Ami Industries, Inc.

Martin Shawn Day

Chad R Pacheco

Douglas Foisie

Donald Pinkal

Douglas Alexander Foisie

Douglas A Foisie

Donald R Pinkal

Chad R Pachero

An aircraft seat assembly including stanchions defining elongated guide channels and elongated motion sleds nested in the guide channels and affixed to a seat bucket. An energy absorber implemented as a wire bender assembly is coupled between the stanchions and the motion sled. In use, the elongated guide channels guide motion of the motion sleds and the wire bender assemblies attenuate energy during a dynamic event exceeding a predetermined threshold load value. The elongated interface between the guide channels and motion sleds serve to transfer excessive loading to the seat frame thereby protecting the seat assembly from damage and the occupant from excessive lumbar spinal loads.

Aircraft seat with nested energy attenuation guide system

An aircraft seat assembly including first and second stanchions forming interior spaces open through forward slots. A seat pan is pivotally attached to the stanchions and includes rearward extensions that extend through the forward slots and are received in the interior spaces. First and second spring mechanisms reside in the respective first and second interior spaces and are attached at opposing ends to their respective stanchion and to the seat pan. In use, rotating the seat pan toward a deployed position elongates the first and second elongation springs thereby energizing a return force of the spring mechanisms.

Aircraft seat with internal seat pan return spring mechanism

A system may include a vehicular seat assembly including first and second seat support beams, a seat pan, a bar, a fabric seat back, and at least one detachable attachment means. The fabric seat back may have a first end and a second end. The fabric seat back may be secured at the first end to the bar. The fabric seat back may have an expandable seat back section secured at the second end to the seat pan. Each detachable attachment means may be secured at a first detachable attachment means end to the seat pan and may be secured at a second detachable attachment means end to a portion of the fabric seat back located between the first end and the second detachable attachment means end. When all detachable attachment means are in the detached state, an effective length of the fabric seat back may extend.

Vehicular seat assembly having expandable seat back section

A track-mounted aircraft seat has seat track locking pins that are capable of moving independently to remain engaged with the seat track assembly in a warped-floor condition. The seat track locking pins are actuated by means of a pair of torque tubes that rotate independently about a common pilot shaft. A control link, which is operated by the user, acts on a pair of bell cranks each of which acts on one of the torque tubes. The control link is attached to the bell cranks by means of a spherical joint. Because the torque tubes rotate independently and because the spherical joint allows the bell cranks also to move independently, in the event of a warped-floor condition, rotation of one torque tube caused by the skewed seat track will not cause the other torque tube to release its track locking pin.

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Colorado Springs, CO, United States of America

Martin Shawn Day