The Boeing Company

Other

James P Schalla

Heidi Joy Kneller

William Anthony Harkness

Buddy Lee Sharpe

Calsee Nicole Robb

Mark Edward Wentland

Bret L Lamoree

Phillip J Bobzien

Dennis C Lin

Michael John Burgess

Richard Leroy Rankin

Jeff Duce

Michael J Burgess

Bradley James Mitchell

Karen Lee Hills

Douglas Alan Brown

Kwun-Wing W Cheung

Kevin S Zielke

Shawn A Claflin

Thomas Joseph Moran

Marcus K Richardson

Raymond H Horstman

Jason Turner

Tateh Wu

Robert J Bengtsson

Ralph N Bladt

Justin William Balvanz

Ashley LaGwyn House

Miguel A Remedios

Kevin Scott Callahan

Ty Aaby Larsen

Yakentim M Ibrahim

William C Quan

David R Space

Mark E King

Nino Senoadi

James Jason Salmon

Steven H Sauer

James Paul Mehlos

Bethany L Franko

Nicholas A Jones

Mark Gus Mehlhaff

Bryce A Van Dyke

Kwu-Wing W Cheung

Eric Anthony Hill

Roland Von Ballmoos

Kyongsoo Chae

Daniel T Sim

Shawn A Clafin

Gabriel Lynn Miller

Lyndsey Jo Penfield

Mark G Mehlhaff

Justin W Balvanz

Chae Kyongsoo

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 galley cart has a rear wall with an inlet port and an outlet port. A first divider has a first edge, wherein a first distance is defined between the first edge and a front wall. A second divider has a second edge, wherein a second distance is defined between the second edge and the front wall. The second distance is less than the first distance for control of the flow of cooling air.

Optimally configured air-flow galley cart

The present disclosure provides system for sealing a refrigerated galley of an aircraft. The system includes a door, and a seal assembly positioned at a bottom surface of the door. The seal assembly includes (i) a housing coupled to the bottom surface of the door, (ii) a seal positioned at least partially in the housing, wherein the seal is moveable relative to the housing and the door, (iii) a biasing mechanism coupled to the housing and the seal and configured to hold the seal in a relaxed state by applying a biasing force to the seal in a direction away from a floor surface of the refrigerated galley, and (iv) an activation mechanism coupled to the housing. The activation mechanism is configured to transition the seal from the relaxed state to a compressed state in response to a rotation of the door from an open position to a closed position.

Systems and methods for sealing a refrigerated galley of an aircraft

In one embodiment, A lice removal comb system includes an inner comb and an outer comb. The inner comb may include a row of lice-removing tines and a handle. The outer comb may include a first row of hair-detangling tines, a second row of hair-detangling tines, a handle, and a slot formed in the outer comb, between the first and second rows of hair-detangling tines. The outer comb may be configured to removably receive the inner comb such that the row of lice-removing tines is disposed between the first and the second rows of hair-detangling tines.

Lice comb system

The present disclosure provides a system for sealing a compartment. The system includes a door with a seal positioned on a bottom surface of the door. The system also includes one or more hinges coupled to the door. The door rotates from a closed position to an open position via the one or more hinges. A height of the door with respect to a floor surface increases in response to a rotation of the door from the closed position to the open position due to a helical slope of both a first cam surface of the one or more hinges and a second cam surface of the one or more hinges. The seal transitions from a compressed state to a relaxed state in response to the rotation of the door from the closed position to the open position.

Systems and methods for sealing a compartment

A galley for an aircraft includes a frame having metal structural members having interior surfaces and panels coupled to and supported by the frame. Each panel has a core and a facesheet having an inner surface. The frame and the panels define a cart compartment configured to receive a galley cart. The interior surfaces of the metal structural members are interior of the inner surface of the corresponding facesheet. The galley includes a cooling system having a supply duct and a return duct along one or more of the panels in flow communication with the cart compartment configured to supply cooled airflow from a heat exchanger. The galley includes insulating panels located in the cart compartment covering the interior surfaces of the corresponding metal structural members.

