Dynamically tilted seat pan

Patent metadata

Field	Value
Publication number	US-10899456-B2
Application number	US-201715727361-A
Country	US
Kind code	B2
Filing date	Oct 6, 2017
Priority date	Oct 6, 2017
Publication date	Jan 26, 2021
Grant date	Jan 26, 2021

Abstract

An apparatus for dynamically tilting a seatpan in an aircraft passenger seating assembly includes a seat frame, seatback, seat cushion, and cushion support structure (e.g., a seatpan), the seat cushion and seatpan together having a forward end and a rear end and together supporting a passenger occupying the seating assembly. Accelerometers may detect an inertial event such as a rapid deceleration that may cause the passenger to pitch forward; dynamic seatpan actuators (e.g., airbags or ballistic devices) connected to the accelerometers react to the inertial event by detonating, driving the seatpan and seat cushion upward. As a result, the head path of the passenger may be redirected upward, alleviating the risk of passenger injury and component damage. Additional airbags may react to the inertial event by tightening the passenger seatbelt.

First claim

We claim:

1. A dynamically tilting seat assembly, comprising:
a seat frame mountable within an aircraft, the seat frame comprising a left-side portion and a right-side portion connected by one or more lateral rails including a forward rail and a rear rail;
a seatpan pivotably coupled to the seat frame, the seatpan having a forward end proximate to the forward rail and a rear end proximate to the rear rail;
at least one detector configured to detect an inertial event associated with the aircraft;
and
at least one ballistic device coupled to the at least one detector and to the forward rail, the at least one ballistic device configured to propel the seatpan upward by driving a piston into the forward end in response to the inertial event.

2. The dynamically tilting seat assembly of claim 1 , further comprising:
at least one seatbelt coupled to the seat frame, the at least one seatbelt configured to adjustably secure a passenger occupying the seat assembly;
and
at least one supplemental dynamic seatpan actuator (DSA) disposed proximate to the rear end and coupled to the at least one detector, the at least one supplemental DSA configured to inflate in response to the inertial event.

3. The dynamically tilting seat assembly of claim 2 , further comprising:
at least one seatbelt coupled to the seat frame, the at least one seatbelt configured to adjustably secure a passenger occupying the seat assembly;
and
at least one second supplemental airbag coupled to the at least one seatbelt.

Assignees

• Rockwell Collins Inc

Inventors

• Penley Randy
• Thompson Jeff B
• Barg Bradley
• Pierson-Moonan Jay

Classifications

• B60N2/4279

  electric or electronic triggering · CPC title

• B64D11/06 Primary

  Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title

• B64D11/0619 Primary

  with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash · CPC title

• B60R21/23

  Inflatable members (B60R21/18 takes precedence; connection to inflation fluid source retainers B60R21/217) · CPC title

• B60R21/18

  the inflatable member formed as a belt or harness or combined with a belt or harness arrangement · CPC title