Inflating rotorcraft external airbags in stages

• US 9,452,843 B1
• Filed: 05/13/2015
• Issued: 09/27/2016
• Est. Priority Date: 05/13/2015
• Status: Active Grant

• Current Assignee: Bell Helicopter Textron Incorporated (Textron Inc)
• Original Assignee: Bell Helicopter Textron Incorporated (Textron Inc)
• Inventors: Lu, Zi, Seifert, Michael, Tho, Cheng-Ho
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): Lee, Tyler J
• Application Number:
  US14/711,230
• Time in Patent Office: 503 Days
• Field of Search: 701/3, 701/45, 244/100.A
• US Class Current: 1/1
• CPC Class Codes: B64C 2025/325 specially adapted for helicopters
• CPC Class Codes: B64C 25/32 characterised by elements which contact the ground or similar surface arrester hooks B64C25/68
• CPC Class Codes: B64C 25/56 inflatable
• CPC Class Codes: B64D 2201/00 Airbags mounted in aircraft for any use
• CPC Class Codes: B64D 25/00 Emergency apparatus or devices, not otherwise provided for parachutes B64D17/00, B64D19/00; jettisoning of fuel tanks or fuel per se B64D37/00; specially adapted for protection against criminal attack, e.g. anti-hijacking systems B64D45/0015 ; safety belts or body harnesses in general A62B35/00; safety belts or body harnesses for land vehicles B60R22/00; jettisonable parts of fuselage facilitating emergency escape B64C

Abstract

An aircraft airbag inflation system includes an airbag mounted on an external surface of an aircraft. The airbag is configured to inflate in one of multiple stages prior to the aircraft crashing, and each stage is associated with a respective pressure. The system also includes multiple sensors disposed on-board the aircraft and configured to sense aircraft velocities and an aircraft attitude. The system also includes a controller disposed on-board the aircraft and configured to receive multiple signals from the sensors, the multiple signals representing the aircraft velocities and the aircraft attitude sensed by the sensors, determine a crash event for the aircraft based on the received multiple signals, the crash event including an aircraft sink rate, an aircraft attitude at crash time, and an aircraft distance from the impact surface, and determine a stage at which the airbag is to be inflated based on the crash event.

Claims

1. An aircraft airbag inflation system comprising:

a first airbag, a second airbag, and a third airbag each mounted on an external surface of an aircraft, each of the first airbag, the second airbag, and the third airbag configured to inflate in one of a plurality of stages prior to the aircraft crashing, each stage associated with a respective pressure, the plurality of stages comprising a first stage associated with a first pressure, a second stage associated with a second pressure greater than the first pressure, and a third stage associated with a third pressure greater than the second pressure;

a plurality of sensors disposed on-board the aircraft and configured to sense a plurality of aircraft velocities and an aircraft attitude; and

a controller disposed on-board the aircraft and configured to perform operations comprising;

receiving a plurality of signals from the plurality of sensors, the plurality of signals representing the plurality of aircraft velocities and the aircraft attitude sensed by the plurality of sensors,

determining a crash event for the aircraft based on the received plurality of signals, the crash event comprising an aircraft sink rate, an aircraft attitude at crash time, and an aircraft distance from an impact surface, and

determining a stage at which the airbags are to be inflated based on the crash event, comprising determining, based on the determined crash event, that the first airbag is to be inflated to the first stage, the second airbag is to be inflated to the second stage, and the third airbag is to be inflated to the third stage.

2. The system of claim 1, wherein the controller is configured to perform operations comprising:

transmitting a first signal to inflate the first airbag to the first stage, a second signal to inflate the second airbag to the second stage and a third signal to inflate the third airbag to the third stage.

3. The system of claim 1, wherein the controller is configured to inflate each of the first airbag, the second airbag and the third airbag at different times.

4. The system of claim 1, wherein the plurality of aircraft velocities comprise a vertical aircraft velocity, a forward aircraft velocity and a lateral aircraft velocity.

