Methods for predicting a speed brake system fault

• US 9,449,438 B2
• Filed: 11/10/2014
• Issued: 09/20/2016
• Est. Priority Date: 04/16/2013
• Status: Active Grant

• Current Assignee: GE Aviation Systems Limited (GE Aerospace)
• Original Assignee: GE Aviation Systems Limited (GE Aerospace)
• Inventors: Catt, Christopher Joseph, Howard, Julia Ann
• Primary Examiner(s): Beaulieu, Yonel
• Application Number:
  US14/536,898
• Publication Number:
  US 20150066288A1
• Time in Patent Office: 680 Days
• Field of Search: 701/3, 701/9, 701/14, 244/75.1, 340/945, 340/963
• US Class Current: 1/1
• CPC Class Codes: B64C 19/00 Aircraft control not otherwise provided for
• CPC Class Codes: B64C 9/323 associated with wings
• CPC Class Codes: B64D 45/0005 Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
• CPC Class Codes: B64F 5/60 Testing or inspecting aircraft components or systems
• CPC Class Codes: G01M 17/00 Testing of vehicles testing fluid tightness G01M3/00; testing elastic properties of bodies or chassis, e.g. torsion-testing, G01M5/00; testing alignment of vehicle headlight devices G01M11/06; testing of engines G01M15/00
• CPC Class Codes: G07C 5/0816 Indicating performance data, e.g. occurrence of a malfunction

Abstract

Methods of predicting a speed brake fault in an aircraft having a speed brake system including multiple control surfaces, a handle for setting the position of the multiple control surfaces, and at least one control surface position sensor, the methods include receiving a position signal from the at least one position sensor, determining a variation in the position signal and predicting a fault in the speed brake system.

Claims

1. A method of predicting a speed brake fault in an aircraft having a speed brake system including multiple control surfaces, the method comprising:

determining a position of at least one of the multiple control surfaces;

comparing the determined position to a reference position value to define a position comparison;

determining from the position comparison a variation parameter indicative of the variation of the determined position from the reference position value;

comparing the variation parameter to a variation reference value to define a variation comparison;

predicting a fault in the speed brake system based on the variation comparison; and

providing an indication of the predicted fault.

2. The method of claim 1 wherein the determining a portion of at least one of the multiple control surfaces comprises receiving a position signal, from at least one position sensor, indicative of the position of the at least one of the multiple control surfaces.

3. The method of claim 1 wherein the determining the position comprises determining positions of a plurality of the multiple control surfaces.

4. The method of claim 3 wherein the determining comprises receiving a plurality of position signals, with each position signal corresponding to a different one of the plurality of the multiple control surfaces.

5. The method of claim 1 wherein the reference position value comprises a predetermined position value of the at least one of the multiple control surfaces.

6. The method of claim 1 wherein the reference position value is based on historical information corresponding to positions of the at least one of the multiple control surfaces.

7. The method of claim 1, further comprising defining variation comparisons over a number of flights of the aircraft to define multiple variation comparisons.

8. The method of claim 7 wherein the predicting the fault is based on the multiple variation comparisons.

9. The method of claim 8 wherein the fault is predicted when the variation comparison indicates the variation parameter exceeds the variation reference value a predetermined number of times over a predetermined number of flights.

10. The method of claim 1 wherein providing the indication comprises providing the indication on a PFD in a cockpit of the aircraft.

11. The method of claim 1 wherein the control surfaces comprise spoilers.

12. A method of predicting a speed brake fault in an aircraft having a speed brake system including multiple control surfaces and a handle, which controls a position of the multiple control surfaces, the method comprising:

determining a position of at least one of the multiple control surfaces;

determining a position of the handle;

defining a reference position value for the at least one of the multiple control surfaces based on the determined position of the handle;

comparing the determined position of the at least one of the multiple control surfaces to the defined reference position value;

predicting a fault in the speed brake system based on the comparison; and

providing an indication of the predicted fault.

13. A method of predicting a speed brake fault in an aircraft having a speed brake system including multiple control surfaces, a handle for setting the position of the multiple control surfaces, and at least one control surface position sensor, the method comprising:

receiving a position signal from the at least one control surface position sensor;

determining from the position signal a time for at least one of the multiple control surfaces to move to a reference position

comparing the determined time to a reference value;

predicting a fault in the speed brake system based on the comparing; and

providing an indication of the predicted fault.

14. The method of claim 13 wherein the reference value is a historical time value.

15. The method of claim 13, further comprising repeating the receiving, determining, and comparing over a number of flights of the aircraft to define multiple comparisons.

16. The method of claim 15 wherein the fault is predicted when the multiple comparisons indicate the determined time exceeds the reference value a predetermined number of times over a predetermined number of flights.