Ami Industries, Inc.

Douglas Foisie

Chad R Pacheco

Martin Shawn Day

Kyler Marutzky

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 flexible actuation assembly for an aircraft component may include a flexible linkage including at least one primary element. The at least one primary element may be coupled to at least one locking pin of the flexible actuation assembly via at least one interlocking assembly. The flexible linkage may be coupled to an actuator of an aircraft component. The flexible linkage may be configured to retract the at least one locking pin from a lock position when a load applied to the actuator is translated through the flexible linkage. The flexible linkage may be fabricated from a material with a spring force able to return the at least one locking pin to the lock position when the load is removed from the actuator.

Flexible actuation assembly for an aircraft component

In various embodiments, the present disclosure provides an energy attenuating mounting foot comprising a load beam having a longitudinal axis, a top surface, a bottom surface, an inner track interface lobe, and an outer track interface lobe, the inner track interface lobe and the outer track interface lobe extending laterally from the load beam, and a channel along the longitudinal axis having a depth extending from the load beam bottom surface toward the top surface. In various embodiments, the inner track interface lobe has a first length extending in a direction from the bottom surface towards the top surface and the outer track interface lobe has a second length extending in a direction from the bottom surface towards the top surface, the first length being less than the second length.

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Colorado Springs, CO, United States of America

Douglas Foisie