Abstract: A seat release system and device, the system including an interface assembly that provides actuation signaling, an actuation device that communicatively provides mechanical motion in response to the actuation signaling, a cable connected to the actuation device, and a recline release cylinder having a gas release button and a release lever at a first end, and having a cylinder piston arm in the recline release cylinder at a second end. The release lever is attached to a second end of the cable where the cable moves the release lever in response to the mechanical motion of the actuation device. The gas release button vents the recline release cylinder to atmosphere in response to being depressed as a result of the cable moving the release lever. The cylinder piston arm may move in the recline release cylinder in response to the gas release button being depressed.

Abstract: A heated seat for an aircraft includes a heating element disposed on a cushioning material and overlayed by an upholstery. The heating element includes a flexible base and a plurality of thin and flexible heating coils that conform to the seat shape such that no cushioning material is applied between the heating element and the upholstery. By providing direct contact between the heating element and the upholstery, smaller heating elements requiring less electrical power may be used to sufficiently heat the seat compared with traditional heating elements.

Abstract: Contemporary aircraft seats are often designed to meet specifications regarding safety and flightworthiness without much consideration for occupant comfort. The aircraft seats disclosed are designed to achieve a high level of occupant comfort while maintaining a simple, symmetrical, and lightweight construction. The seat comprises a mechanism with an actuator that can reconfigure the seat in TTOL, Task, Enhanced, Zero-G, and Slumber positions that each suit different activities a crew member or passenger may undertake while aboard an aircraft. At least one of the positions supports a neutral body posture, and the chair is thoroughly outfitted with rigid supports, comfortable padding, and a design contoured to the human body to maximize comfort. The seat can be configured with a control mechanism that may allow users to adjust the position of the seat via a mobile device or a control panel configured on the seat.

Abstract: A heated seat for an aircraft includes a heating element disposed on a cushioning material and overlayed by an upholstery. The heating element includes a flexible base and a plurality of thin and flexible heating coils that conform to the seat shape such that no cushioning material is applied between the heating element and the upholstery. By providing direct contact between the heating element and the upholstery, smaller heating elements requiring less electrical power may be used to sufficiently heat the seat compared with traditional heating elements.

Abstract: A seat release system and device, the system including an interface assembly that provides actuation signaling, an actuation device that communicatively provides mechanical motion in response to the actuation signaling, a cable connected to the actuation device, and a recline release cylinder having a gas release button and a release lever at a first end, and having a cylinder piston arm in the recline release cylinder at a second end. The release lever is attached to a second end of the cable where the cable moves the release lever in response to the mechanical motion of the actuation device. The gas release button vents the recline release cylinder to atmosphere in response to being depressed as a result of the cable moving the release lever. The cylinder piston arm may move in the recline release cylinder in response to the gas release button being depressed.

Abstract: A substructure in an aircraft cabin includes a drawer-insert accepting portion that defines multiple racks. Each rack may receive an exchangeable drawer insert. A module-accepting portion of the substructure defines an opening that includes a supporting surface, a back wall which extends upward and outward, and a lateral side wall. A module is provided for optionally installing in the module-accepting portion. The module has concealed areas upon installing that include: (i) a base adapted to rest on the supporting surface, (ii) a side wall adapted to abut the lateral side wall, and (iii) a rear wall adapted to abut the back wall. The module has exposed surfaces upon installing that are adapted to match an existing profile of the drawer-insert accepting portion. The module-accepting portion is configured for stowing cargo in a first mode and for receiving the module in a second mode. The module may include a locking assembly.

Abstract: A substructure in an aircraft cabin includes a drawer-insert accepting portion that defines multiple racks. Each rack may receive an exchangeable drawer insert. A module-accepting portion of the substructure defines an opening that includes a supporting surface, a back wall which extends upward and outward, and a lateral side wall. A module is provided for optionally installing in the module-accepting portion. The module has concealed areas upon installing that include: (i) a base adapted to rest on the supporting surface, (ii) a side wall adapted to abut the lateral side wall, and (iii) a rear wall adapted to abut the back wall. The module also has exposed surfaces upon installing that are adapted to match an existing profile of the drawer-insert accepting portion. The module-accepting portion is configured for stowing cargo in a first mode and for receiving the module in a second mode.

