IP Library Patent Application 12557910
Patent Application
App. No. 12/557,910

ACTIVATION-DEACTIVATION PROCESS ON THE GROUND FOR AN AIRCRAFT TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM

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Quick Facts
Patent No.
US None
App. No.
12/557,910
Abstract

An aircraft is equipped with a traffic alert and collision avoidance system. This system includes an interrogating function to interrogate a transponder on-board another aircraft. The interrogating function is activated when the aircraft is on the ground and is located below a distance threshold in relation to a take-off/landing runway. The interrogating function is deactivated when the aircraft is on the ground and one of the two following conditions is met: (i) there is no take-off/landing runway with respect to which the aircraft is located below a distance threshold greater than the distance threshold first mentioned, and (ii) after a wait time following activation, there is no take-off/landing runway with respect to which the aircraft is located below a distance threshold at least equal to the distance threshold first mentioned.

Claims (32)

1 . A process to control an on-board aircraft traffic alert and collision avoidance system, the traffic alert and collision avoidance system comprises an interrogating function to interrogate a transponder on-board another aircraft, the process comprising:

activation of the interrogating function when the aircraft is on the ground and is located below a distance threshold with respect to a take-off/landing runway;

deactivation of the interrogating function when the aircraft is on the ground and one of the two following conditions is met:

(a) there is no take-off/landing runway with respect to which the aircraft is located below a distance threshold greater than the distance threshold first mentioned, and

(b) after a wait time following activation, there is no take-off/landing runway with respect to which the aircraft is located below a distance threshold at least equal to the distance threshold first mentioned.

2 . A process according to claim 1 , in which geographical data related to the take-off/landing runway is obtained from a database.

3 . A process according to claim 2 , in which the database includes at least one of the following databases: (i) a centralized aircraft database, (ii) an EGWPS (Enhanced Ground Proximity Warning System) or TAWS (Terrain Awareness and Warning System) environment surveillance calculator database, and (iii) an OANS (On-Board Navigation System) airport navigation calculator database.

4 . A process according to claim 1 , in which detection of a displacement phase of an aircraft launches activation of a transponder on-board the aircraft.

5 . A process according to claim 1 , in which detection of an operating phase of at least an aircraft engine engages activation of the a transponder on-board the aircraft.

6 . A process according to claim 1 , in which the detection of a shutdown phase of the engines of the aircraft launches the deactivation of a transponder on-board the aircraft.

7 . An aircraft traffic alert and collision avoidance system, the system comprising:

an interrogating function to interrogate a transponder on-board another aircraft; and

a control module designed to activate the interrogating function when the aircraft is on the ground and is located below the distance threshold with respect to a take-off/landing runway, and to deactivate the interrogating function when one of the two following conditions is met:

(a) there is no take-off/landing runway with respect to which the aircraft is located below a distance threshold greater than the distance threshold first mentioned, and

(b) after a wait time following activation, there is no take-off/landing runway with respect to which the aircraft is located below a distance threshold at least equal to the distance threshold first mentioned.

8 . A system according to claim 7 , the system being designed to function in an override mode in which the interrogation function is activated and deactivated manually.

9 . A system according to claim 7 , the system being designed to obtain geographical data related to the take-off/landing runway from a database.

10 . A system according to claim 9 , in which the database includes at least one of the following databases: (i) a centralized aircraft database, (ii) an EGWPS (Enhanced Ground Proximity Warning System) or TAWS (Terrain Awareness and Warning System) environment surveillance calculator database, and (iii) an OANS (On-Board Navigation System) airport navigation calculator database.

11 . A system according to claim 7 , the system being designed to launch activation of a transponder on-board the aircraft in response to detecting a displacement phase of the aircraft.

12 . A system according to claim 7 , the system being designed to launch activation of a transponder on-board the aircraft in response to detecting an operating phase of at least one aircraft engine.

13 . A system according to claim 7 , the system being designed to launch deactivation of a transponder on-board the aircraft in response to detecting an engine shutdown phase of the aircraft.

14 . An aircraft with a traffic alert and collision avoidance system, the system comprising:

an interrogating function to interrogate a transponder on-board another aircraft; and

a control module designed to activate the interrogating function when the aircraft is on the ground and is located below the distance threshold with respect to a take-off/landing runway, and to deactivate the interrogating function when one of the two following conditions is met:

(a) there is no take-off/landing runway with respect to which the aircraft is located below a distance threshold greater than the distance threshold first mentioned, and

(b) after a wait time following activation, there is no take-off/landing runway with respect to which the aircraft is located below a distance threshold at least equal to the distance threshold first mentioned.

15 . An aircraft with a system according to claim 14 , the system being designed to function in an override mode in which the interrogation function is activated and deactivated manually.

16 . An aircraft with a system according to claim 14 , the system being designed to obtain geographical data related to the take-off/landing runway from a database.

17 . An aircraft with a system according to claim 16 , in which the database includes at least one of the following databases: (i) a centralized aircraft database, (ii) an EGWPS (Enhanced Ground Proximity Warning System) or TAWS (Terrain Awareness and Warning System) environment surveillance calculator database, and (iii) an OANS (On-Board Navigation System) airport navigation calculator database.

18 . An aircraft with a system according to claim 14 , the system being designed to launch activation of a transponder on-board the aircraft in response to detecting a displacement phase of the aircraft.

19 . An aircraft with a system according to claim 14 , the system being designed to launch activation of a transponder on-board the aircraft in response to of detecting an operating phase of at least one aircraft engine.

20 . An aircraft according to claim 14 , the system being designed to launch deactivation of a transponder on-board the aircraft in response to of detecting an engine shutdown phase of the aircraft.

Assignments (2)
MERGER Recorded May 18, 2011
From: AIRBUS FRANCE
To: AIRBUS OPERATIONS SAS
Reel/Frame 026298/0269 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 14, 2010
From: MAILY, CHRISTOPHE
To: AIRBUS OPERATIONS S.A.S.
Reel/Frame 023787/0958 →