxi distance of the aircraft, prevent excessive wear of the wheels, and can cooperate with other airborne systems to realize the turning and parking functions of the aircraft. The important system for safe take-off and landing of aircraft is an important part of modern aircraft. [0003] At present, hydraulic brake systems are widely used in various types of aircraft due to their high power-to-mass ratio and high technological maturity. However, the hydraulic system's leakage, pipeline vibration, and hydraulic pipeline weight hinder its further ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/44
CPCB64C25/44
Inventor 焦宗夏李冰尚耀星刘晓超
Owner 北京航辰机载智能系统科技有限公司
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