Aircraft trim safety system and backup controls

• US 20080237402A1
• Filed: 01/28/2008
• Published: 10/02/2008
• Est. Priority Date: 12/19/2005
• Status: Abandoned Application

• Current Assignee: Astronics Advanced Electronic Systems Corporation (Astronics Corporation)
• Original Assignee: Astronics Advanced Electronic Systems Corporation (Astronics Corporation)
• Inventors: DeVries, Kevin, Dostal, Jake, Ausman, Marc
• Application Number:
  US12/021,022
• Publication Number:
  US 20080237402A1
• Time in Patent Office: Days
• US Class Current: 244/229
• CPC Class Codes: G01D 2207/10 Displays which are primarily used in aircraft or display aircraft-specific information
• CPC Class Codes: G01D 7/00 Indicating measured values
• CPC Class Codes: G05D 1/0077 using redundant signals or controls

Abstract

Methods and apparatuses that control trim of an aircraft even in the presence of conflicting trim inputs, for example by disabling the trim input switches on the aircraft when conflicting switch inputs are received. When conflicting switch inputs are received and certain time conditions are met, the controller can disable the switch inputs and provide a backup and independent means to control the trim circuitry. The pilot can be allowed to re-enable the disabled inputs.

Claims

1. ) A method of controlling trim surfaces in an aircraft, responsive to a first operator input specifying a first direction for trim adjustment, and a second operator input specifying a second direction for trim adjustment, comprising:

a) Determining if the first input is active and the second input is inactive, and then adjusting the trim according to the first direction;

b) Determining if the first input is inactive and the second input is active, and then adjusting the trim according to the second direction;

c) Determining if the first input is active and the second input is active, and then not adjusting the trim in either the first or the second direction.

2. ) A method as in claim 1, further comprising determining if the first input and the second input are both active for a predetermined time, and if so, then not adjusting the trim regardless of the activation of the first input or the second input.

3. ) A method as in claim 2, further comprising accepting a reset input, and after activation of the reset input adjusting the trim responsive to the first and second inputs.

4. ) A method as in claim 2, further comprising accepting a backup first input and a backup second input, and adjusting the trim responsive to the backup first input and the backup second input.

5. ) A method as in claim 4, wherein, when it has been determined that the first input and the second input are both active for a predetermined time, then presenting to the user controls corresponding to the backup first input and the backup second input.

6. ) A method of controlling trim surfaces in an aircraft, responsive to a trim input from a pilot, and a trim input from a co-pilot, comprising adjusting the trim such that, in the event that the pilot trim input conflicts with the co-pilot trim input, the trim is either adjusted according to the pilot trim input or the trim is not adjusted while such conflict exists.

7. ) A method as in claim 6, wherein adjusting the trim comprises, if the pilot trim input conflicts with the co-pilot trim input, adjusting the trim according to the pilot trim input.

8. ) A method as in claim 6, wherein adjusting the trim comprises, if the pilot trim input conflicts with the co-pilot trim input, not adjusting the trim while such conflict exists.

9. ) A method as in claim 8, wherein, if the pilot trim input conflicts with the co-pilot trim input continuously for a predetermined period of time, then not adjusting the trim regardless of the pilot trim input and the co-pilot trim input.

10. ) A method as in claim 9, further comprising accepting a backup trim input, and adjusting the trim responsive to the backup trim input.

11. ) A method as in claim 8, further comprising accepting a reset input, and after activation of the reset input adjusting the trim responsive to the pilot and co-pilot trim inputs.

12. ) A method as in claim 6, further comprising accepting a pilot override input, and, responsive to such input, controlling the trim responsive to the pilot trim input regardless of the co-pilot trim input.

13. ) A method as in claim 10, further comprising providing a soft key for use as the backup trim input.

14. ) An apparatus to facilitate control of trim surfaces in an aircraft, comprising a control system, adapted to be placed in operable relationship with a trim surface of the aircraft, and adapted to be placed in communication with a pilot trim input subsystem, wherein the pilot trim input subsystem is capable of indicating either of two trim adjustment directions, wherein the control system is adapted to cause adjustment of the trim surface in the direction indicated by the pilot trim input subsystem if only one of the two trim adjustment directions is indicated, and to cause no adjustment of the trim surface if both of the two trim adjustment directions are indicated.

15. ) An apparatus as in claim 14, wherein the control system is further adapted to determine if both of the two trim adjustment directions are indicated, and if so, then to refrain from causing adjustment of the trim surface responsive to the pilot trim input system.

16. ) An apparatus as in claim 14, wherein the control system is further adapted to present a backup trim input to an operator, and to cause adjustment of the trim surface responsive to the backup trim input.

17. ) An apparatus as in claim 14, wherein the control system is further adapted to be placed in communication with a co-pilot trim input system, wherein the co-pilot trim input subsystem is capable of indicating either of two trim adjustment directions, and to cause adjustment of the trim surface according the co-pilot trim input system if the pilot trim input system does not indicate a conflicting trim adjustment direction.

18. ) An apparatus as in claim 17, wherein the control system is adapted to cause adjustment of the trim surface according the pilot trim input system if the pilot trim input system indicates a conflicting trim adjustment direction from that indicated by the co-pilot trim input system.

19. ) An apparatus as in claim 17, wherein the control system is adapted to cause no adjustment to the trim surface if the pilot trim input system indicates a conflicting trim adjustment direction from that indicated by the co-pilot trim input system.

20. ) An apparatus as in claim 19, wherein the control system is adapted to present a backup trim control input to an operator after detecting that the pilot trim input system and the co-pilot trim input system have indicated conflicting trim adjustment directions, and to cause adjustment of the trim control surface responsive to the backup trim control input.

21. ) An apparatus as in claim 17, wherein the control system is adapted to accept an input indicating that the co-pilot trim input system is to be disabled, and, after that input is received, then adjusting the trim responsive to the pilot trim input system without regard to the co-pilot trim input system.