Patent classifications
B64D11/0643
Using foam for structural components of a seat assembly
Seat assemblies (200) including structural components (212, 222, 232) made of foam are described. A seat sub-assembly (210, 220, 230) can include a frame (214, 224, 234) and a foam support (212, 222, 232). The foam support (212, 222, 232) can be coupled to the frame (214, 224, 234) for receiving a load on the seat sub-assembly (210, 220, 230), dissipating at least half of the load, and dispersing the load through the frame (214, 224, 234).
VEHICLE SEAT HAVING LEGREST WITH SEAT CUSHION FUNCTION
The present disclosure provides a vehicle seat having a legrest with a seat cushion function, which may mount a legrest on a back portion of a front seatback to be deployable such that a passenger seated on a rear seat may place and support a calf and a foot on the deployed legrest, and recline a front seatback forward to use the deployed legrest as a seat cushion on which the passenger may be seated while facing a passenger seated on the rear seat.
Reversible seat assembly
A reversible seat assembly for use with an airplane. The reversible seat comprises a base assembly and a vertical assembly. The base assembly and the vertical assembly are connected to a support structure and are collectively disposable into and out of a first travel position, a second travel position, and a third travel position. In the first and second travel positions a user or passenger may assume a usual sitting position. In the third travel position the user may assume a reverse sitting position. The base assembly comprises a right segment and a left segment connected and rotationally movable to a central segment. The vertical assembly comprises a lower segment and an upper segment connected to and rotationally movable a middle segment. The reversible seat assembly may further comprise a back armrest connected to an opposite side of said middle segment and structure to provide support to the arms of the user.
Aircraft with crew quarters
An aircraft is disclosed with a fuselage including a cabin delimited by a cabin floor and having crew quarters. The crew quarters include an upper portion above a floor plane defined by the cabin floor and a lower portion beneath the floor plane. The crew quarters include a seat adjustable between a sitting configuration and a berthing configuration. A method of transitioning a crew member of an aircraft to a berthing configuration in a crew quarters is also disclosed.
Aircraft interior structure including actuatable panels and a footwell
An aircraft interior structure may include a primary monument, an auxiliary monument, and a passenger seating section. The primary monument may include one or more storage compartments and a primary panel configured to actuate between a primary panel stowed position and a primary panel deployed position. The auxiliary monument may be spaced a select distance from the primary monument across a floor area of an aircraft cabin, and may include an auxiliary panel configured to actuate between an auxiliary panel stowed position and an auxiliary panel deployed position. The passenger seating section may include a footwell at least partially within the primary monument and proximate to the one or more storage compartments. The footwell may correspond to an aircraft seat. The aircraft seat may be configured to form a bed surface with at least a portion being within the footwell when the aircraft seat is in a lie-flat position.
Aircraft seating module
An aircraft seating module (20) includes a seating mount (26) having a horizontal mounting rail (28) integrally joined to a vertical mounting post (30) at an adjoining elbow (32). The rail (28) includes a mounting boss (34) longitudinally spaced from the post (30) for attachment to an aircraft cabin seat track (18). Both the rail (28) and post (30) include mounting holes (38) for attaching a passenger seat (22) and appended furniture (24) directly to the seating mount (26) and in turn indirectly to the seat track (18) in the cabin floor (12).
Seating apparatus
An aircraft seat including: a seat chassis; a seat assembly including a seat pan and a seat back; the seat pan being mounted to the seat chassis by a first pivoting connection defining a seat pan pivot axis about which the seat pan pivots, the first pivoting connection being configured such that the seat pan can pivot about the seat pan pivot axis without undergoing a related translational movement; the second pivoting connection defining a seat back pivot axis about which the seat back pivots; at least one seat pan link for controlling pivoting of the seat pan about said seat pan pivot axis; wherein the at least one seat pan link is coupled to the seat pan in front of the seat pan pivot axis; and at least one recline link connected to the seat back and the at least one seat pan link.
VEHICLE SEAT
A vehicle seat includes: a base mounted to a floor of a vehicle; a seat cushion that is placed on the base and allowed to be tipped up with a rotating shaft as a fulcrum; an ottoman that is provided on a front side of the seat cushion and extractable between a normal position and an extracted position; a seat back that is provided in a rear end of the seat cushion; and a storage locking mechanism that is capable of relatively moving the ottoman with respect to the seat cushion in a storing direction which is a direction opposite to an extracting direction, wherein the storage locking mechanism is operated such that the seat back becomes in a forward-tiltable state and/or the seat cushion becomes in a tippable state, and locking of the locking mechanism is released so that the ottoman becomes movable in the storing direction.
Paired herringbone high density business class seating arrangement
Described are seating arrangements having at least one set of columns that include an aisle column of seating units positioned adjacent a wall column of seating units. The aisle column is positioned adjacent an aisle, and the wall column is positioned adjacent an exterior wall. Each seating unit has a bed position having a head end and a foot end, wherein at least a height-limited portion of the foot end is less than a delineating height that separates a lower portion of the aisle from a upper portion of the aisle. The seating units in the adjacent columns are longitudinally aligned and positioned adjacent one another, as well as being angled with respect to each other. The height-limited portion of the foot ends in the aisle column is positioned adjacent the aisle, and the height-limited portion of the foot ends in the wall column is positioned within a concave portion of the exterior wall.
AIRCRAFT PASSENGER SEAT WITH ENHANCED LIE FLAT POSITION SPACING
In an illustrative embodiment of an aircraft cabin passenger seating arrangement, first and second adjacent passenger seats are positioned at different angles with reference to a longitudinal axis of an aircraft, and longitudinally offset from each other such that the first seat is positioned forward of the second seat by an amount less than a length of the second passenger seat when in the lie-flat position. The first and second adjacent passenger seats may be longitudinally offset from a third passenger seat separated from the second passenger seat by an aisle, the third passenger seat disposed proximate a fourth passenger seat, such that a row of passenger seats includes two staggered groups of passenger seating. The first passenger seat may be vertically offset from the second passenger seat.