5. The system of claim 1, wherein the aircraft attitude comprises a pitch, a roll and a yaw.

6. The system of claim 1, wherein the crash event further comprises an aircraft body acceleration and an impact surface condition.

7. The system of claim 1, wherein the operations that the controller is configured to perform comprise transmitting a signal representing the determined stage to the airbag, wherein the airbag inflates to a pressure associated with the determined stage prior to the aircraft crashing to prevent aircraft tumbling.

8. The system of claim 1, wherein the airbag comprises a plurality of inflators, each inflator corresponding to a respective stage, each inflator configured to discharge gas to a pressure associated with the respective stage.

9. The system of claim 8, wherein the plurality of stages comprises three stages and the plurality of inflators comprises three inflators, and wherein the controller is configured to:

determine that the stage at which the airbag is to be inflated based on the crash event is the second stage; and

transmit a first signal and a second signal to a first inflator and a second inflator, respectively, wherein the first inflator and the second inflator discharge gas at a respective pressure to inflate the airbag to the second stage.

10. The system of claim 1, wherein determining the crash event for the aircraft based on the received plurality of signals, the crash event comprising the aircraft sink rate, the aircraft attitude at crash time, and the aircraft distance from the impact surface comprises:

storing a plurality of crash event values in a computer-readable storage medium, each crash event value associated with a respective plurality of aircraft velocities and aircraft attitude; and

comparing the plurality of aircraft velocities and the aircraft attitude sensed by the plurality of sensors with the stored plurality of aircraft velocities and aircraft attitude.

11. The system of claim 1, wherein determining the crash event for the aircraft based on the received plurality of signals, the crash event comprising the aircraft sink rate, the aircraft attitude at crash time, and the aircraft distance from the impact surface comprises solving aircraft flight equations that receive the plurality of aircraft velocities and the aircraft attitude as inputs and provide the crash event as outputs.

12. The system of claim 11, wherein the aircraft flight equations are solved in real time.

13. A method comprising:

receiving a plurality of signals from a plurality of sensors disposed on-board an aircraft, the plurality of signals representing a plurality of aircraft velocities and an aircraft attitude sensed by the plurality of sensors;

determining a crash event for the aircraft based on the received plurality of signals, the crash event comprising an aircraft sink rate, an aircraft attitude at crash time, and an aircraft distance from an impact surface;

determining a stage at which a first airbag, a second airbag, and a third airbag mounted on an external surface of an aircraft are to be inflated based on the crash event, each of the first airbag, the second airbag, and the third airbag configured to inflate in one of a plurality of stages prior to the aircraft crashing, each stage associated with a respective pressure, wherein the plurality of stages comprises a first stage associated with a first pressure, a second stage associated with a second pressure greater than the first pressure, and a third stage associated with a third pressure greater than the second pressure;

determining, based on the determined crash event, that the first airbag is to be inflated to the first stage, the second airbag is to be inflated to the second stage, and the third airbag is to be inflated to the third stage; and

transmitting a signal representing the determined stage to the airbags, wherein the airbags inflate to a pressure associated with the transmitted signal, wherein transmitting a signal comprises transmitting a first signal to inflate the first airbag to the first stage, a second signal to inflate the second airbag to the second stage, and a third signal to inflate the third airbag to the third stage.

14. The method of claim 13, wherein the airbags comprise a plurality of inflators, each inflator corresponding to a respective stage, each inflator configured to discharge gas to a pressure associated with the respective stage, wherein the plurality of stages comprises three stages and the plurality of inflators comprises three inflators, and wherein the operations further comprise:

determining that the stage at which the second airbag is to be inflated based on the crash event is the second stage; and

transmitting a first inflator signal and a second inflator signal to a first inflator and a second inflator, respectively, wherein the first inflator and the second inflator discharge gas at a respective pressure to inflate the second airbag to the second stage.

15. The method of claim 13, wherein the plurality of aircraft velocities comprise a vertical aircraft velocity, a forward aircraft velocity and a lateral aircraft velocity.

