Granted Patent B2

US 12,208,720 · App. 17/838,676 · Granted Jan 28, 2025

Inventors: John L. Hampton (Colorado Springs, CO); Glen Shaw (Colorado Springs, CO); Tyler Fahey (Woodland Park, CO); Donald Borchelt (Monument, CO); John R. Skola (Rowlett, TX); Robert Mishkin (Colorado Springs, CO)

Assignee: ROCKWELL COLLINS, INC.

B60N2/90B64D25/10B60N2002/981G08B6/00

Abstract

Claims (50)

1. A vibrotactile system for an aircraft, comprising:

a seat cushion;

a seatback cushion;

a plurality of tactors including a plurality of left seat tactors located in the seat cushion, a plurality of right seat tactors located in the seat cushion, a plurality of left seatback tactors located in the seatback cushion, and a plurality of right seatback tactors located in the seatback cushion, the plurality of left seat tactors being located between a midplane of the seat cushion and a left side of the seat cushion, the plurality of right seat tactors being located between the midplane of the seat cushion and a right side of the seat cushion, the plurality of left seatback tactors being located between a midplane of the seatback cushion and a left side of the seatback cushion, and the plurality of right seatback tactors being located between the midplane of the seatback cushion and a right side of the seatback cushion;

a tactor driver operably coupled to the plurality of tactors and configured to send vibrations commands to the plurality of tactors in response to a signal received from an aircraft controller; and

a first tangible, non-transitory memory configured to communicate with the tactor driver, the first tangible, non-transitory memory having instructions stored thereon that, in response to execution by the tactor driver, cause the tactor driver to perform operations comprising:

receiving, by the tactor driver, the signal from the aircraft controller;

determining, by the tactor driver, a vibration sequence for the plurality of tactors based on the signal received from the aircraft controller; and

outputting, by the tactor driver, vibrate commands corresponding to the vibration sequence to at least one of the plurality of left seat tactors, the plurality of right seat tactors, the plurality of left seatback tactors, and the plurality of right seatback tactors;

wherein the vibration sequence and the vibrate commands are configured to cause at least one of the plurality of left seat tactors or the plurality of right seat tactors to vibrate sequentially such that a first tactor of the at least one of the plurality of left seat tactors or the plurality of right seat tactors vibrates first and a second tactor of the at least one of the plurality of left seat tactors or the plurality of right seat tactors vibrates last, the first tactor being located proximate a first end of the seat cushion and the second tactor being located proximate a second end of the seat cushion opposite the first end.

2. The vibrotactile system of claim 1 , wherein the vibration sequence and the vibrate commands are configured to cause each of the plurality of left seat tactors, the plurality of right seat tactors, the plurality of left seatback tactors, and the plurality of right seatback tactors to vibrate simultaneously.

3. The vibrotactile system of claim 1 , further comprising:

the aircraft controller; and

a second tangible, non-transitory memory configured to communicate with the aircraft controller, the second tangible, non-transitory memory having instructions stored thereon that, in response to execution by the aircraft controller, cause the aircraft controller to perform operations comprising:

receiving, by the aircraft controller, flight and aircraft data;

determining, by the aircraft controller, the signal to send to the tactor driver based on the flight and aircraft data; and

outputting, by the aircraft controller, the signal to the tactor driver.

4. The vibrotactile system of claim 3 , wherein the flight and aircraft data is received from at least one of an avionic system, a sensor, or a landing gear system.

5. The vibrotactile system of claim 3 , wherein the flight and aircraft data is received from a seat occupant monitoring system.

6. The vibrotactile system of claim 1 , wherein the tactor driver is configured to receive a direction signal from the aircraft controller and, in response to receiving the direction signal, the tactor driver determines the vibration sequence and outputs the vibrate commands to cause the plurality of tactors to vibrate in a manner configured to draw attention of an occupant of the aircraft to a direction of an alert.

7. The vibrotactile system of claim 1 , wherein:

the plurality of left seat tactors are located closer to the left side of the seat cushion than to the midplane of the seat cushion; and

the plurality of right seat tactors are located closer to the right side of the seat cushion than to the midplane of the seat cushion.

8. The vibrotactile system of claim 1 , wherein:

the plurality of left seatback tactors are located closer to the left side of the seatback cushion than to the midplane of the seatback cushion; and

the plurality of right seatback tactors are located closer to the right side of the seatback cushion than to the midplane of the seatback cushion.

