Robert N Papke

US Patent:

20120074258, Mar 29, 2012

Filed:

Sep 21, 2011

Appl. No.:

13/239294

Inventors:

ROBERT PAPKE - CAMANO ISLAND WA, US
ANDREW J. LUNDBERG - STANWOOD WA, US
WILLIAM J. BANFIELD - LAKE STEVENS WA, US

Assignee:

BE INTELLECTUAL PROPERTY, INC. - WELLINGTON FL

International Classification:

B64D 11/00

US Classification:

2441185

Abstract:

An integrated aircraft interior module includes one or more ceiling panels, sidewall linings, decompression ventilation provisions, and overhead stowage compartments including cabin air distribution ducting, personal service units. The sidewall linings, overhead stowage compartments and other interior structure integrated items attach to existing aircraft structural provisions.

US Patent:

20110233333, Sep 29, 2011

Filed:

Dec 9, 2010

Appl. No.:

12/964059

Inventors:

Robert PAPKE - Camano Island WA, US

Assignee:

BE INTELLECTUAL PROPERTY, INC - Wellington FL

International Classification:

B64D 11/00

US Classification:

2441186

Abstract:

An aircraft crew rest station includes an overhead crew rest portion including a central deck portion, forward and aft bunk portions, and a central entry vestibule connected between a passenger seating area and the central deck portion. The forward and aft bunk portions include a plurality of adjacent partitioned individual sleeping berths configured in interfitting alternating trapezoid shapes to optimize spatial accommodation of body proportions of crew members in the available aircraft space. The central deck portion includes an emergency escape hatch, a fold-down jump seat, and a fold-down entry door that removably covers a stairway of the central entry vestibule.

US Patent:

20180265200, Sep 20, 2018

Filed:

May 23, 2018

Appl. No.:

15/987351

Inventors:

- Wellington FL, US
Robert Papke - Camano Island WA, US
James B. Hauser - Mukilteo WA, US
Jefferey McKee - Duvall WA, US

International Classification:

B64D 11/00
B64D 11/04
F04B 45/053
E05C 1/08
B64D 47/02
E05C 9/10

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.

US Patent:

20170001726, Jan 5, 2017

Filed:

Jun 23, 2016

Appl. No.:

15/191326

Inventors:

- Wellington FL, US
Robert Papke - Camano Island WA, US
James B. Hauser - Mukilteo WA, US
Jefferey McKee - Duvall WA, US

International Classification:

B64D 11/00
F04B 45/053
E05C 1/08
E05C 9/10
B64D 11/04
B64D 47/02

Abstract:

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.

US Patent:

20160272321, Sep 22, 2016

Filed:

May 26, 2016

Appl. No.:

15/166173

Inventors:

- Wellington FL, US
Jefferey McKee - Duvall WA, US
Wade Johnson - Edmonds WA, US
James Brian Hauser - Mukilteo WA, US
Robert Papke - Camano Island WA, US
David R. Benton - Edmonds WA, US
Frank E. Hashberger - Snohomish WA, US

International Classification:

B64D 11/02
B64D 11/04

Abstract:

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.

US Patent:

20140224930, Aug 14, 2014

Filed:

Feb 7, 2014

Appl. No.:

14/175537

Inventors:

- Wellington FL, US
Jefferey McKee - Duvall WA, US
Wade Johnson - Edmonds WA, US
James Brian Hauser - Mukilteo WA, US
Robert Papke - Camano Island WA, US
David R. Benton - Edmonds WA, US
Frank E. Hashberger - Snohomish WA, US

Assignee:

B/E Aerospace, Inc. - Wellington FL

International Classification:

B64D 11/02
B64D 11/04

US Classification:

2441185

Abstract:

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.