16. The method of claim 13, wherein the aircraft attitude comprises a pitch, a roll and a yaw.

17. The method of claim 13, wherein the crash event further comprises an aircraft body acceleration and an impact surface condition.

18. A non-transitory computer-readable medium storing instructions executable by data processing apparatus to perform operations comprising:

receiving a plurality of signals from a plurality of sensors disposed on-board an aircraft, the plurality of signals representing a plurality of aircraft velocities and an aircraft attitude sensed by the plurality of sensors;

determining a crash event for the aircraft based on the received plurality of signals, the crash event comprising an aircraft sink rate, an aircraft attitude at crash time, and an aircraft distance from an impact surface;

determining a stage at which a first airbag, a second airbag, and a third airbag mounted on an external surface of an aircraft are to be inflated based on the crash event, each of the first airbag, the second airbag, and the third airbag configured to inflate in one of a plurality of stages prior to the aircraft crashing, each stage associated with a respective pressure, wherein the plurality of stages comprises a first stage associated with a first pressure, a second stage associated with a second pressure greater than the first pressure, and a third stage associated with a third pressure greater than the second pressure;

determining, based on the determined crash event, that the first airbag is to be inflated to the first stage, the second airbag is to be inflated to the second stage, and the third airbag is to be inflated to the third stage; and

transmitting a signal representing the determined stage to the airbags, wherein the airbags inflate to a pressure associated with the transmitted signal, wherein transmitting a signal comprises transmitting a first signal to inflate the first airbag to the first stage, a second signal to inflate the second airbag to the second stage, and a third signal to inflate the third airbag to the third stage.

19. An aircraft airbag inflation system comprising:

an airbag mounted on an external surface of an aircraft, the airbag configured to inflate in one of a plurality of stages prior to the aircraft crashing, each stage associated with a respective pressure;

a plurality of sensors disposed on-board the aircraft and configured to sense a plurality of aircraft velocities and an aircraft attitude; and

a controller disposed on-board the aircraft and configured to perform operations comprising;

receiving a plurality of signals from the plurality of sensors, the plurality of signals representing the plurality of aircraft velocities and the aircraft attitude sensed by the plurality of sensors,

determining a crash event for the aircraft based on the received plurality of signals, the crash event comprising an aircraft sink rate, an aircraft attitude at crash time, and an aircraft distance from an impact surface, wherein determining a crash event comprises;

storing a plurality of crash event values in a computer-readable storage medium, each crash event value associated with a respective plurality of aircraft velocities and aircraft attitude; and

comparing the plurality of aircraft velocities and the aircraft attitude sensed by the plurality of sensors with the stored plurality of aircraft velocities and aircraft attitude; and

determining a stage at which the airbag is to be inflated based on the crash event.

20. A method comprising:

receiving a plurality of signals from a plurality of sensors disposed on-board an aircraft, the plurality of signals representing a plurality of aircraft velocities and an aircraft attitude sensed by the plurality of sensors;

determining a crash event for the aircraft based on the received plurality of signals, the crash event comprising an aircraft sink rate, an aircraft attitude at crash time, and an aircraft distance from an impact surface;

determining a stage at which an airbag mounted on an external surface of an aircraft is to be inflated based on the crash event, the airbag configured to inflate in one of a plurality of stages prior to the aircraft crashing, each stage associated with a respective pressure, wherein the airbag comprises a plurality of inflators, each inflator corresponding to a respective stage, each inflator configured to discharge gas to a pressure associated with the respective stage;

determining that the stage at which the airbag is to be inflated based on the crash event is a second stage of the plurality of stages; and

transmitting a signal representing the determined stage to the airbag, wherein the airbag inflates to a pressure associated with the transmitted signal, the transmitting comprising transmitting a first signal and a second signal to a first inflator and a second inflator, respectively, of the plurality of inflators, wherein the first inflator and the second inflator discharge gas at a respective pressure to inflate the airbag to the second stage.