Seat back breakover with dynamically triggered actuator

Patent metadata

Field	Value
Publication number	US-10414501-B2
Application number	US-201715610167-A
Country	US
Kind code	B2
Filing date	May 31, 2017
Priority date	May 31, 2017
Publication date	Sep 17, 2019
Grant date	Sep 17, 2019

Abstract

An aircraft passenger seat having a dynamic breakover assembly includes a seat bottom frame and a seat back pivotally-mounted to the seat bottom frame that allows the angle of the seat back relative to the seat bottom frame to be varied from an upright taxi takeoff and landing (TTOL) position to a reclined position. The seat may include a means for sensing acceleration corresponding to a force indicative of an abnormal event; and a breakover mechanism coupled to the seat bottom frame and the seat back in which the means for sensing acceleration is coupled to the breakover mechanism. The breakover mechanism can prevent movement of the seat back in a forward direction past the TTOL position during normal use, and permit forward movement of at least a portion of the seat back in the forward direction past the TTOL position upon activation by the means for sensing acceleration.

First claim

What is claimed is:

1. An aircraft passenger seat having a dynamic seat back breakover assembly, comprising:
a seat bottom frame;
a seat back pivotally-mounted to the seat bottom frame for permitting an angle of the seat back relative to the seat bottom frame to be varied at least from an upright taxi takeoff and landing (TTOL) position to a reclined position;
an accelerometer for sensing acceleration corresponding to a force indicative of an emergency event; and
a breakover mechanism coupled to the seat bottom frame and the seat back, wherein
the accelerometer is communicatively coupled to an actuator configured to cause actuation of the breakover mechanism in response to a sensed emergency event, and
the breakover mechanism is configured to
i) prevent movement of the seat back in a forward direction past the TTOL position toward a passenger seated in the aircraft passenger seat during use, and
ii) permit forward movement of at least a portion of the seat back in the forward direction past the TTOL position upon activation by the actuator.

2. The aircraft passenger seat of claim 1 , wherein the actuator is a solenoid configured to cause decoupling of the seat back from the seat bottom frame in response to the sensed emergency event.

3. The aircraft passenger seat of claim 1 , wherein the accelerometer is communicatively coupled to the actuator via at least one of a wired or wireless connection.

4. The aircraft passenger seat of claim 1 , wherein the accelerometer is communicatively coupled to actuators for respective breakover mechanisms for a plurality of seats in a grouping of passenger seats such that the accelerometer is configured to cause actuation of the breakover mechanisms for each of the plurality of seats in response to a sensed emergency event.

5. The aircraft passenger seat of claim 1 , wherein the breakover mechanism includes a shaft coupled to the actuator, the shaft having a first end affixed to the seat bottom frame and a second end configured to be inserted into a recess in the seat back such that the shaft inserted into the recess is configured to prevent movement of the seat back in the forward direction past the TTOL position.

6. The aircraft passenger seat of claim 5 , wherein the actuator is configured to cause retraction of the shaft from the recess in the seat back thereby permitting forward movement of the at least a portion of the seat back in the forward direction past the TTOL position in response to a sensed emergency event.

7. The aircraft passenger seat of claim 6 , wherein the breakover mechanism further includes a spring co-axial with the shaft, the spring configured to assist the breakover mechanism in causing the retraction of the shaft from the recess in the seat bottom frame in response to the sensed emergency event by resisting inward motion by the shaft toward the recess.

8. The aircraft passenger seat of claim 7 , wherein the breakover mechanism further includes a ball entrapment element coupled to the shaft, the ball entrapment element having a plurality of channels each configured to house a respective ball of a plurality of balls when the shaft is inserted into the recess in the seat back.

9. The aircraft passenger seat of claim 8 , wherein the breakover mechanism further includes a collar affixed to the seat back, the collar surrounding the ball entrapment element and configured to house the plurality of balls upon actuation of the breakover mechanism in response to the sensed emergency event.

10. The aircraft passenger seat of claim 9 , wherein the retraction of the shaft from the recess in the seatback causes the plurality of balls to fall from each of the plurality of channels of the ball entrapment element into the collar thereby permitting forward movement of the at least a portion of the seat back in the forward direction past the TTOL position.

11. The aircraft passenger seat of claim 7 , wherein the breakover mechanism further includes a gear bushing fixedly attached to the seat back having gear teeth configured to engage complementary gear teeth of a gear ring surrounding the shaft to prevent forward movement of the at least a portion of the seat back in the forward direction past the TTOL position.

12. The aircraft passenger seat of claim 11 , wherein the breakover mechanism further includes a trigger ring surrounding the shaft, the trigger ring configured to rotate in response to actuation by the accelerometer for sensing acceleration in response to the sensed emergency event, thereby permitting forward motion of the at least a portion of the seat back in the forward direction past the TTOL position.

13. The aircraft passenger seat of claim 1 , wherein the breakover mechanism includes a gear latch configured to mesh with a complementary gear feature on the seat back such that the meshing between the gear latch and the complementary gear feature is configured to prevent movement of the seat back in the forward direction past the TTOL position.

14. The aircraft passenger seat of claim 13 , wherein the actuator is configured to cause unmeshing of the gear latch from the complementary gear feature on the seat back thereby permitting forward movement of the at least a portion of the seat back in the forward direction past the TTOL position.

15. The aircraft passenger seat of claim 1 , wherein the breakover mechanism includes a bracket fixedly attached at a first end to the seat back and pivotably attached at a second end to a recline lock mechanism for the aircraft passenger seat via a fastener, wherein attachment of the second end of the bracket to the recline lock mechanism is configured to prevent movement of the seat back in the forward direction past the TTOL position, wherein the bracket includes a pair of members configured to pivotably attach the bracket to the recline lock mechanism, and wherein the actuator is configured to cause opening of the pair of members thereby causing decoupling of the bracket from the fastener and the recline lock mechanism.

16. An aircraft passenger seat having a dynamic seat back breakover assembly, comprising:
a seat bottom frame;
a seat back pivotally-mounted to the seat bottom frame for permitting an angle of the seat back relative to the seat bottom frame to be varied at least from an upright taxi takeoff and landing (TTOL) position to a reclined position;
an inertial release assembly for sensing acceleration corresponding to a force indicative of an emergency event; and
a breakover mechanism coupled to the seat bottom frame and the seat back, wherein
the inertial release assembly is coupled to the breakover mechanism and is configured to rotate in response to a sensed emergency event such that rotation of the inertial release assembly causes decoupling of the seat back from the seat bottom frame, and
the breakover mechanism is configured to
i) prevent movement of the seat back in a forward direction past the TTOL position toward a passenger seated in the aircraft passenger seat during use, and
ii) permit forward movement of at least a portion of the seat back in the forward direction past the TTOL position upon decoupling caused by the inertial release assembly.

17. The aircraft passenger seat of claim 16 , wherein the inertial release assembly includes a first end coupled to the breakover mechanism and a second end having a weighted element configured to cause the rotation of the inertial release assembly in response to the sensed emergency event.

Assignees

• Rockwell Collins Inc

Inventors

• Thompson Jeff
• Pierson Jay
• Barg Brad
• Finlay Travis
• Martz Thomas
• Yue Neng
• Hedrick Dennis
• Penley Randy

Classifications

• B64D11/0619 Primary

  with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash · CPC title

• B64D11/064

  Adjustable inclination or position of seats · CPC title