Aircrew headgear ejection means

• US 4,711,411 A
• Filed: 10/24/1986
• Issued: 12/08/1987
• Est. Priority Date: 10/25/1985
• Status: Expired due to Term

• Current Assignee: The secretary of state for defence in her Britannic Majesty's Government of the United Kingdom of Great Britain And Northern Ireland
• Original Assignee: The secretary of state for defence in her Britannic Majesty's Government of the United Kingdom of Great Britain And Northern Ireland
• Inventors: Copp, Warren K.
• Primary Examiner(s): BAREFOOT, GALEN L
• Application Number:
  US06/922,881
• Time in Patent Office: 410 Days
• Field of Search: 244/118.5, 244/122 R, 244/122 A, 244/122 AG, 244/121, 244/122 AE, 244/122 B, 244/1 R, 33/262, 33/252, 33/263, 350/547, 350/549, 350/145, 350/638, 2/6, 2/422, 128/207.11, 128/206.27, 128/206.21
• US Class Current: 244/1.00R
• 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 apparatus for ejecting an aircrewmans helmet-mounted electro-optical equipment from an aircraft cockpit comprising an arm having a first end pivotally mounted at a position behind an aircrewmans ejection seat, a second end of the arm having on it a line reel-in apparatus and a flexible line depending therefrom, the flexible line attachable to helmet mounted electro-optical equipment, a guide and damper connecting the arm to the ejection seat, upon operation of the ejection seat the electro-optical equipment being detached from the helmet, the ejection seat rising in the cockpit and causing rotation of the arm about the pivot point, the line reel-in apparatus locking to prevent the line extending and the electro-optical equipemnt being ejected from the cockpit into the airstream by rotation of the arm prior to the ejection seat leaving the cockpit.

Claims

1. Apparatus for ejection of aircrew helmet-mounted equipment from an aircraft cockpit, comprising an ejector arm engageable with an airman'"'"'s ejection seat and having a first end pivotally mountable behind the seat, and a flexible linkage for attaching the helmet-mounted equipment to the second end of the ejector arm, so that in operation of the ejection seat, the arm is rotated about its pivot by upward movement of the ejection seat so that the equipment is detached from the airman'"'"'s helmet and ejected from the cockpit by the rotating arm.

2. Apparatus according to claim 1 in which the first end of the ejector arm is pivotally mounted at a position in the cockpit offset from the centreline of the ejection seat.

3. Apparatus according to claims 1 or 2 in which the second end of the ejector arm supports an inertia reel-in assembly adapted to receive the line connecting the helmet-mounted equipment when no tension is applied to the line and to lock under conditions of high loading.

4. Apparatus according to claim 3 having an extensible telescopic portion mounted on the second end of the ejector arm in which the telescopic portion carries the inertia reel-in assembly and is extendable on operation of the ejection seat.

5. Apparatus according to claim 1 in which the ejector arm is hinged at a point along its length to facilitate access to the cockpit.

6. Apparatus according to claim 1 in which the pivot axis of the ejector arm is inclined with respect to the pitch and roll axes of the aircraft.

7. Apparatus according to claim 1 and further including guide means and damper means retaining the arm against the ejection seat.

8. Apparatus according to claim 1 in which the second end of the flexible arm and the helmet-mounted equipment are connected by cables adapted for the transmission of electricity.

9. Apparatus according to claim 1 in which the second end of the flexible arm and the helmet-mounted equipment are connected by cables adapted for transmission of light.