Crash survivable seat

• US 4,150,805 A
• Filed: 10/20/1976
• Issued: 04/24/1979
• Est. Priority Date: 10/20/1976
• Status: Expired due to Term

• Current Assignee: ARA Incorporated
• Original Assignee: ARA Incorporated
• Inventors: Mazelsky, Bernard
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US05/734,362
• Time in Patent Office: 916 Days
• Field of Search: 244/122 R, 244/122 AG, 244/138 R, 244/151 R, 188/1 B, 188/1 C, 188/1 R, 297/216, 74/492, 52/98, 114/247
• US Class Current: 244/122.00R
• CPC Class Codes: B64D 25/04 Seat modifications

Abstract

A tri-axis crash survivable seat, utilizing a plurality of energy absorbers, which are swivel mounted to the seat bucket and also to a frame where the frame is securely fastened to the structure of a rotary wing or fixed wing aircraft. The energy absorbers are utilized in upper, intermediate and lower pairs, each having different energy absorbing characteristics, stroking distances, and force-displacement relationships from the other pairs. The energy absorbing devices attach to the bucketseat and supporting frame so as to permit tri-axial energy absorption during impact for various vertical or combined vertical impact angles. Each of the intermediate pair of energy absorbing devices is a two stage device designed to minimize the dynamic overshoot associated with the elasticity of the human body, such that a reduced probability of injury is obtained. Energy is dissipated in a controlled manner through the process of the displacement of the seat relative to the craft under arbitrary crash conditions.

Claims

1. An improved crash survivable seat for rotary wing and fixed wing aircraft of the type having a seat bucket, a carriage for said seat bucket secured to the craft structure, and a plurality of energy absorbing devices interconnecting said seat bucket and carriage, said plurality of energy absorbing devices including at least one upper pair of energy absorbing devices and at least one lower pair of energy absorbing devices, wherein the improvement comprises:

said upper pair and said lower pair of energy absorbing devices being operable to absorb energy in both tension and compression and having the capability of absorbing energy at all times during crash induced motion;

energy absorbing means interconnecting said seat bucket and said carriage for controlled transfer of force to said seat in stages wherein said energy absorbing means is responsive to crash induced seat displacement, said energy absorbing means comprising at least one pair of energy absorbing devices disposed intermediately of said upper pair of energy absorbing devices and said lower pair of energy absorbing devices including;

first rupturable means responsive to initial crash induced forces for transfer of force to said seat to a predetermined maximum value;

second elastically deformable means responsive to crash induced seat displacement for absorption of energy at a substantially constant force transfer below said predetermined maximum value of said first means;

third elastically deformable means responsive to crash induced seat displacement for absorption of energy at a substantially constant force transfer intermediate to the force values of said first and second means; and

means for connecting each said energy absorbing means to said seat and said carriage for permitting concurrent vertical lateral and longitudinal displacements of said seat for arbitrary crash angles, the response of said first means, said second means and said third means occurring sequentially with a force-displacement relationship substantially as shown by the graph;

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2. The invention as set forth in claim 1 further including a first receptacle pair carried by said seat bucket and a second receptacle pair carried by said carriage, said first receptacle pair articulating with one pair of ball joint ends of said upper pair of energy absorbing devices, and said second receptacle pair articulating with said pair of other ball joint ends of said upper pair of energy absorbing devices, such that said upper pair of energy absorbing devices is pivotably coupled to said seat bucket and to said carriage.

3. A crash survivable seat for aircraft comprising:

a seat bucket;

a carriage secured to said aircraft, said seat bucket being attached to said carriage;

a plurality of energy absorbing means connected between said seat bucket and said carriage, said energy absorbing means comprising upper energy absorbing means, lower energy absorbing means, and intermediate energy absorbing means, the latter comprising first rupturable means responsive to initial crash induced forces for transfer of force to said seat only until a predetermined maximum value of force has been reached, second elastically deformable means responsive to crash induced seat displacement for absorption of energy thereafter at a substantially constant force below said predetermined maximum value of said first energy absorbing means, and third elastically deformable means responsive to crash induced seat displacement for absorption of energy at a substantially constant force below said predetermined maximum value of said first means, and different from the force at which said second means absorbs energy, said upper and said lower energy absorbing means being operable to absorb energy in both tension and compression and having the capability of absorbing energy at all times during crash induced motion, said plurality of energy absorbing means being connected between said seat bucket and said carriage at such different angles as to provide for energy absorption upon displacements in a vertical, fore-and-aft or laeral direction.

4. The invention as set forth in claim 3 wherein said upper energy absorbing means comprises at least an upper pair of energy absorbers, and wherein said lower energy absorbing means comprises at least a lower pair of energy absorbers, and wherein said intermediate energy absorbing means comprises at least an intermediate pair of energy absorbers.

5. The invention as set forth in claim 3 wherein said third means absorbs energy at a substantially constant force intermediate between said predetermined maximum value of force of said first means and said substantially constant force of said second means.

6. The invention as set forth in claim 3 wherein said first means, said second means and said third means respond sequentially to a crash with a force-displacement relationship substantially as shown by the graph:

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