The Boeing Company

James Jason Salmon

Patrick William O'Neill

Sergey D Barmichev

Ty Aaby Larsen

James P Schalla

Nick Shadbeh Evans

Gregg W Podnar

Michael Allan Long

David R Space

Richard John Loftis

Nicholas A Jones

Keith Harrell

Gregory Earl Mattocks

Eric Anthony Hill

Gabriel Lynn Miller

Scot McKee

Mark Gordon Sellars

Michael Joseph Surface

Jeffrey Scott Roberts

Daniel T Sim

Scot Mckee

A ventilation assembly comprises a number of fan systems configured to purify air and a number of air distribution assemblies. Each air distribution assembly of the number of air distribution assemblies is configured to be removably installed on a seatback of a passenger seat. Each air distribution assembly of the number of air distribution assemblies comprises a pair of air distribution vents, ductwork configured to receive air from at least one fan system of the number of fan systems and direct air to the pair of air distribution vents, and a seat attachment device configured to removably couple the pair of air distribution vents to the seatback such that each air distribution vent is situated on opposite sides of the seatback for providing purified air to a seated passenger.

Ventilation assembly in an aircraft

A method including executing a logical computing element (LCE) on a server. Worker LCEs are executed on the server. A first electronic file comprising geometry data in a first data structure is received at the controller LCE. An available worker LCE is identified, by the controller LCE, as an in-use worker LCE from among the worker LCEs. The geometry data is imported by the in-use worker LCE. A job instance is established by the in-use worker LCE. A rendering engine is launched by the in-use worker LCE. The rendering engine generates, for the job instance and using the geometry data, a dataset file in a second data structure different than the first data structure. The dataset file is returned by the in-use worker LCE to the controller LCE. The dataset file is returned by the controller LCE to a remote computer.

Method for automatic creation of real-time rendering content

A component positioning system and method are configured to facilitate positioning of a component (such as a seat assembly) on a seat track within an internal cabin of a vehicle. The component positioning system and method include a component, and a position indicator coupled to a portion of the component. The position indicator emits a proper position indication when the component is in a proper position in relation to the seat track. The position indicator emits a remedial position indication when the component is not in the proper position with respect to the seat track.

Component positioning systems and methods for an internal cabin of vehicle

Systems and methods are provided for handling luggage. One exemplary system includes an interface that receives input from a check-in system that indicates sizes and weights for pieces of luggage that are each associated with a unique identifier; and a controller that selects a delivery, identifies pieces of luggage for the delivery, correlates the delivery with dimensions of a cargo hold of a vehicle servicing the delivery, receives input indicating a loading restriction for loading luggage into the cargo hold, and generates a baggage map. The baggage map is based on the sizes and the weights of the pieces of luggage for the delivery, indicates a location for each piece of luggage for the delivery within the cargo hold, and complies with the loading restriction. The system further includes a memory that stores the baggage map.

Intelligent baggage handling

A landing gear for an aircraft. The landing gear may have a wheel/truck assembly, an oleo strut/support frame for supporting the wheel/truck assembly, and a retraction assembly attached to the oleo strut/support frame, the retraction assembly for moving the landing gear between a deployed position and a retracted position. The retraction assembly may have a pivoting trunnion brace attached to the oleo strut/support frame and to a fuselage of the aircraft for positioning the wheel/truck assembly, the oleo strut/support frame and the retraction assembly at least substantially fully within the fuselage of the aircraft in the retracted position.

Fuselage mounted landing gear

A substantially strong, lightweight load bearing window for use in a mobile platform, for example, an aircraft. The window includes a rim portion having a carbon reinforced resin structure and a transparent portion having a fiberglass reinforced resin structure. A plurality of holes are formed in the rim portion for enabling a plurality of connectors to be inserted therethrough. The rim portion has a smaller cross sectional area (i.e., thickness) than the transparent portion such that the rim portion is adapted to fit behind a skin of an aircraft, the transparent portion is adapted to be flush with the skin of the aircraft. The connectors fix the window to the skin of the aircraft. The window effectively forms a strong, structurally integral portion of the skin.

Load bearing window

A method and apparatus for actuating an aircraft nose portion. The aircraft can have a longitudinal axis and a pitch axis generally transverse to the longitudinal axis. The fuselage can include a pressure bulkhead and a pressurized payload portion aft of the pressure bulkhead. The nose portion can be positioned forward of the pressure bulkhead and can be changeable from a first configuration to a second configuration while the pressurized payload portion is capable of being pressurized relative to a region external to the aircraft. For example, the nose portion can be inclined upwardly relative to the longitudinal axis when pivoted from a first position to a second position. Accordingly, the length of the aircraft can be reduced, for example, to accommodate the aircraft at a loading gate or other ground support area.

Method and apparatus for actuating an aircraft nose portion

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Kirkland, WA, United States of America

James Jason Salmon