Position and restraint system for aircrewman

• US 4,437,628 A
• Filed: 06/29/1979
• Issued: 03/20/1984
• Est. Priority Date: 06/29/1979
• Status: Expired due to Term

• Current Assignee: the united states of america as represented by the secretary of the navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Schwartz, Marcus
• Primary Examiner(s): Blix, Trygve M.
• Assistant Examiner(s): Corl, Rodney
• Application Number:
  US06/053,465
• Time in Patent Office: 1,726 Days
• Field of Search: 244/122 R, 244/122 A, 244/122 B, 244/122 AB, 244/122 AC, 244/122 AD, 244/122 AE, 244/122 AF, 244/122 AG, 244/122 AH, 244/141, 280/729, 280/733, 280/743, 280/753, 297/465, 297/466, 297/216, 2/2, 2/DIG. 3, 9/341, 9/342
• US Class Current: 244/122.0AG
• CPC Class Codes: B64D 25/02 Supports or holding means for living bodies
• CPC Class Codes: B64D 25/06 Harnessing

Abstract

An aircraft ejection seat position and restraint system for protecting an rcrewman against back injuries during emergency escape. The ejection sequence is initiated by the aircrewman pulling a lower ejection handle or a face curtain handle with both hands to release or shatter the cockpit canopy. A torso harness suit is concommittantly tightened with inflation of a vest worn between the aircrewman and the suit, and catapult rockets are fired to propel the seat out of the cockpit. The harness suit draws the aircrewman'"'"'s upper torso against the back of the seat while the inflated vest pushes his hips back and down into the seat pan for optimally positioning his spine before ejection thereby negating the effects of an aircrewman purposely or inadvertently flying with a loose harness. After ejection, the seat is separated from the aircrewman but the vest remains inflated inside the harness providing cushioning against the opening shock force of the parachute which is attached to the harness suit. The inflatable vest is formed as a separate, one-piece garment which may be removed between flights.

Claims

1. A system for positioning and restraining an aircrewman in an aircraft ejection seat catapulted by a thrust motor comprising, in combination:

a torso harness suit including lap belt means formed to be releasably connected at one end to the seat, and shoulder strap means;

retracting means formed to be secured to the seat including restraint strap means releasably connected at the outer ends to said shoulder strap means;

inflatable vest means formed to be worn by the aircrewman and positioned beneath the front and shoulder portions of said suit adjacent to said lap belt means and said shoulder strap means for forcing upper and lower torso of the aircrewman against the back of the seat; and

control means operable by the aircrewman for emergency escape including first actuator means connected to said retracting means for concomittantly retracting said restraint strap means and inflating said vest means, and second actuator means formed to be connected to the thrust motor for initiating ejection a predetermine time after operation of said first actuating means;

whereby the aircrewman'"'"'s spinal column is positioned as near as possible along the direction of seat ejection.

2. A system according to claim 1 wherein:

said retracting means includes an inertia reel for permitting free fore and aft movement under normal flight and for retracting said restraint strap means in response to said control means.

3. A system according to claim 2 wherein:

said vest means includes an inflatable bib and shoulder portions coextensive with the front and shoulders of said suit, and gas generating means initiated by said first actuator for producing gas pressure within said portions.