IP Library Granted Patent US 7,673,721
Granted Patent B2
US 7,673,721 · App. 11/577,757 · Granted Mar 9, 2010

Electrically actuated aircraft brakes

Assignee: Meggitt Aerospace Limited
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,673,721
App. No.
11/577,757
Granted
Mar 9, 2010
Kind
B2
Abstract

Method and apparatus for monitoring electrically-actuated aircraft brakes includes measuring the break heat pack thickness to determine wear of the brake discs and adjusting the measurement so as to give ongoing compensation for temperature variations and hence expansion of the heat pack.

Claims (10)

1. A method for monitoring an aircraft braking system including measuring the brake heat pack thickness and temperature, adjusting the measured thickness by taking into account the temperature and the coefficient of thermal expansion of the heat pack in order to compensate for temperature variations above ambient temperature in the heat pack that would cause expansion of the brake heat pack, and comparing the adjusted thickness value with a reference value measured at ambient temperature in order to determine the overall disc wear.

2. A method according to claim 1 , including determining an equivalent heat pack thickness at ambient temperature.

3. A method according to claim 1 , including measuring the heat pack thickness from the point at which an actuator ram contacts the closed heat pack and adjusting the measured brake heat pack thickness for any temperature difference above ambient to determine the equivalent heat pack thickness at ambient temperature.

4. A method according to claim 3 , including measuring the actuator ram position or heat pack thickness to compensate for any temperature variation from ambient.

5. A method according to claim 4 , including predicting the remaining service life of a brake heat pack by determining brake wear by adjusting the measured actuator ram position or measured heat stack thickness for any temperature variation from ambient and using the adjusted value to predict the remaining brake life.

6. Apparatus for monitoring an aircraft braking system including means for measuring the brake heat pack thickness, means for measuring the brake heat pack temperature, means for adjusting the measured thickness by taking into account the temperature and the coefficient of thermal expansion of the heat pack in order to compensate for temperature variations above ambient temperature in the heat pack that would cause expansion of the brake heat pack and means for comparing the adjusted thickness value with a reference value measured at ambient temperature in order to determine the overall disc wear.

7. Apparatus according to claim 6 , including means for determining the equivalent heat pack thickness at ambient temperature.

8. Apparatus according to claim 6 , including means for determining the point at which an actuator ram contacts the closed heat pack and measuring heat pack thickness from this position, and means for adjusting the measured brake heat pack thickness for any temperature difference above ambient to determine the equivalent heat pack thickness at ambient temperature.

9. Apparatus according to claim 8 , including means for measuring the actuator ram position or heat pack thickness to compensate for any temperature variation from ambient.

10. Apparatus according to claim 9 , including means for predicting the remaining service life of a heat pack by determining brake wear by adjusting the measured actuator ram position or measured heat pack thickness for any temperature variation from ambient and using the adjusted value to predict the remaining brake life.

Assignments (3)
CORRECTIVE NAME CHANGE. THE NAME CHANGE (PREVIOUSLY RECORDED AT REEL/FRAME 020794/0906 ON APRIL 15, 2008) USED AN INCORRECT EXECUTION DATE OF DECEMBER 9, 1997. THE CORRECT EXECUTION DATE SHOULD BE JANUARY 4, 2008. Recorded Nov 24, 2008
From: DUNLOP AEROSPACE LIMITED
To: MEGGITT AEROSPACE LIMITED
Reel/Frame 021876/0456 →
CHANGE OF NAME Recorded Apr 15, 2008
From: DUNLOP AEROSPACE LIMITED
To: MEGGITT AEROSPACE LIMITED
Reel/Frame 020794/0906 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 24, 2007
From: BAILEY, DAVID ALEXANDER; LUMB, JONATHAN DERIC; WHITTINGHAM, ANDREW
To: DUNLOP AEROSPACE LIMITED
Reel/Frame 019199/0553 →
Priority Claims (1)
GB 0500304.1 · Jan 8, 2005 · national
Continuity (1)
Related Publication 20090084637A1 · Apr 2, 2009