Drop down overhead galley stowage system

Patent metadata

Field	Value
Publication number	US-10207806-B2
Application number	US-201815987351-A
Country	US
Kind code	B2
Filing date	May 23, 2018
Priority date	Jul 2, 2015
Publication date	Feb 19, 2019
Grant date	Feb 19, 2019

Abstract

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.

First claim

What is claimed is:

1. A method of installing an aircraft overhead stowage system for a cross-aisle galley complex, the method comprising:
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, each stowage compartment movable between a stowed position and a deployed position relative to the stowage compartment housing;
aligning the stowage compartment housing and the stowage support structure with the bin support rails;
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;
installing a control panel in a selected location accessible to a cabin crew member and electrically connecting the control pan& to a vacuum system mounted on the stowage compartment housing, wherein the control panel is configured to activate the vacuum system to move one of the first stowage compartment and the second stowage compartment between the stowed position and the deployed position; and
installing a galley ceiling system on the ceiling of the galley complex, comprising:
installing a first ceiling panel on the ceiling of the galley complex below the stowage compartment housing, the first ceiling panel including attached ceiling-mounted flex hoses for connecting to a ventilation duct and to an air passageway disposed above the ceiling of the galley complex;
attaching aircraft side systems interfaces to a center ceiling systems panel the aircraft side systems interfaces including a vent plenum, a gasper nozzle, and emergency lighting;
installing the center ceiling systems panel with attached aircraft side systems interfaces into the ceiling of the galley complex below the stowage compartment housing and adjacent to the first ceiling panel; and
installing a second ceiling panel on the ceiling of the galley complex below the stowage compartment housing and adjacent to the center ceiling systems panel opposite the first ceiling panel.

2. The method of claim 1 , wherein the step of installing the galley ceiling system further comprises: attaching a plurality of interface duct plenums to a bin support rail; connecting a first galley venting hose and a first gasper hose to the interface duct plenums; connecting the first galley venting hose to the ventilation duct, and connecting the first gasper hose to the air passageway; and further attaching a plurality of ceiling mounted flex hoses including a second galley venting hose and a second gasper hose integrated on the first ceiling panel to the interface duct plenums, connecting the second galley venting hose to the vent plenum, and connecting the second gasper hose to the gasper nozzle.

3. The method of claim 1 , further comprising removing previously existing galley cross-aisle ceiling and systems elements from the ceiling of the galley complex.

4. A method for operating an aircraft overhead stowage system for a cross-aisle galley complex, method comprising:
generating a vacuum force through a vacuum bellows connected to a stowage compartment so as to move the stowage compartment into a stowed position within a housing;
engaging a latch pin with a locking strike to prevent the stowage compartment from moving into a deployed position, wherein the latch pin and locking strike are part of a latch strike assembly that includes a pressure piston;
releasing the vacuum force from the vacuum bellows to allow the vacuum bellows to expand; and
generating a vacuum force to the pressure piston to disengage the locking strike from the latch pin to allow the stowage compartment to move into the deployed position.

5. The method of claim 4 , further comprising transmitting an electrical signal to a activate bypass valve to prevent the vacuum force from reaching the vacuum bellows.

Assignees

• Be Aerospace Inc

Inventors

• Claflin Shawn A
• Papke Robert
• Hauser James B
• Mckee Jefferey

Classifications

• B64D47/02

  Arrangements or adaptations of signal or lighting devices · CPC title

• E05C1/085

  With means for assisting depression of the latch bolt during latching · CPC title

• E05C9/10

  Actuating mechanisms for bars {(E05C9/02 - E05C9/06 take precedence)} · CPC title

• F04B45/0536 Primary

  the actuating fluid being controlled by one or more valves · CPC title

• B64D11/04

  Galleys · CPC title