The Boeing Company

Theboeing Company

James A Fullerton

Max Urban Kismarton

David Henry Wykes

Sebastian Petry

Blake Emery

Don Chadwick

David R Space

Jeffrey Bernett

Scott Edward Coburn

Timothy J Arnaud

R Klaus Brauer

Jayant Dahyabhai Patel

John N Harris

Stephen M Trent

Sergio H Sanchez

Bradley James Mitchell

Kevin Scott Callahan

Mithra M K V Sankrithi

Trevor Milton Laib

Sergey D Barmichev

Ty Aaby Larsen

Shawn A Claflin

Douglas Alan Brown

Mark Edward Wentland

William C Sanford

Melanie L Kimsey-Lin

Gary Lee Senechal

Charles A Stout

Jon B Shaw

Gregory Eisele

Stephanie K Licht

R Klaus-Brauer

Myriam Khalil

Bobbie Lee Cole

Gregory T Eisele

Jon Burton Shaw

A system and method include a seat assembly including a seat duct fluidly coupled to one or more air outlets. An air delivery manifold is underneath the seat assembly. The air delivery manifold includes a first outlet port. The seat duct is fluidly coupled to the first outlet port. Air is delivered to the one or more air outlets via the air delivery manifold.

Ventilation systems and methods for internal cabins of vehicles

A headrest ventilation assembly is configured to secure to a headrest of a seat assembly, and includes an air conduit including one or more air inlets and one or more air outlets, and an air filter disposed within the air conduit between the one or more air inlets and the one or more air outlets. The air filter is configured to remove contaminants from the air that is drawn into the air conduit before being delivered out of the one or more air outlets. The assembly can also include a fan disposed on or within the air conduit. The fan is configured to draw the air into the one or more air inlets and provide airflow to deliver the air out of the one or more air outlets. The assembly can also include one or more ultraviolet (UV) light emitters disposed on or within the air conduit. The UV light emitter(s) are configured to emit UV light into the air to sanitize the air before the air is delivered out of the one or more air outlets.

Headrest ventilation systems and methods for seating assemblies

A lavatory is provided which includes a plurality of walls including a first wall having a doorway, and an expandable door. The expandable door includes a main panel having dimensions that conform to the doorway and a main hinge connecting the main panel to the first wall. The lavatory further includes a latch. The main panel is configured to, in a deployed state, increase in at least one dimension to form a privacy barrier around an expansion zone located outside of the plurality of walls. The latch is configured to lock the expandable door in place in the deployed state.

Lavatory with expandable door

An aircraft and method of deterring avian species from the aircraft include a lighting system including a lighting assembly coupled to the exterior. The lighting assembly includes an ultraviolet (UV) light-emitting element that emits UV light outside of the aircraft.

Avian-deterring lighting systems and methods for aircraft

A fuselage is described that includes a plurality of frames and a plurality of seat rows spaced apart according to a seat pitch. Each frame includes a lateral floor beam, and each seat row of the plurality of seat rows includes a load-bearing structural base with a plurality of legs attached to a proximal lateral floor beam and a distal lateral floor beam. Each seat row also includes a seat or bank of seats attached to the load-bearing structural base, where the seat or bank of seats includes at least one seat bottom and at least one seat back. Further, each seat row includes an interface between (i) the load-bearing structural base and (ii) the seat or bank of seats to allow for attachment and detachment of the seat or bank of seats relative to the load-bearing structural base.

Integrated aircraft fuselage and load-bearing structural base for aircraft seats

A room partition assembly is configured to selectively convert an area within an internal cabin of a vehicle between a standard use and a non-standard use. The room partition assembly includes a mounting frame that is configured to be secured to a monument within the internal cabin, and a panel that is moveably coupled to the mounting frame. The panel is selectively moved between a retracted position and an extended position with respect to the mounting frame. The area is configured for the standard use when the panel is in the retracted position. The area is configured for the non-standard use when the panel is in the extended position.

Room partion assemblies, systems, and methods

A foot washing system includes a support panel, and a basin including a foot-washing area and a drain that is configured to drain water out of the foot-washing area. The basin is moveably coupled to the support panel. The basin is selectively moveable between a stowed position and a deployed position in relation to the support panel. The deployed position allows for foot washing within the foot-washing area.

Foot washing systems and methods

A multifunctional fully integral panel system design, a unique material configuration, and a process for fabricating a net shape (or nearly net shape) panel in one production cycle. The panel may comprise a base facing with an outer perimeter, a decorative film applied to the exterior of the base facing, an aft facing having an outer perimeter fused to the base facing, and a reinforcement core disposed between the unfused portions of the base and aft facings, which reinforcement core also acts as acoustic insulation (i.e., a noise attenuator). Alternatively or additionally, a foam core or blanket having thermal and/or acoustic insulation properties is attached to the external surface of the aft facing. The fabrication process involves the application of different heat treatments to panel components having different forming temperature or rubbery/elastic plateaus.

Aircraft interior panels and methods of panel fabrication

A method for providing purified air to an occupant of a seat in a mask lacking corporeal features that is generated by an apparatus. The apparatus includes a contaminant conditioning system that delivers purified air to a first and a second laminar flow generator. Each laminar flow generator produces a respective laminar flow that combines to form and fill a breathing space with purified air that envelopes an inhalation sphere of the occupant and inhibits air other than the purified air from entering the breathing space.

Personal ventilation in an aircraft environment

An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.

Modular passenger seat for an aircraft

An aircraft passenger seat configured in accordance with an embodiment of the invention utilizes composite materials to achieve significant weight savings relative to conventional seat designs. The seat includes one or more lightweight composite support legs, a lightweight composite seat pan, and a lightweight composite seat back structure. The support legs are coupled to the seat pan, which is in turn coupled to the seat back structure. The support legs utilize composite frame elements that are formed as continuous compression molded composite extrusions. The seat pan includes composite fore and aft cross beams that are also formed as continuous compression molded composite extrusions. The aft cross beam includes a rear flange that serves as a flexible 'hinge' for the seat back structure. The seat can leverage producible and relatively inexpensive composite manufacturing techniques such that the seat can be economically produced for use as an economy class seat.

Method of manufacturing a composite leg structure for a lightweight aircraft seat assembly

A composite seat pan for a lightweight aircraft passenger seat includes an open-section fore cross beam, an open-section aft cross beam and a seat pan membrane carried by the fore cross beam and the aft cross beam.

Composite seat pan structure for a lightweight aircraft seat assembly

Composite leg structure for a lightweight aircraft seat assembly

Growing community of inventors

Bothell, WA, United States of America

James A Fullerton