Method and device for inhibiting the operation of an electronic device during take-off and landing of an aircraft

• US 5,815,407 A
• Filed: 12/14/1995
• Issued: 09/29/1998
• Est. Priority Date: 12/14/1995
• Status: Expired due to Term

• Current Assignee: Google Technology Holdings LLC (Alphabet Inc.)
• Original Assignee: Motorola, Inc. (Motorola Solutions, Inc.)
• Inventors: Van Myers, Jeffrey, Huffman, James R., Jambhekar, Shrirang Nikanth, Cruickshank, Ronald D., Collins, Russell L.
• Primary Examiner(s): Voeltz, Emanuel T.
• Assistant Examiner(s): DAM, TUAN QUANG
• Application Number:
  US08/572,603
• Time in Patent Office: 1,020 Days
• Field of Search: 364/427-428, 364/424.06, 364/566, 364/492, 395/182.12, 395/182.13, 395/182.2, 395/182.22, 395/750.01, 395/750.05, 395/750.02, 395/750.08, 340/500, 340/588, 340/571, 340/635-636, 340/945, 340/959, 340/960, 340/963, 340/971, 340/973, 340/975, 340/978, 244/76 R, 244/183, 244/191, 701/5, 701/14, 701/15, 701/16, 701/9
• US Class Current: 702/57
• CPC Class Codes: B64C 27/006 Safety devices

Abstract

An apparatus (700) for inhibiting operation of an electronic device (702) during take-off and landing of an aircraft (802) has a sensor (704) that measures a lateral acceleration. A control circuit (706) is coupled to the sensor (704) and has an output (708) coupled to the electronic device (702).

Claims

1. A method for inhibiting operation of an electronic device which performs non-aircraft function during take-off and landing of an aircraft, comprising the steps of:

(a) sensing a parameter indicative of at least one of take-off and landing;

(b) determining if the parameter indicative of at least one of take-off and landing exceeds a predetermined threshold; and

(c) when the parameter indicative of at least one of take-off and landing exceeds the predetermined threshold for a predetermined period of time, inhibiting operation of the electronic device which performs non-aircraft function.

2. The method of claim 1, wherein step (b) further including the steps of:

(b1) when the lateral acceleration does not exceed the predetermined threshold returning to step (a); and

(b2) when the lateral acceleration does not exceed the predetermined threshold for the predetermined period of time, returning to step (a).

3. The method of claim 2, further including the steps of:

(d) determining if the lateral acceleration is below a second predetermined threshold; and

(e) when the lateral acceleration is below the second predetermined threshold for a second predetermined period of time, not inhibiting operation of the electronic device.

4. The method of claim 1, wherein the step of inhibiting operation of the electronic device includes the steps of:

(c1) setting an inhibit operation flag; and

(c2) starting a shut down procedure.

5. The method of claim 4, further including the steps of:

(c3) when a start-up request is received, determining if the inhibit operation flag is set; and

(c4) when the inhibit operation flag is set, denying the start-up request.

6. The method of claim 1, where the step of inhibiting operation of the electronic device includes the steps of:

(c1) activating an inhibit operation signal; and

(c2) opening a power switch.

7. The method of claim 1, wherein step (c) is replaced with the following steps:

(c) determining if a second event has occurred; and

(d) when the second event has occurred and the lateral acceleration exceeds the predetermined threshold for the predetermined period of time, inhibiting operation of the electronic device.

8. The method of claim 7, wherein step (c) further includes the step of determining if a vibration characteristic is present.

9. The method of claim 7, wherein step (c) further includes the step of determining if an absolute rate of ascent is present.

10. The method of claim 1, wherein the parameter indicative of at least one of take-off and landing is lateral acceleration.

11. An apparatus for inhibiting operation of an electronic device which performs non-aircraft function during take-off and landing of an aircraft, comprising:

a first sensor operative to measure a at least one of take-off and landing parameters; and

a control circuit coupled to the first sensor and having an output coupled to the electronic device which performs non-aircraft function.

12. The apparatus of claim 11, further including a second sensor having an output, wherein the output of the second sensor and the output of the control circuit are inputs to an AND circuit.

13. The apparatus of claim 12, wherein the second sensor measures an absolute rate of ascent.

14. The apparatus of claim 12, wherein the second sensor is a vibration sensor.

15. The apparatus of claim 11, wherein the control circuit includes a comparator having an output of the first sensor as a first input and a predetermined threshold as a second input.

16. The apparatus of claim 11, wherein the control circuit includes a microprocessor.

17. The apparatus of claim 11, further including a controllable switch coupled the output of the control circuit.

18. The apparatus of claim 17, wherein the controllable switch is connected across a power line.

19. The apparatus of claim 11, wherein the electronic device includes a microprocessor and the output of the control circuit is connected to the microprocessor.

20. The apparatus of claim 11, wherein at least one of take-off and landing parameter is lateral acceleration.

21. A computer-readable storage medium having computer-readable data that when inserted into and executed by a computer device, performs the following steps:

(a) receiving a lateral acceleration from a sensor in the computer device;

(b) determining if the lateral acceleration exceeds a threshold; and

(c) when the lateral acceleration exceeds the threshold for a period of time, inhibiting an operation of the computer device which performs non-aircraft function.

22. The computer-readable storage medium of claim 21, wherein step (b) further includes the steps of:

(b1) when the lateral acceleration does not exceed the predetermined threshold returning to step (a); and

(b2) when the lateral acceleration does not exceed the predetermined threshold for the predetermined period of time, returning to step (a).

23. The computer-readable storage medium of claim 22, further including the steps of:

(d) determining if the lateral acceleration is below a second predetermined threshold; and

(e) when the lateral acceleration is below the second predetermined threshold for a second predetermined period of time, not inhibiting operation of the electronic device.

24. A method for inhibiting operation of a carry-on electronic device during take-off and landing of an aircraft, comprising the steps of:

(a) sensing a lateral acceleration using the carry-on electronic device;

(b) determining if the lateral acceleration exceeds a predetermined threshold; and

(c) when the lateral acceleration exceeds the predetermined threshold for a period of time, inhibiting operation of the carry-on electronic device.

25. The method of claim 24, wherein the carry-on electronic device is a radio.

26. The method of claim 24, wherein the carry-on electronic device is a tape player.

27. The method of claim 24, wherein the carry-on electronic device is an electronic book.

28. An apparatus for inhibiting operation of a carry-on electronic device which performs non-aircraft function during take-off and landing of an aircraft, comprising:

a first sensor operative to measure a lateral acceleration; and

a control circuit coupled to the first sensor and having an output coupled to the carry-on electronic device.

29. The apparatus of claim 28, wherein the carry-on electronic device is a radio.

30. The apparatus of claim 28, wherein the carry-on electronic device is a tape player.

31. The apparatus of claim 28, wherein the carry-on electronic device is an electronic book.