METHOD OF MONITORING AIRCRAFT BRAKE PERFORMANCE AND APPARATUS FOR PERFORMING SUCH A METHOD

• US 20120154177A1
• Filed: 02/17/2011
• Published: 06/21/2012
• Est. Priority Date: 12/21/2010
• Status: Abandoned Application

• Current Assignee: Airbus Operations Limited (Airbus SE)
• Original Assignee: Airbus Operations Limited (Airbus SE)
• Inventors: WINGATE, John
• Application Number:
  US13/029,333
• Publication Number:
  US 20120154177A1
• Time in Patent Office: Days
• US Class Current: 340/945
• CPC Class Codes: B60T 17/22 Devices for monitoring or checking brake systems; Signal devices
• CPC Class Codes: B60T 8/17 Using electrical or electronic regulation means to control braking detecting or indicating faulty operation B60T8/885
• CPC Class Codes: B60T 8/1703 for aircrafts
• CPC Class Codes: B64C 25/42 Arrangement or adaptation of brakes
• CPC Class Codes: B64D 2045/0085 Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: F01D 5/021 for flow machines or engines with only one axial stage for more than one stage F01D5/06
• CPC Class Codes: F01D 5/022 with concentric rows of axial blades
• CPC Class Codes: F01D 5/025 Fixing blade carrying members on shafts attachment of a member on a shaft in general F16D1/06; for non-positive displacement pumps F04D29/00
• CPC Class Codes: F01D 5/08 Heating, heat-insulating or cooling means specially adapted for radial flow machines or engines F01D5/04
• CPC Class Codes: F02C 3/073 the compressor and turbine stages being concentric
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A brake performance monitoring system operates by an energy differential calculated from brake demand energy and energy absorbed during a braking operation. A significant differential would be reported as a possible problem with the braking system.

Claims

1. A method of monitoring the performance of an aircraft wheel brake comprising the steps of:

providing an aircraft having a wheel brake,

measuring brake performance input variable data during a braking operation,

calculating an energy demand to be absorbed by the brake over at least part of the braking operation using the brake control input variable data,

measuring brake performance output variable data during the braking operation,

calculating an energy absorbed by the brake over at least part of the braking operation using the brake performance output variable data,

determining a brake performance metric from the energy demand and the energy absorbed,

comparing the brake performance metric with a brake performance criterion to detect impaired performance of the brake.

2. A method according to claim 1 in which the brake performance input variable is brake demand.

3. A method according to claim 2 in which the brake performance input variable is brake servo pressure.

4. A method according to claim 3 comprising the step of converting the brake servo pressure to an estimated brake torque demand.

5. A method according to claim 3 in which the estimated brake torque demand is a percent (%) brake torque demand.

6. A method according to claim 4 comprising the steps of:

providing a braked wheel arranged to be braked by the brake,

recording the speed of the braked wheel during the braking operation,

using the braked wheel speed to calculate the energy demand.

7. A method according to claim 6 in which the step of calculating the energy demand comprises the steps of:

multiplying the estimated brake torque demand by the speed of the braked wheel to calculate power demand data,

integrating the power demand data over time to calculate the energy demand.

8. A method according to claim 1 in which the brake performance output variable is brake torque.

9. A method according to claim 8 in which brake torque is measured at the brake.

10. A method according to claim 8 comprising the steps of:

providing a braked wheel arranged to be braked by the brake,

monitoring the speed of the braked wheel during the braking operation,

using the braked wheel speed to calculate the energy absorbed.

11. A method according to claim 10 in which the step of calculating the energy absorbed comprises the steps of:

multiplying the brake torque by the speed of the braked wheel to calculate power absorbed data,

integrating the power absorbed data over time to calculate the energy absorbed.

12. A method according to claim 1, in which the brake performance indicator is a brake energy differential between (i) the energy absorbed and (ii) an expected energy absorbed for a healthy brake, for the given energy demand.

13. A method according to claim 12 in which the brake performance criterion is at least three standard deviations of a normal distribution of brake energy differentials from a relationship between energy demand and energy absorbed for a healthy brake.

14. A method according to claim 1 comprising the step of:

producing an alert if impaired performance of the brake is detected.

15. An aircraft wheel brake monitoring apparatus comprising:

a memory,

a first sensor arranged to measure brake performance input variable data during a braking operation and send the brake performance input variable data to the memory,

a second sensor arranged to measure brake performance output variable data during the braking operation and send the brake performance output variable data to the memory,

a processor arranged to access the memory and configured to;

(i) calculate energy demand to be absorbed by the brake over at least part of a braking operation using the brake control input variable data,

(ii) calculate energy absorbed by the brake over at least part of a braking operation using the brake performance output variable data,

(iii) calculate a brake performance metric from the energy demand and the energy absorbed, and,

(iv) compare the brake performance metric with a brake performance criterion to detect impaired performance of the brake.