Abstract: A multi-function credenza includes at least one cabinet with a first top surface and a seat adjacent the cabinet. The seat has a convertible seat back for converting to a second top surface adjacent to the first top surface when the seat is stowed. A multi-function credenza in an aircraft cabin includes a first cabinet that has a first inboard panel and a first top surface, a second cabinet that has a second inboard panel and a second top surface, and a stowable seat located between the first cabinet and the second cabinet. A stowable seat includes a seat back that has a first side adapted for seating in a first mode and a second side adapted as a working surface in a second mode. The seat back articulates between the first mode and the second mode for deploying and stowing the seat, respectively.

Abstract: A system and method for simulating a structure is disclosed. An adjustable interior mockup for simulating a structure has a base with a first elongated side and a second elongated side, the first elongated side being nonadjacent the second elongated side; and an adjustable frame secured to the base. The adjustable frame includes a plurality of girder members secured along the first and second elongated sides to form an arc; a plurality of brackets; a plurality of arms having a latch attached to one end; and a sheet of fabric. The girders are securely fastened along the first elongated side of the base at predetermined intervals; the brackets are secured to the girders; the arms are received by the brackets and adjustably anchored to the girders via a fastener; and the latches engage the sheet of fabric, thus pulling the fabric into a shape that resembles the structure.

Abstract: A system and method for simulating a structure is disclosed. An adjustable interior mockup for simulating a structure has a base with a first elongated side and a second elongated side, the first elongated side being nonadjacent the second elongated side; and an adjustable frame secured to the base. The adjustable frame includes a plurality of girder members secured along the first and second elongated sides to form an arc; a plurality of brackets; a plurality of arms having a latch attached to one end; and a sheet of fabric. The girders are securely fastened along the first elongated side of the base at predetermined intervals; the brackets are secured to the girders; the arms are received by the brackets and adjustably anchored to the girders via a fastener; and the latches engage the sheet of fabric, thus pulling the fabric into a shape that resembles the structure.

Abstract: An articulating armrest includes a first protrusion and a second protrusion that protrude from a member a predetermined spacing apart. Each protrusion aligns within a separate track within a housing configured for stowing the armrest within a seat back. The two tracks include straight and curved portions configured to articulate the armrest. Specifically, the armrest moves along a curvilinear path between stowed and deployed positions by translating along the tracks and pivoting about the second protrusion. The armrest may stow in a seat back and beneath the seat bottom to provide a full length armrest when deployed, and the armrest may stow flush with the seat back for sitting against. Mechanical tension may be provided to automatically deploy the armrest, and a rotational damper and a gas spring may be used to control the speed at which the armrest deploys.

Abstract: A system and method for simulating a structure is disclosed. An adjustable interior mockup for simulating a structure has a base with a first elongated side and a second elongated side, the first elongated side being nonadjacent the second elongated side; and an adjustable frame secured to the base. The adjustable frame includes a plurality of girder members secured along the first and second elongated sides to form an arc; a plurality of brackets; a plurality of arms having a latch attached to one end; and a sheet of fabric. The girders are securely fastened along the first elongated side of the base at predetermined intervals; the brackets are secured to the girders; the arms are received by the brackets and adjustably anchored to the girders via a fastener; and the latches engage the sheet of fabric, thus pulling the fabric into a shape that resembles the structure.

Abstract: A multi-function credenza includes at least one cabinet with a first top surface and a seat adjacent the cabinet. The seat has a convertible seat back for converting to a second top surface adjacent to the first top surface when the seat is stowed. A multi-function credenza in an aircraft cabin includes a first cabinet that has a first inboard panel and a first top surface, a second cabinet that has a second inboard panel and a second top surface, and a stowable seat located between the first cabinet and the second cabinet. A stowable seat includes a seat back that has a first side adapted for seating in a first mode and a second side adapted as a working surface in a second mode. The seat back articulates between the first mode and the second mode for deploying and stowing the seat, respectively.

Abstract: A system and method for simulating a structure is disclosed. An adjustable interior mockup for simulating a structure has a base with a first elongated side and a second elongated side, the first elongated side being nonadjacent the second elongated side; and an adjustable frame secured to the base. The adjustable frame includes a plurality of girder members secured along the first and second elongated sides to form an arc; a plurality of brackets; a plurality of arms having a latch attached to one end; and a sheet of fabric. The girders are securely fastened along the first elongated side of the base at predetermined intervals; the brackets are secured to the girders; the arms are received by the brackets and adjustably anchored to the girders via a fastener; and the latches engage the sheet of fabric, thus pulling the fabric into a shape that resembles the structure.