Stephen L Scown

7059565, Jun 13, 2006

Aug 26, 2004

10/927606

Stephen L. Scown - Seattle WA, US
Gregory A. Tubbs - Seattle WA, US
Cory M. Hitchcock - Seattle WA, US

The Boeing Company - Seattle WA

B64C 1/06

244117R, 244119, 244131, 2961467, 29614615, 52544

Aircraft frames having multiple bracket mounting holes, corresponding brackets, and associated methods are disclosed. An aircraft frame member in accordance with one embodiment of the invention includes multiple sets of mounting holes, each set having one or more mounting holes. Brackets in accordance with an embodiment of the invention can be attached to either of at least two of the sets of mounting holes, for example, using snap fit attachment devices or other attachment devices. Each bracket can support one or more components (e. g. , insulation, wiring, ECS ducting) relative to the aircraft frame member. The bracket can also span between two or more aircraft frame members. Each bracket can be installed in any of a variety of positions without the use of tools and can support any of a variety of devices. Accordingly, the time and cost associated with manufacturing, inventorying, installing and repositioning the brackets and the devices they support can be reduced.

7128295, Oct 31, 2006

Jan 7, 2005

10/905502

Stephen L. Scown - Edmonds WA, US

The Boeing Company - Chicago IL

B64D 11/00

2441181, 2441185, 16266

A pivot assembly is provided including a first pivot boss having an engagement extension and a first race element having a central race socket. A central engagement bushing is rotatably secured within the central race socket and includes an engagement chamber adapted to removably engage the engagement extension. The central engagement bushing allows the first race element to rotate relative to the first pivot boss while remaining longitudinally engaged to the first fixed pivot boss.

7497638, Mar 3, 2009

Nov 9, 2006

11/595286

Gregory A. Tubbs - Marysville WA, US
Stephen L. Scown - Edmonds WA, US

The Boeing Company - Chicago IL

F16C 11/00

403 76, 403240, 403263, 403353, 2441181, 244131

An apparatus, system, and method includes a socket having a substantially spherical inner contour being accessible via an opening. A member having a partial spherical shape substantially similar to the spherical inner contour. A cross-sectional profile of the member is adapted to pass through the opening into the socket and to remain uncoupled with the socket when the socket and the member are in a first relative orientation. The member is further adapted to couple with the socket when the member is in the socket and in a second relative orientation with the socket.

7527402, May 5, 2009

Nov 13, 2006

11/559010

Stephen L. Scown - Edmonds WA, US
David A. Young - Bellingham WA, US

The Boeing Company - Chicago IL

B60Q 1/00

362480, 362 96, 362523, 362234

An integrated reading light and personal air outlet for a passenger service unit (PSU) employs a housing carried in the PSU with an air nozzle mounted within the housing and a light ring of light emitting diodes mounted to the housing surrounding the air nozzle. The housing is swivels in the PSU for orientation of a primary axis for directing a light beam from the LED light ring and the air nozzle separately swivels within the housing for orientation of a secondary axis for directing airflow from the nozzle.

8177163, May 15, 2012

Feb 24, 2009

12/391880

Paul J. Wilcynski - Seattle WA, US
Jeffrey R. Nix - Stanwood WA, US
Stephen L. Scown - Edmonds WA, US
Mostafa Ghoreishi - Bellevue WA, US
Anthony E. Anderson - Snohomish WA, US

The Boeing Company - Chicago IL

B64D 11/00

2441185

The disclosure provides for an aircraft video control station. In an embodiment, the aircraft video control station comprises a wall mounted control panel, a desktop, a seat that is stowed when not in use, and a cabinet that contains the wall mounted control panel, the desktop, and the seat. The cabinet may have a depth in the range of about 10 inches to about 37 inches, and preferably has a depth of 15 inches. The seat may be in the form of a swing out seat.

8262022, Sep 11, 2012

Dec 15, 2009

12/638878

David A. Young - Bellingham WA, US
Stephen L. Scown - Edmonds WA, US

The Boeing Company - Chicago IL

B64D 11/00

2441185, 2441181, 312246

An ergonomically improved stowage system includes a supporting structure, a bin having a volume with an opening to receive a load, the bin being movable with respect to the supporting structure from a closed to an open position, and an attaching mechanism for attaching the bin to the structure. The attaching mechanism includes a bin pivot axis that is located in substantial alignment with a center of gravity of the bin in the closed position.

20140077033, Mar 20, 2014

Sep 17, 2012

13/621462

Stephen Lee Scown - Edmonds WA, US
Paul Joseph Wilcynski - Seattle WA, US
Jeffrey Nix - Stanwood WA, US
Marc Anton Spane - Camano Island WA, US

THE BOEING COMPANY - Chicago IL

B64D 11/02
E06B 11/00
A47K 4/00

2441185, 49 70, 49506

A method and apparatus operating a moveable partition. The moveable partition is configured for use with a first lavatory and a second lavatory. The moveable partition is further configured to separate the first lavatory and the second lavatory into separate spaces within a fixed perimeter for the first lavatory and the second lavatory when the moveable partition is in a first configuration. The moveable partition is further configured to define a single space within the fixed perimeter when the moveable partition is in a second configuration. The moveable partition is connected to a door for the first lavatory in the second configuration.

6883753, Apr 26, 2005

Mar 25, 2004

10/708791

Stephen L. Scown - Edmonds WA, US

The Boeing Company - Chicago IL

B64C001/06

2441181

A monument support system () for an aircraft () includes multiple aircraft frame elements (″). An adapter bridge () is coupled to the aircraft frame elements (″) and has multiple attachment points (″). A coupling member () is coupled to the adapter bridge (). A monument () is coupled to the frame elements (″) via the adapter bridge () and the coupling member ().