Safety system, a helicopter fitted with such a system, and a safety method seeking to avoid an undesirable event

Patent metadata

Field	Value
Publication number	US-10062293-B2
Application number	US-201615008780-A
Country	US
Kind code	B2
Filing date	Jan 28, 2016
Priority date	Jan 29, 2015
Publication date	Aug 28, 2018
Grant date	Aug 28, 2018

Abstract

A safety system seeking to avoid an undesirable event while piloting a helicopter. According to the invention, the system is remarkable in that it comprises a computer making it possible at any instant t to generate a three-dimensional envelope of fallback paths for the helicopter, the envelope being obtained by calculating, at the instant t , a set of positions that can be reached by the helicopter during a predetermined flight duration, the computer having parameters previously set with data relating to the flight capabilities of the helicopter and including at least one of the following capabilities: maximum speeds and accelerations in all three spatial directions, minimum turning radii for yaw, nose-down, and/or nose-up movements, maximum weight of the transported load, and maximum stresses.

First claim

What is claimed is:

1. A safety system for minimizing the consequences of a helicopter suffering an accident while piloting the helicopter, wherein the safety system comprises:
a computer generating at any instant t a three-dimensional envelope of fallback paths for the helicopter, the three-dimensional envelope being obtained by calculating, at the instant t, a set of positions that can be reached by the helicopter during a predetermined flight duration, the computer having parameters previously set with data relating to the flight capabilities of the helicopter and including at least one of the following flight capabilities of the helicopter: maximum speeds and accelerations in all three spatial directions, higher order derivatives of at least one of the maximum speeds or accelerations in all three spatial directions, minimum turning radii for yaw movements, climbing or descending angles, maximum weight of the transported load, and maximum stresses;
the computer counting the fallback paths and comparing an amount of fallback paths to a first threshold value and to a second threshold value, wherein the second threshold value is less than or equal to the first threshold value;
an emergency member suitable for issuing a warning signal when the amount of the fallback paths is less than the first threshold value; and
a control member suitable, when the amount of the fallback paths is less than the second threshold value, for implementing corrective helicopter piloting actions to minimize the consequences of the helicopter suffering an accident.

2. The safety system according to claim 1 , wherein the fallback paths belong to at least two groups of paths corresponding to two distinct safety levels as pre-set by a pilot before a mission.

3. The safety system according to claim 1 , wherein the computer identifies at least one preferred fallback path from the three-dimensional envelope of fallback paths, and wherein the safety system includes a man-machine interface enabling a pilot to select the preferred fallback path.

4. A helicopter, including a safety system according to claim 1 .

5. A safety method seeking to minimize the consequences of a helicopter suffering an accident while piloting the helicopter, wherein the method comprises at least the steps of:
before a mission of the helicopter, setting parameters of a computer with data relating to the flight capabilities of the helicopter and including at least one of the following flight capabilities of the helicopter: maximum speeds in all three spatial directions, accelerations in all three spatial directions, higher order derivatives of at least one of the maximum speeds or accelerations in all three spatial directions, minimum turning radii for yaw movements, climbing or descending angles, maximum weight of the transported load, and maximum stresses;
calculating and generating, at any instant t, a three-dimensional envelope of fallback paths for the helicopter, the three-dimensional envelope being obtained by calculating, at the instant t, a set of positions that can be reached by the helicopter during a predetermined flight duration;
counting the fallback paths for the helicopter and detecting that an amount of the fallback paths is zero;
determining that an undesirable event is imminent as the amount of the fallback paths is less than a third predetermined threshold value greater than zero;
issuing a warning signal as the amount of the fallback paths is less than a first predetermined threshold value greater than zero; and
in response to the amount of the fallback paths being zero:
inhibiting piloting commands from at least one of a manual piloting member and an automatic piloting member of the helicopter; and
generating and transmitting new helicopter piloting commands, the new helicopter piloting commands serving to perform corrective actions to minimize the consequences of the helicopter suffering an accident.

6. The method according to claim 5 , wherein the fallback paths are generated so that they belong to at least two groups of paths corresponding to two distinct safety levels pre-set by a pilot before a mission.

7. The method according to claim 5 , wherein the method includes the steps of:
identifying at least one preferred fallback path within the three-dimensional envelope of fallback paths; and
using a man-machine interface to give a pilot an option of selecting the preferred fallback path when an undesirable event is detected.

8. The method according to claim 7 , wherein in the absence of the pilot of the helicopter selecting the preferred fallback path, the method includes a step of automatically following the preferred fallback path.

9. The method according to claim 5 , wherein prior to a helicopter mission, the safety method includes a step of supplying a computer with parameters specific to the flight conditions of the helicopter, the parameters being selected from the group consisting of: a weight of the load transported by the helicopter, a position of its center of gravity, and flight endurance of the helicopter.

10. The method according to claim 5 , wherein prior to a helicopter mission, the safety method includes a step of transmitting piloting preferences to a computer for use in the situation in which the undesirable event has been identified, the preferences being selected from the group consisting of: a dynamic stress limit of the helicopter, proximity to terrain in relief, proximity to stationary obstacles, proximity to moving obstacles, a limit on changes of direction in a short period of time, and departure from an initial route.

11. The method according to claim 5 , wherein the safety method includes a step of transmitting data to a computer, which data comes from a sensor suitable for reconstituting a three-dimensional image of the outside environment.

12. The method according to claim 5 , wherein the safety method includes a step of transmitting data to a computer, which data comes from a database stored in a memory, the data consisting of a three-dimensional map of the outside environment.

13. A safety method seeking to minimize the consequences of a helicopter suffering an accident while piloting the helicopter, the method comprising:
before a mission of the helicopter, setting parameters of a computer with data relating to the flight capabilities of the helicopter and including at least one of the following flight capabilities of the helicopter: maximum speeds in all three spatial directions, accelerations in all three spatial directions, higher order derivatives of at least one of the maximum speeds or accelerations in all three spatial directions, minimum turning radii for yaw movements, climbing or descending angles, maximum weight of the transported load, and maximum stresses;
calculating and generating, by the computer, at any instant t, a three-dimensional envelope of fallback paths for the helicopter, the three-dimensional envelope being obtained by calculating, at the instant t, a set of positions that can be reached by the helicopter during a predetermined flight duration from a current position of the helicopter at the instant t;
counting, by the computer, the fallback paths and detecting, by the computer, that an amount of the fallback paths is less than a second threshold value, wherein the second threshold value is less than the first threshold value;
issuing a warning signal, by an emergency member, as the amount of the fallback paths is less than the first threshold value; and
implementing corrective helicopter piloting actions, by a control member, to minimize the consequences of the helicopter suffering an accident as the amount of the fallback path

Assignees

• Airbus Helicopters

Inventors

• Nikolajevic Konstanca
• Belanger Nicolas
• Damiani Nicolas
• Violette Arnaud

Classifications

• G05D1/0061

  for transition from automatic pilot to manual pilot and vice versa · CPC title

• G08G5/003

  Physics · mapped topic

• B64C27/04 Primary

  Helicopters · CPC title

• G08G5/0021

  Physics · mapped topic

• G08G5/0078

  Physics · mapped topic