Method and a device for detecting lack of reaction from the crew of an aircraft to an alarm related to a path

• US 8,493,239 B2
• Filed: 12/16/2010
• Issued: 07/23/2013
• Est. Priority Date: 12/23/2009
• Status: Active Grant

• Current Assignee: Airbus, Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Original Assignee: Airbus, Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Inventors: Christophe, Laure, Merle, Jean-Michel, Pellerin, Philippe, Dehais, Frdric
• Primary Examiner(s): Bugg, George
• Assistant Examiner(s): Labbees, Edny
• Application Number:
  US12/970,229
• Publication Number:
  US 20110148665A1
• Time in Patent Office: 950 Days
• Field of Search: 340/500, 340/506, 340/945, 340/963, 340/995.1, 340/995.14, 340/575, 340/576, 340/995.11, 701/301, 701/302, 701 7- 11, 244/118.5, 244/75.1
• US Class Current: 340/963
• CPC Class Codes: G08B 29/02 Monitoring continuously signalling or alarm systems
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91
• CPC Class Codes: G08G 5/0086 for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935
• CPC Class Codes: G08G 5/045 Navigation or guidance aids, e.g. determination of anti-collision manoeuvers radar or analogous systems specially adapted for anti-collision between aircraft G01S13/933

Abstract

A method and a device are provided for detecting lack of reaction of the crew of an aircraft to an alarm related to a path. The method includes monitoring the emitting condition of a plurality of alarms related to dangers in the path of the aircraft and monitoring a reaction of a crew during first and second time intervals determined based on how long the crew should take to response to the initial alarm in the first time interval and an auxiliary alarm in the second time interval. The method also includes implementing automatic avoidance operation for coping with the danger if the crew has not reacted to the alarms by the end of the second time interval.

Claims

1. A device for detecting lack of reaction of a crew of an aircraft to an alarm regarding the danger related to a path of the aircraft, the device comprising:

an alarm monitoring device for automatically monitoring the emitting condition of a plurality of alarms regarding dangers related to the path of the aircraft;

a first internal determining device for automatically determining, in case one of the alarms is emitted, a first time interval, for the crew to react to the alarm emitted by implementing at least one procedure to cope with the danger causing the emitted alarm;

a crew monitoring device for automatically monitoring the reaction of the crew without implementing an automatic avoidance operation during the first time interval;

an instruction generation device and a signalling device automatically emitting an auxiliary alert signal, if at the end of the first time interval from the emitted alarm, the crew has not reacted to the emitted alarm;

a second internal determining device for automatically determining a second time interval, for the crew to react to the alarm by implementing a procedure for coping with the danger, the second time interval being determined only if at the end of the first time interval, the crew has not reacted to the alarm; and

an avoidance path generation device and an auto pilot device for automatically implementing, if at the end of the second time interval the crew has not yet reacted to the alarm, an automatic avoidance operation along an avoidance path for coping with the danger, the avoidance operation being implemented only if such an avoidance path can be calculated.

2. The device according to claim 1, further comprising:

an alarm device configured to emit in the aircraft alarms regarding dangers related to the path of the aircraft.

3. A method for detecting lack of reaction of a crew of an aircraft to an alarm regarding a danger related to a path of the aircraft, the method comprising the following steps carried out automatically:

(a) monitoring the emitting condition of a plurality of alarms regarding the dangers related to the path of the aircraft;

(b) in case one of the alarms is emitted, determining a first time interval for the crew to react to the emitted alarm by implementing at least one procedure for coping with the danger this alarm originates from;

(c) monitoring the reaction of the crew during the first time interval without implementing an automatic avoidance operation during the first time interval; and

(d) only if at the end of the first time interval from the emission, the crew has not reacted to the alarm, performing the following operations;

(d1) emitting at least one auxiliary alert signal;

(d2) determining a second time interval for the crew to react to the emitted alarm by implementing a procedure for avoiding the danger the emitted alarm originates from; and

(d3) if at the end of the second time interval the crew has not yet reacted to the emitted alarm, implementing an automatic avoidance operation along an avoidance path for coping with the danger, the avoidance operation being implemented only if such avoidance path can be calculated.

4. The method according to claim 3, wherein in step (b), the first time interval is determined using information regarding the current state vector of the aircraft and the distance from the current position of the aircraft to the position of the event the alarm originates from.

5. The method according to claim 3, wherein in step (c), the actions performed by the crew are monitored on interface devices of the aircraft.

6. The method according to claim 3, wherein the aircraft includes a plurality of parameter viewing screens selectively used by the pilot and wherein step (d1) further includes:

determining the parameter viewing screen where the attention of the pilot of the aircraft is currently focused; and

emitting the auxiliary alert signal at least on the parameter viewing screen thus determined.

7. The method according to claim 3, wherein in step (d1), if additional alarms are emitted simultaneously with the emitted alarm regarding a danger related to a path of the aircraft, the strength of the emitted alarm regarding a danger related to a path of the aircraft is increased with respect to the additional alarms.

8. The method according to claim 3, wherein in step (d1), several different auxiliary alert signals are emitted simultaneously.

9. The method according to claim 3, further comprising:

assessing the current position of the aircraft;

determining the relief in the vicinity of the current position; and

showing the relief in a flight director horizon of a parameter viewing screen for viewing the primary flight parameters.

10. The method according to claim 9, wherein the relief is shown in three dimensions in the flight director horizon which is in two dimensions.