The invention relates to energy absorbers for passenger seats or the like.
In various modes of transportation, many passenger seats are at least partially surrounded by walls or monuments or may be placed behind other passenger seats where items are mounted to the seat back, such as video displays, telephones, shrouds, or other items.
During a minor crash landing, a passenger may be thrown forward so that the passenger's head and/or body strikes these structures due to inertial loads from the event. Typically, these structures are rigid in nature, so as not to provide any energy absorbing or deflecting features. As a result,
Thus, it may be desirable to provide internal structures with energy absorbing and/or energy deflecting features within a potential strike zone to reduce and/or control the amount of head acceleration a passenger experiences during a minor crash.
Embodiments of the present invention include an active seat back for a passenger seat comprising a seat back comprising a pivot location, at least one active system coupled to the pivot location, and at least one sensing circuit electrically connected to the at least one active system, wherein the at least one sensing circuit comprises integrated logic to monitor for crash scenarios and to transmit a signal to the at least one active system when such a scenario is detected. The passenger seat back may be rotated aft when the at least one active system receives the signal from the at least one sensing circuit.
In certain embodiments, the at least one active system may be configured to provide translational movement and may further comprise an inflator. The at least one active system may be coupled to a connector that is configured to convert the translational movement into rotational movement, such as a crankshaft or a linear actuator and gear.
Embodiments of the present invention may also include an active seat back for a passenger seat comprising a seat back comprising a first pivot location, a head rest coupled to the passenger seat back and comprising a second pivot location, at least one active system coupled to the first and second pivot locations, and at least one sensing circuit electrically connected to the at least one active system, wherein the at least one sensing circuit comprises integrated logic to monitor for crash scenarios and to transmit a signal to the at least one active system when such a scenario is detected. The passenger seat back and the head rest may be rotated to aft positions when the at least one active system receives the signal from the at least one sensing circuit.
According to certain embodiments, the active seat back may be deployed by sensing that a crash has occurred, transmitting a signal to the at least one active system, and rotating the passenger seat back aft. A head rest may be coupled to the passenger seat back, wherein the step of rotating the passenger seat back aft further comprises rotating the head rest aft. The method may further comprise the step of moving the at least one active system.
The described embodiments of the invention provide active seat backs for passenger seats. While the active seat backs are discussed for use with aircraft seats, they are by no means so limited. Rather, embodiments of the active seat backs may be used in passenger seats or other seats of any type or otherwise as desired.
The active system 12 may be coupled to a pivot location 18 of the seat back 16. The pivot location 18 may be positioned adjacent the location where the seat back 16 couples to a seat pan 20. In other embodiments, the seat back 16 may comprise a pivot location 18 that is positioned above the location where the seat back 16 couples to the seat pan 20. For example, the seat back 16 may be configured to maintain a fixed position relative to the seat pan 20 during normal operation, but may include an emergency pivot location 18 for use during crashes. One of ordinary skill in the relevant art will understand that the pivot location 18 may be positioned in any suitable location in the seat back 16.
In certain embodiments, the active system 12 and/or an additional active system 12 may be coupled to a second pivot location 22 adjacent a head rest 24 of the seat back 16.
In these embodiments, the active system 12 may comprise any type of system that is configured to rotate the pivot location 18 and/or 22 and thereby cause an aft rotation of the seat back 16 and/or head rest 24. For example, the active system 12 may comprise a pre-stress system, a compressed spring, an electric motor, a pyrotechnic gas inflator, a cold gas inflator, or other suitable system.
In some embodiments, the active system 12 may comprise a rotational movement design, such as where the active system 12 is an electric motor or other rotational movement device. In these embodiments, the active system 12 may be coupled directly to the pivot location 18 and/or 22 so as to cause an aft rotation of the seat back 16 and/or head rest 24.
In other embodiments, the active system 12 may comprise a translational movement design, such as where the active system 12 is a compressed spring, inflator, or other translational movement device. In these embodiments, the translational movement of the active system 12 must be converted to rotational movement prior to coupling to the pivot location 18 and/ or 20 via a connector 26. For example, as shown in
In other embodiments, as illustrated in
In certain embodiments, the sensing circuit 14 may comprise integrated logic to monitor for crash scenarios and to transmit a signal to one or both active systems 12 when such a scenario is detected. When the active system 12 receives the signal from the sensing circuit 14, the active system 12 begins to move. The sensing circuit 14 may include a battery for reserve power and inflator firing charge capability. The sensing circuit 14 may be electrically connected to one or both active systems 12. For example, the sensing circuit 14 may be an electronics module assembly (“EMA”) or other suitable electronics control module.
In use, when the sensing circuit 14 detects that a crash has occurred, the sensing circuit 14 sends a signal to the active system 12, which in turn causes the active system 12 to move. The active system 12 movement, through its coupling to the pivot location 18, thereby causes the seat back 16 to rotate aft so as to shorten the distance between a passenger's head and the seat back 16. The reduction in distance limits the amount of acceleration that a passenger's head may achieve before impacting the seat back 16, thus also reducing the highest spikes in acceleration.
In the embodiments where the active system 12 is also coupled to the pivot location 22, the active system 12 movement also causes the head rest 24 to rotate aft which both further shortens the distance between the passenger's head and the seat back 16, as well as providing some additional cushioning to absorb at least a portion of the impact of the passenger's head. The additional reduction in distance, as well as the potential cushioning effect, may further limit the amount of acceleration that a passenger's head may achieve before impacting the seat back 16, thus potentially further reducing the highest spikes in acceleration.
The foregoing is provided for purposes of illustrating, explaining, and describing embodiments of the present invention. Further modifications and adaptations to these embodiments will be apparent to those skilled in the art and may be made without departing from the scope or spirit of the invention.
This application is related to and claims priority benefits from U.S. Provisional Application Ser. No. 61/506,689, filed on Jul. 12, 2011, entitled ACTIVE SEAT BACK FOR AIRCRAFT (the “'689 application”). The '689 application is hereby incorporated herein in its entirety by this reference.
Number | Date | Country | |
---|---|---|---|
61506689 | Jul 2011 | US |