Airplane distress system

• US 20040201499A1
• Filed: 02/05/2004
• Published: 10/14/2004
• Est. Priority Date: 09/20/2001
• Status: Active Grant

• Current Assignee: Norman Understein
• Original Assignee: Norman Understein
• Inventors: Understein, Norman
• Granted Patent: US 6,980,103 B2
• Time in Patent Office: Days
• US Class Current: 340/945
• CPC Class Codes: B64D 45/0059 by communicating emergency situations to ground control or between crew members
• CPC Class Codes: G08B 31/00 Predictive alarm systems characterised by extrapolation or other computation using updated historic data

Abstract

An airline distress system is provided for an airplane. The airplane includes a pilot cockpit and a transponder for transmitting signals to an air traffic controller. The airline distress system includes an auxiliary transponder (10) that transmits auxiliary signals to the air traffic controller. The auxiliary transponder is preferably disposed outside of the pilot cockpit and inaccessible to airplane crew and passengers. In one embodiment, a sensor (16) is operatively coupled with the cockpit door, and a switch (20) communicates with the sensor (16) and the auxiliary transponder (10). The auxiliary transponder (10) is configured to be automatically activated by the switch (20) according to a signal from the sensor that the cockpit door has been opened.

Claims

1. An airline distress system for an airplane including a pilot cockpit and a transponder for transmitting signals to an air traffic controller, the airline distress system comprising an auxiliary transponder that transmits auxiliary signals to the air traffic controller, the auxiliary transponder being disposed outside of the pilot cockpit and inaccessible to airplane crew and passengers.

2. An airline distress system according to claim 1, wherein the auxiliary transponder is configured to emit up to two emergency codes.

3. An airline distress system according to claim 2, wherein the two emergency codes are changeable by authorized personnel only.

4. An airline distress system according to claim 1, wherein the auxiliary transponder is configured such that once activated, the auxiliary transponder cannot be deactivated by the airplane crew or passengers.

5. An airline distress system according to claim 1, wherein the pilot cockpit is secured with a cockpit door, the system further comprising a sensor operatively coupled with the cockpit door and communicating with the auxiliary transponder, wherein the auxiliary transponder is configured to be automatically activated according to a signal from the sensor that the cockpit door has been opened.

6. An airline distress system according to claim 5, further comprising a switch accessible to the pilot coupled with the sensor for activating the sensor.

7. An airline distress system according to claim 6, wherein the switch is configured also to deactivate the sensor.

8. An airline distress system according to claim 1, further comprising a panic button accessible to the pilot and communicating with the auxiliary transponder for activating the auxiliary transponder.

9. An airline distress system according to claim 8, wherein the auxiliary transponder is configured such that once activated, the auxiliary transponder cannot be deactivated by the airplane crew or passengers.

10. A method of operating an airline distress system in an airplane including a pilot cockpit and a transponder for transmitting signals to an air traffic controller, the airline distress system having an auxiliary transponder, the method comprising:

(a) disposing the auxiliary transponder outside of the pilot cockpit and inaccessible to airplane crew and passengers;

(b) activating the auxiliary transponder according to an activate signal; and

(c) transmitting auxiliary signals to the air traffic controller.

11. A method according to claim 10, wherein step (c) is practiced by emitting up to two emergency codes.

12. A method according to claim 11, further comprising configuring the auxiliary transponder such that the two emergency codes are changeable by authorized personnel only.

13. A method according to claim 10, further comprising configuring the auxiliary transponder such that once activated, the auxiliary transponder cannot be deactivated by the airplane crew or passengers.

14. A method according to claim 10, wherein the pilot cockpit is secured with a cockpit door, and wherein step (b) is practiced by automatically activating the auxiliary transponder when the cockpit door is opened.

15. A method according to claim 14, further comprising, prior to automatically activating the auxiliary transponder, arming the cockpit door.

16. A method according to claim 15, further comprising enabling the cockpit door to be selectively disarmed.

17. A method according to claim 10, wherein step (b) is practiced by pressing a panic button accessible to the pilot.

18. A method according to claim 17, further comprising configuring the auxiliary transponder such that once activated, the auxiliary transponder cannot be deactivated by the airplane crew or passengers.

19. An airline distress system for an airplane including a pilot cockpit secured by a cockpit door and a transponder for transmitting signals to an air traffic controller, the airline distress system comprising:

an auxiliary transponder that transmits auxiliary signals to the air traffic controller, the auxiliary transponder being disposed outside of the pilot cockpit and inaccessible to airplane crew and passengers;

a sensor operatively coupled with the cockpit door; and

a switch communicating with the sensor and the auxiliary transponder, wherein the auxiliary transponder is configured to be automatically activated by the switch according to a signal from the sensor that the cockpit door has been opened.

20. An airline distress system according to claim 19, wherein the auxiliary transponder is configured such that once activated, the auxiliary transponder cannot be deactivated by the airplane crew or passengers.