Galley and method of assembling a galley

A system and method are disclosed for displaying the storage status of overhead luggage storage bins in an aircraft. A camera is provided that is mounted with a field of view directed at an inner portion of a group of open bins. The camera is communicatively coupled to a controller and selectively provides images of the inner portion of the bins immediately prior to when the bins are closed to the controller. A projector is also provided for each group of bins. The projector is communicatively coupled to the controller and is mounted such that an image received from the controller is projected onto an outer surface of the closed bins. The controller receives images from each of the cameras and selectively provides such images to the projector associated with each camera so that a storage status display is projected on an outer surface of the bins.

System for displaying the status of use of aircraft overhead luggage storage bins

Embedded lighting, microphone, and speaker features for composite panels are described. An example composite panel includes a plurality of plies assembled in a stack-up, and a trace sheet with electrically conductive traces and a plurality of transducer discs positioned onto the electrically conductive traces at positions such that the electrically conductive traces form an electrical interconnection between selected ones of the electrically conductive traces and associated ones of the transducer discs. The trace sheet is included as an internal ply in the stack-up of the plurality of plies. The composite panel also includes a composite base upon which the stack-up of the plurality of plies is applied, and the plurality of plies are cured upon the composite base to integrate the trace sheet and the plurality of transducer discs into the composite base.

Method of manufacturing a composite panel

A stowage container including a barrier such as a door or access panel and a breach detector for monitoring and/or detecting a breach of the barrier. The breach detector includes an indicator assembly having a slot that can be positioned between, and defined by, a front panel and a back panel of the barrier, and an indicator within the slot. The indicator assembly further includes a retainer that maintains the indicator in a first state when the barrier is in a first position (e.g., closed or sealed) and which releases the indicator into a second state when the barrier moves from the first position to a second position (e.g., open or breached). Upon returning the barrier to the first position, the indicator remains in the second state until the indicator reset to the first state.

Stowage container with breach detection and indication system

Lighting panels and methods of manufacturing lighting panels are described. An example lighting panel includes a substrate that has a planar surface, electrically conductive traces printed onto the planar surface of the substrate, and light sources mounted onto the electrically conductive traces at mounting positions such that the electrically conductive traces form an electrical interconnection between selected ones of the electrically conductive traces and associated ones of the light sources. The lighting panel also includes a polymer sheet provided over the light sources, and a composite base upon which a stack-up of the substrate with the printed electrically conductive traces, the light sources, and the polymer sheet is applied. The light sources are embedded into the composite base and are also flush with a top surface of the stack-up, and the substrate is also embedded into the composite base underneath the light sources at the mounting positions.

Embedded lighting features for lighting panels

In one embodiment, an unmanned aircraft comprises a housing, an inflatable fuselage, three motors, and three propellers. The housing may comprise an enclosure configured to house one or more electrical components. The inflatable fuselage may comprise a first, a second and a third spindle each extending from the housing. The first motor may be coupled to a first propeller and mounted to the first spindle. The second motor may be coupled to a second propeller and mounted to the second spindle. The third motor may be coupled to a third propeller and mounted to the third spindle.

Unmanned inflatable aircraft

An aircraft is provided that includes a passenger service unit for a passenger seated in a seat in its cabin. The aircraft includes a camera configured to acquire an image of the passenger, and a control module configured to at least receive the image of the passenger. The control module is configured to receive non-tactile gesture preference data and dominant hand data, and access a non-tactile gesture data store that includes a plurality of images of non-tactile hand signals or non-tactile hand gestures. Based on the foregoing, the control module is configured to generate non-tactile gesture data in accordance with and indicative of a non-tactile hand signal or a non-tactile gesture made by the passenger. And the control module is configured to control one or more cabin systems including in at least one instance the passenger service unit based on the non-tactile gesture data.

Aircraft having gesture-based control for an onboard passenger service unit

A galley refrigeration system includes a liquid heat exchange loop and an air heat exchange loop in thermal communication with the liquid heat exchange loop. The air heat exchange loop includes a heat exchanger configured to be coupled in flow communication with at least one galley cart. Optionally, the galley refrigeration system may include a control system in operative communication with the liquid heat exchange loop and the air heat exchange loop.

Galley refrigeration system of an aircraft

Growing community of inventors

Seattle, WA, United States of America

James P Schalla