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Document Number
US Patent 5415366
Issued Date
May 16, 1995
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Abstract
An arm restraint system for an ejection seat of an aircraft. The arm restraint system includes a pair of shrouds that are attached to the seat and each contain an outer channel. Extending through each outer channel is a corresponding strap that is coupled to the cockpit and fastened to a ring on the belt of the pilot. When the seat is ejected, the straps are pulled and the shrouds are deployed onto the arms of the pilot. The shrouds extend to a position which captures the wrists of the pilot, thereby preventing both sideward and upward movement of the arms.
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Arm restraint - US Patent 5415366 Drawing
Drawing from US Patent 5415366
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Number of Claims:
14
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Owner
Published
May 16, 1995
Application Number
08/204,860
Filed
February 28, 1994
US Classification
244/122AG  
Int'l Classification
B64D   25/02   (20060101)   B64D   25/00   (20060101)  
USPTO Field of Search
244/122R   244/122A   244/122AG   244/122B   244/121  
Related Patents
5732907 - Ejection seat buckle - Owned by Capewell Components Company Limited Partnership (Cromwell, CT)

An ejection seat buckle assembly and an arm restraint system incorporating such a buckle assembly wherein the buckle of the assembly includes latch and strike portions each having a respective cable guide ring integrally formed therewith. Arm restraint cables passing through the guide rings deploy safety nets or pull the sleeves or arms of an occupant inward toward the occupant's torso or lap to prevent arm injury during seat ejection from an aircraft. In one embodiment, the guide rings are formed integrally with the latch and strike portions by forming generally oval shaped openings in lap belt adjusters mounted to respective latch and strike engagement portions by latch hinges. In another embodiment, the cable guide rings are D-shaped rings integral with the latch and strike of the ejection seat buckle.

Claims
Description
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