Eureka AIR delivers breakthrough ideas for toughest innovation challenges, trusted by R&D personnel around the world.

Redundant driving electric brake of airplane and control method for redundant driving electric brake

A technology for driving controllers and electric brakes, which is applied in the direction of control valves, air release valves, brakes, brake components, etc. It can solve the problems of low reliability, improve life and reliability, and ensure safe braking.

Inactive Publication Date: 2012-10-03
NORTHWESTERN POLYTECHNICAL UNIV
View PDF6 Cites 15 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

None of these electric brakes use redundant technology, and the reliability is not high

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Redundant driving electric brake of airplane and control method for redundant driving electric brake
  • Redundant driving electric brake of airplane and control method for redundant driving electric brake
  • Redundant driving electric brake of airplane and control method for redundant driving electric brake

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0027] Such as figure 1 As shown, the present invention includes a redundant drive controller 1, a brake actuator 2 and a brake wheel 3. The redundant drive controller 1 receives a given brake pressure signal, and through the control method, drives the double-redundancy brushless DC motor 4 in the brake actuator 2 to work, so that the brake pressure applied on the brake wheel 3 follows the brake Pressure given signal. In the present invention, the control power supply, driving power supply, motor windings, motor Hall sensor, pressure sensor, and power drive unit are backed up.

[0028] Among them, the redundant drive controller 1 includes a brake pressure feedback conditioning unit 5, a brake pressure given receiving unit 6, a DSP unit 7, a CPLD unit 11, an isolation circuit unit 12, a power drive unit 13, a current acquisition unit 8, and an overcurrent protection unit. Auxiliary unit 9 and power system unit 13. The brake pressure setting receiving unit 6 converts the brake pr...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a redundant driving electric brake of an airplane and a control method for the redundant driving electric brake. A redundant driving controller part receives a brake pressure given signal and drives a brake actuator to work, so that brake pressure applied to a braked wheel follows the brake pressure given signal. By adopting a redundant technology, easily damaged mechanisms in an airplane brake driving device are subjected to warm backup; under the condition of normal working, the corresponding parts work at half of rated power, so that the service life of the driving device is prolonged, and the reliability of the driving device is improved; when certain redundancy of the driving device fails, a failure can be detected in real time and isolated, so that a fault motor quits a working state, and the driving device runs after being switched to a single-channel mode; and therefore, the reliability of a braking system of an airplane is improved.

Description

Technical field [0001] The invention relates to an electric brake redundant drive device and control method, in particular to an aircraft electric brake redundant drive device and control method. Background technique [0002] The aircraft brake system is a relatively independent functional subsystem on the aircraft. Its role is to carry the aircraft’s static weight, dynamic impact load, and absorb the kinetic energy of the aircraft when it is landing, so as to realize the braking and control of the aircraft’s take-off, landing, taxiing and turning. [0003] At present, the research results of electric brake control system include: the patent "Aircraft Electric Brake Control System Architecture" with publication number CN101117155 and the patent "Reduced Power Mode of Aircraft Full Electric Brake System" with publication number CN101568458 are two technologies researched by Boeing. . The article "Design and Key Technology Research of Aircraft All-electric Brake Driver" published in...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): B60T8/17B60T8/34
Inventor 齐蓉戴志勇郭皓林辉
Owner NORTHWESTERN POLYTECHNICAL UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com