9. A method for operating a vibrotactile system for an aircraft, the method comprising:

receiving, by a tactor driver, a signal from an aircraft controller;

determining, by the tactor driver, a vibration sequence for a plurality of tactors based on the signal received from the aircraft controller; and

outputting, by the tactor driver, vibrate commands corresponding to the vibration sequence to at least one of a plurality of left seat tactors, a plurality of right seat tactors, a plurality of left seatback tactors, and a plurality of right seatback tactors;

wherein the vibration sequence and the vibrate commands are configured to cause at least one of the plurality of left seat tactors or the plurality of right seat tactors to vibrate sequentially such that a first tactor of the at least one of the plurality of left seat tactors or the plurality of right seat tactors vibrates first and a second tactor of the at least one of the plurality of left seat tactors or the plurality of right seat tactors vibrates last, the first tactor being located proximate a first end of a seat cushion and the second tactor being located proximate a second end of the seat cushion opposite the first end;

wherein the plurality of tactors includes the plurality of left seat tactors located in the seat cushion, the plurality of right seat tactors located in the seat cushion, a plurality of left seatback tactors located in a seatback cushion, and a plurality of right seatback tactors located in the seatback cushion, the plurality of left seat tactors being located between a midplane of the seat cushion and a left side of the seat cushion, the plurality of right seat tactors being located between the midplane of the seat cushion and a right side of the seat cushion, the plurality of left seatback tactors being located between a midplane of the seatback cushion and a left side of the seatback cushion, and the plurality of right seatback tactors being located between the midplane of the seatback cushion and a right side of the seatback cushion.

10. The method of claim 9 , further comprising:

receiving, by the aircraft controller, flight and aircraft data;

determining, by the aircraft controller, the signal to send to the tactor driver based on the flight and aircraft data; and

outputting, by the aircraft controller, the signal to the tactor driver.

11. The method of claim 10 , wherein the flight and aircraft data is received from at least one of an avionic system, a sensor, a landing gear system, or a seat occupant monitoring system.

12. The method of claim 11 , wherein the flight and aircraft data is indicative of a location of the aircraft relative to a boundary, and wherein determining, by the aircraft controller, the signal to send to the tactor driver comprises comparing, by the aircraft controller, a distance between the aircraft and the boundary to a threshold distance, and wherein the aircraft controller is configured to send the signal to the tactor driver in response to the distance being less than the threshold distance.

13. The method of claim 12 , wherein the signal sent by the aircraft controller and the vibrate commands sent by the tactor driver are configured to cause the plurality of tactors to vibrate faster as the distance between the aircraft and the boundary decreases.

14. The method of claim 11 , wherein the flight and aircraft data is indicative of a foreign object approaching the aircraft, and wherein the vibration sequence is configured to convey a direction from which the foreign object is approaching the aircraft.

15. An ejection seat, comprising:

a seatback including a seatback cushion;

a seat bucket coupled to the seatback and including a seat cushion;

a plurality of seatback tactors located in the seatback cushion, the plurality of seatback tactors including a plurality of left seatback tactors and a plurality of right seatback tactors, the plurality of left seatback tactors being located between a midplane of the seatback cushion and a left side of the seatback cushion, and the plurality of right seatback tactors being located between the midplane of the seatback cushion and a right side of the seatback cushion;

a plurality of seat tactors located in the seat cushion, the plurality of seat tactors including a plurality of left seat tactors and a plurality of right seat tactors, the plurality of left seat tactors being located between a midplane of the seat cushion and a left side of the seat cushion, the plurality of right seat tactors being located between the midplane of the seat cushion and a right side of the seat cushion; and

a tactor driver operably coupled to the plurality of seatback tactors and the plurality of seat tactors, the tactor driver being configured to send vibrations commands to the plurality of seatback tactors and the plurality of seat tactors, wherein the tactor driver is configured to:

receive a signal from an aircraft controller;

determine a vibration sequence for the plurality of tactors based on the signal received from the aircraft controller; and

output vibrate commands corresponding to the vibration sequence to at least one of the plurality of left seat tactors, the plurality of right seat tactors, the plurality of left seatback tactors, and the plurality of right seatback tactors;

wherein the vibration sequence and the vibrate commands are configured to cause at least one of the plurality of left seat tactors or the plurality of right seat tactors to vibrate sequentially such that a first tactor of the at least one of the plurality of left seat tactors or the plurality of right seat tactors vibrates first and a second tactor of the at least one of the plurality of left seat tactors or the plurality of right seat tactors vibrates last, the first tactor being located proximate a first end of the seat cushion and the second tactor being located proximate a second end of the seat cushion opposite the first end.

Assignments (1)

Continuity (1)

References Cited (13)