The Boeing Company

Kenneth George Davis

Timothy Todd King

Matthew R Thomas

Jason W Mullins

Carl Aaron Davison

Mark J Nadvornick

Andrew Francis Szerlag

Edward W Gillette

Marius Ursescu

Andrew P Keleher

James R McCune

Cory Michael Hitchcock

Brett N Altmyer

Mitchel D Jacobs

Cynthia T Parrish

Christopher J Steele

Gil-Antonio Lora

Douglas R Ackerman

Adam Joseph Brockett

James R Mccune

A self-aligning structural attachment and a corresponding method are disclosed. The self-aligning structural attachment includes a main body having a proximal end and a distal end, wherein the main body is attached to (i) a CIP of a support system and (ii) a clevis on an airframe of an aircraft. Further, the self-aligning structural attachment includes a first attachment fitting disposed on the proximal end, wherein the first attachment fitting is a slide-and-swivel attachment fitting. Still further, the self-aligning structural attachment includes a second attachment fitting disposed on the distal end, wherein the second attachment fitting is a slide attachment fitting. Yet still further, the self-aligning structural attachment includes a pivoting hinge disposed between the first attachment fitting and the second attachment fitting.

Self-aligning structural attachment for crown integration panel (CIP)

Devices and methods to capture moisture at a structural member in a vehicle. The devices include a flexible tray that can snap-fit onto an exterior of the structural member. Once attached, the flexible tray can collect moisture from the structural member. A diverter is coupled to the flexible tray. The diverter diverts the collected moisture away from the structural member.

Devices and methods to capture moisture from a structural member

A system and method for exiting an overhead area in an aircraft. An egress apparatus is automatically moved from a closed state to an open state in response to opening a hatch that closes an opening in an overhead area in an aircraft. The apparatus comprises a platform attached to a substantially vertical structure by a first hinge structure. A guide panel is attached to the platform by a second hinge structure. The apparatus is configured to be moved from a closed state to an open state. The platform extends outward from the substantially vertical structure and under the opening in an overhead area in an aircraft when the apparatus is the open state. The guide panel extends upward from the platform when the apparatus is in the open state.

Platform and guide panel for aircraft cabin egress

A dual-bracketed support system and a corresponding method are disclosed. The dual-bracketed support system includes (i) a first bracket connected to a support structure for a crown portion of an aircraft, (ii) a second bracket, and (iii) a support rod having a proximal end and a distal end. The proximal end is connected to the first bracket and the distal end is connected to the second bracket. The second bracket is configured to allow the support rod to translate along a longitudinal axis defined by the support rod.

Crown raceway support (CRS) for crown integration panel (CIP)

A system for adjusting a height of a ceiling panel in an aircraft and a corresponding method is disclosed. The system includes an arm and at least one ceiling support latch, wherein each of the at least one ceiling support latches is attached to the arm. The system further includes an adjustable fitting attached to the arm, wherein the adjustable fitting includes (i) a first sliding block attached to the arm, (ii) a second sliding block attached to a support structure, and (iii) an adjustment screw. Adjustment of the adjustment screw forces the first and second sliding blocks to move relative to one another.

Adjustable support structure for aircraft cabin ceiling

A support system for a crown area of an aircraft and a corresponding method is disclosed. The support system includes a crown integration panel (CIP). The CIP is configured to provide a mounting surface for a plurality of aircraft equipment and to provide an electrical ground for at least one of the aircraft equipment of the plurality of aircraft equipment. The system further includes a first attachment and a second attachment attached to the CIP. The first attachment and the second attachment are configured to attach to an airframe of the aircraft. The system further includes a crown raceway support (CRS) having a first end and a second end, where the first end is attached to a first end of the CIP and the second end is configured to attach to an outboard rail of the aircraft.

Support system having a crown integration panel (CIP)

A system and method for exiting a crew rest area located in an overhead area in an aircraft. An opening in the crew rest area is located in an overhead area in the aircraft. An egress apparatus is configured to move between a closed state and an open state. The egress apparatus is configured to direct a person moving on the egress apparatus from the opening to a passenger cabin in the aircraft when the egress apparatus is in the open state.

Aircraft cabin egress

Growing community of inventors

Brier, WA, United States of America

Kenneth George Davis