B/e Aerospace, Inc.

James Brian Hauser

Shawn A Claflin

Jefferey M McKee

Robert Papke

Wade Johnson

Frank E Hashberger

Clarence Ivester

Erik Eivind Sutton Nilsen

Mark Robert Hacker

David R Benton

William David Noble

Anthony Earl Chamberlin

Jeffery Mckee

In a preferred embodiment, a vertically stowable aircraft storage unit for providing additional storage in a cabin area of an aircraft can include a storage compartment and a vacuum lift mechanism for lifting and lowering the storage compartment between a stowed position and a deployed position. The vacuum lift mechanism can include at least one vacuum actuator in fluid communication with a vacuum source. The aircraft storage unit can further include an overhead mounting frame for mounting the vacuum lift mechanism to an upper structure of an interior of the aircraft, and a storage compartment frame configured to releasably receive the storage compartment. The vacuum lift mechanism may be releasably attached, at an upper end, to the overhead mounting frame, and at a lower end, to the storage compartment frame. The upper structure of the interior of the aircraft can be above a ceiling of the cabin area.

Vacuum powered actuation mechanism for a vertically stowable aircraft storage unit

In an illustrative embodiment, a vertically stowable aircraft storage unit for providing additional storage in a cabin area of an aircraft includes a storage compartment, a vacuum lift mechanism, and a stowage container housing. The vacuum lift mechanism may include at least one vacuum actuator, and an air manifold in fluid communication with a vacuum source, the air manifold configured to provide vacuum and venting to the at least one vacuum actuator. The stowage container housing may be configured to receive the storage compartment in the stowed position and may be configured for mounting above a ceiling of the cabin area. The vacuum actuator may be mounted for lifting and lowering the storage compartment between the stowed position and a deployed position

Vacuum powered lifting mechanism

A method of installing an aircraft overhead stowage system includes installing a plurality of bin support rail fittings onto a plurality of bin support rails disposed above a ceiling of a cross-aisle galley complex; positioning a stowage compartment housing supported by a stowage support structure above the ceiling of the galley complex, the stowage compartment housing including a first stowage compartment and a second stowage compartment each movably engaged with and disposed inside the stowage compartment housing; aligning the stowage compartment housing and the stowage support structure with the bin support rails; and fastening the stowage support structure to the bin support rails using the bin support rail fittings such that the stowage compartment housing is structurally supported above the ceiling of the galley complex.

Drop down overhead galley stowage system

An aircraft overhead stowage system for a cross-aisle galley complex. The aircraft overhead stowage system includes a stowage compartment housing disposed above a ceiling of the galley complex that is supported above the ceiling by a stowage support structure. A first stowage compartment and a second stowage compartment are each movably engaged with and disposed inside the stowage compartment housing, and each stowage compartment is movable between a stowed position and a deployed position relative to the stowage compartment housing using a vacuum system. A vacuum generator that creates a vacuum force is mounted on the stowage compartment housing, and a plurality of vacuum bellows connected to each stowage compartment are in fluid communication with the vacuum generator. The vacuum system causes the stowage compartments to move between the stowed position and the deployed position. Vacuum-driven and manually-driven latching assemblies and removable extensions for each stowage compartment are also provided.

A combination lavatory and galley arrangement for aircraft includes a lavatory portion having adjacent inboard and outboard lavatories, and a galley portion, and can be located aft of aft aircraft aft doors, and can at least partially rearwardly extend into the aircraft's aft pressure dome. The inboard and outboard lavatories can be separated by a movable wall or partition to provide access for persons with restricted mobility, and can be provided in a modular housing to facilitate retrofit assembly within an aircraft. The movable wall can be an articulating movable lavatory partition movable between a first, linearly extended configuration and a second, folded configuration in a stowed position to provide entry for persons with restricted mobility.

Compact aircraft galley and lavatory arrangement and articulating lavatory partition for an aircraft

A vacuum powered system for moving a movable component, such as for raising and lowering a stowage container, includes a vacuum actuator connected between a fixed structure and a movable component. The vacuum actuator includes one or more intake ports that are configured to connect with a source of vacuum for moving the movable component in a first direction to a first position, and one or more bleed valve ports for venting the vacuum actuator to move the movable component in a second direction to a second position. The vacuum actuator may be an air bellows, a single acting linear vacuum actuator, or a dual acting linear vacuum actuator. A guiding system is further provided that includes elongated tracks in a stationary stowage container housing that houses the movable component, and corresponding guide elements on the movable component that slidably engage with the elongated tracks for moving the movable component.

A retractable flight attendant chair includes an anchor box, a sled coupled to the anchor box for horizontal translation of the retractable chair into and out of the stowage compartment, and a chair mounted on the sled. The chair includes an expanding/folding backrest and seat portion that allows the chair to be stowed in a small envelope compartment when not in use.

Stowable aircraft cabin attendant seat

A mountable cork puller including a tray open on one major side thereof adapted to be mounted in a recess in a wall, a hinge pin associated with the tray, and a hinge pivotally carried on the hinge pin, the hinge attached at its free end to a cork puller such that the hinge swings the cork puller between a stowed position in the tray and a deployed use position removed from the tray.

Mountable cork puller

A modular integrated galley in a passenger vehicle, including a mounting rack in the form of a vertical wall including upper, middle and lower storage areas, at least one storage slot extending laterally between the middle and lower storage areas for storing a work surface therein, and a latch for ejecting the work surface at least partially from the slot into a position for being further extended into a fully deployed position by a user. An elongate hinge that extends vertically along a mounted edge of the doors and is adapted for allowing the door to move 180 degrees of travel between its closed and open positions is also disclosed.

Growing community of inventors

Clinton, WA, United States of America

James Brian Hauser