Patent US4005765A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4005765A Expired / Lapsed US ⏱️ 0.0 years remaining

Crash load attenuating troop seat

Assignee: United States Department of the Navy
•
Filing: 1975-02-24
•
Granted: 1977-02-01
•
Expires: 1995-02-24
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A lightweight, low cost, collapsible, side-facing seat construction for tp carrying aircraft designed to attenuate crash load forces in an improved manner. A fabric seat sling depending from a support strap assembly is suspended via energy absorbing devices from an aircraft overhead frame structure and is supported by a simple pivoted strut assembly secured to the aircraft floor structure. Shoulder and lap safety belts are secured through the seat by tie-down straps angled outwardly from both sides of the seat directly to the aircraft floor for increased occupant safety and anti-sway resistance. A minimum of rigid, heavy, relatively expensive compression-carrying structural members is thus utilized in this unique seat while providing maximum comfort and safety to its occupant.

Inventors

  • 👤 Mason J. Reilly

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 15:14
CPC Classifications
B; B60; B60N; B60N2/00; B60N2/24; B60N2/42; B60N2/4207; B60N2/4242; B64; B64D; B64D25/00; B64D25/02; B64D25/04

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 127 words
A shock absorber of the metal deforming type for use in conjunction with a strap-supported troop seat to absorb sudden impact comprising: a hollow housing having two opposed openings thereto; first and second rods spatially separated and laterally positioned between said openings and secured at their ends to the interior walls of said housing; a shock absorbing wire bent back upon itself near its midpoint and formed to connect to the aircraft defining first and second wire halves, said first and second wire halves each weaving from the midpoint into one of said openings around the distal sides of respective ones of said rods, crossing between said rods, weaving around the distal sides of the respective others of said rods and out the other of said openings.
Claim 2
Dependent Claim 127 words
A shock absorber of the metal deforming type for use in conjunction with a strap-supported troop seat to absorb sudden impact comprising: a hollow housing having two opposed openings thereto; first and second rods spatially separated and laterally positioned between said openings and secured at their ends to the interior walls of said housing; a shock absorbing wire bent back upon itself near its midpoint and formed to connect to the aircraft defining first and second wire halves, said first and second wire halves each weaving from the midpoint into one of said openings around the distal sides of respective ones of said rods, crossing between said rods, weaving around the distal sides of the respective others of said rods and out the other of said openings.

References Cited (Backward Citations)

US261121A Cited
GB189415068A Cited
US1511264A Cited
US3057526A Cited
US3087584A Cited
US3289260A Cited
US3377044A Cited
US3372773A Cited
DE1506641A1 Cited
US3446533A Cited
US3547468A Cited
US3730586A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-02-01 1980-08-02 1981-02-01 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-02-01 1984-08-02 1985-02-01 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-02-01 1988-08-02 1989-02-01 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag