Aircraft airbag protection apparatus and method

• US 5,301,902 A
• Filed: 11/09/1992
• Issued: 04/12/1994
• Est. Priority Date: 11/09/1992
• Status: Expired due to Fees

• Current Assignee: Flight Safety Systems Incorporated
• Original Assignee: Kevin W. Kreutzer, Robert C. Kalberer
• Inventors: Kreutzer, Kevin W., Kalberer, Robert C.
• Primary Examiner(s): Mitchell, David M.
• Assistant Examiner(s): Ellis, Christopher P.
• Application Number:
  US07/973,798
• Time in Patent Office: 519 Days
• Field of Search: 280/728 R, 280/729, 280/731, 280/730, 280/730 A, 244/121, 244/118.5, 244/122 AG
• US Class Current: 244/121
• CPC Class Codes: B60R 2021/0093 Aircraft
• CPC Class Codes: B60R 2021/23107 the bag being integrated in a multi-bag system
• CPC Class Codes: B64D 2201/00 Airbags mounted in aircraft for any use
• CPC Class Codes: B64D 25/02 Supports or holding means for living bodies

Abstract

Airbags are positioned relative to an aircraft yoke so as to minimize undesired force application to that yoke upon actuation thereof. The airbag actuation is accomplished by sensors which are capable of responding to multiple traumatic forces upon the aircraft to either establish multiple actuations of a common airbag, or actuation of separate airbags, upon occurrence of each event. The airbags can assume a side lobe configuration so as to minimize the possibility of impact upon side posts, or the interior side of the aircraft cabin structure. The sensors are arranged in an array with common directional alignment for maximizing probability of appropriate actuation. Use of multiple sensors and majority voting circuitry enhances the reliability of the systems and process.

Claims

1. Apparatus for minimizing the prospect for loss of control in a craft which has a movable control yoke that is grippable by an individual for multiple degrees of motion thereof from a relatively neutral position for controlling the craft operation by the degree of yoke motion, comprising:

means for sensing that the craft has experienced an abnormal force,

an airbag assembly including an inflatable airbag mounted relative to the control yoke and means for responding to an actuation signal by expanding said airbag in a first direction so as to substantially fill the space both between the control yoke and an individual in proximity to the control yoke as well as expanding in a second direction so as to substantially fill the space between the control yoke and the frame of the craft thereby retaining the control yoke in the relatively neutral position, and

means responsive to said sensing means for producing said airbag actuation signal for rapidly expanding said airbag in said first and second directions upon the occurrence of an abnormal force relative to the craft.

2. Apparatus in accordance with claim 1 wherein said sensing means includes a plurality of G-force sensors at least one of which is aligned with the normal direction of movement of the craft.

3. Apparatus in accordance with claim 2 wherein said sensing means includes at least one string of G-force sensors arrayed in common alignment, and

said sensing means further including means for determining that a majority of said commonly aligned G-force sensors are producing signals indicative of the abnormal level of G-force present before producing a said actuation signal for said airbag.

4. Apparatus in accordance with claim 1 including a plurality of said means for inflating said airbag, said means responsive to said sensing means including means for producing a multiplicity of said actuation signals for sequential application to said plurality of inflating means.

5. Apparatus in accordance with claim 1 wherein said airbag assembly includes a plurality of airbags each of which has an inflation means therefor, said means responsive to said sensing means including means for producing said actuation signals for sequential application to said airbag inflation means.

6. The method of minimizing injuries to an occupant of an aircraft which has a manually operable and movable yoke that is positioned between a front panel and the seat of the occupant for manual control of the aircraft as the aircraft moves in a given direction, the yoke being manually movable away from a relatively neutral position to achieve manual control of the aircraft, the method comprising the steps of:

detecting that an excessive G-force was applied to the aircraft generally in the given direction of movement thereof,

responding to said detecting step by filling the space between the occupant and the front panel with a force absorber to thereby protect the occupant, and

arranging said force absorber so that the manually operable yoke is retained in the relatively neutral position subsequent to said responding step to thereby neutralize control of the aircraft.

7. The method in accordance with claim 6 wherein said detecting step includes the step of detecting the excessive G-force at a plurality of locations, and

determining that a majority of said G-force detections at said locations has concurrently occurred before actuating said responding step.

8. The method in accordance with claim 6 wherein said arranging step includes the step of inflating an airbag from said yoke towards the occupant and towards the front panel concurrently.

9. The method in accordance with claim 8 wherein said arranging step includes positioning a portion of said airbag which moves toward the occupant so as to intervene between the occupant and at least portion of the aircraft interior which is offset with respect to the occupant and the direction of movement of the aircraft.