The Boeing Company

Lutron Electronics Company, Inc.

Benjamin A Johnson

James Patrick Irwin

David William Minteer

Erik W Dowell

Michael E Rorabaugh

John Thomas Axtell

Daniel Curtis Raneri

Brian Michael Courtney

Justin J Mierta

Robert E Fisher

Lawrence R Carmen, Jr

Eddie Kwon

Peter Apolonio Coronado

Matthew Anthony Dilligan

Christopher Lance Newbolt

Christopher L Newbolt

Rebecca Elizabeth Ahern

Lawrence R Carmen

Peter A Coronado

(nee Ahern) Ludwig

Rebecca Elizabeth Ludwig

Robert E Fischer

A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. In one illustrative embodiment, an apparatus includes a transport member. The transport member is configured for use in the fluid transport system. The transport member includes a material configured to reduce voltages and currents, induced in response to an electromagnetic event, along the transport member.

Composite tubes for a fluid transport system

A hydraulic joint is disclosed. The hydraulic joint includes a tube, a hydraulic fitting, and a tip seal. The hydraulic fitting may be positioned around the tube. The hydraulic fitting may include a first open end for receiving the tube. The tip seal may be configured to define an opening that allows for the passage of leaks. The tip seal may be positioned on the hydraulic fitting adjacent the open end and forming a mechanical barrier between the fitting and the tube.

Apparatus for preventing spark propagation

A bulkhead fitting assembly that includes a tube, a mounting flange attachable to a bulkhead, a thermal shell joining the mounting flange and the tube and having a portion spaced away from the tube forming an air pocket between the tube and the thermal shell, a plurality of mounting studs extending from the mounting flange away from the thermal shell, and a plurality of bushings positioned between the mounting studs and the bulkhead. The plurality of bushings are each shaped to complete a current path from the tube to the plurality of mounting studs, from the plurality of mounting studs to the plurality of bushings, and from the plurality of bushings to the bulkhead. Nuts are threaded on the studs to secure the fitting assembly by sandwiching the bulkhead between the mounting flange and the bushings, which are retained by the nuts.

Bulkhead fitting assembly

A method of sealing an opening in a bulkhead with a fitting assembly having a tube, a mounting flange, a thermal shell, an adapter, a bushing, and a jam nut may include inserting the tube through the opening; placing the mounting flange against the bulkhead, the mounting flange attached to the thermal shell, the thermal shell attached to the tube, and the mounting flange attached to the adapter so that the adapter extends away from the mounting flange and from the thermal shell through the opening; forming an air pocket by spacing a portion of the thermal shell away from the tube; placing the bushing on the adapter; and tightening the jam nut on the adapter to sandwich the bulkhead between the mounting flange and the bushing to form a seal between the mounting flange and the bushing to seal the opening.

Bulkhead fitting assembly and method of sealing a bulkhead opening

A method of making a bulkhead fitting assembly may include joining a tube to a thermal shell of a mounting flange, the mounting flange shaped to be attached to a bulkhead and including an adapter; forming the thermal shell to have a portion spaced away from the tube to form an air pocket between the tube and the thermal shell adjacent the mounting flange; and placing a bushing on the adapter such that the bushing completes a current path from the tube to the adapter, from the adapter to the bushing, and from the bushing to the bulkhead.

Bulkhead fitting assembly and method of making

A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. The aerospace vehicle is operated. The fluid transport system in the aerospace vehicle is comprised of materials selected such that the fluid transport system has an electrical configuration. The intensity of the electrical discharge that occurs within the fluid transport system during operation of the aerospace vehicle is reduced to within selected tolerances by the electrical configuration of the fluid transport system.

Fluid transport system for preventing electrical discharge

A method for directing electrical current to prevent sparking from the interaction between a composite structure and lightning or static electrical charge, the method including the steps of forming a hole in a composite structure; and positioning a bushing into the hole to create an interference fit between the bushing and the composite structure, wherein the bushing is formed of a material that has a coefficient of thermal expansion close to the coefficient of thermal expansion of the composite structure and the bushing provides an electrical path between a fastener disposed in the bushing and the composite structure.

Thin wall bushing for robust electrical bonding to fiber-reinforced structures

A bulkhead fitting assembly may include a tube, a mounting flange, and a thermal shell joining the mounting flange and the tube; the thermal shell may consist of a thin barrier and form an air gap between the tube and the mounting flange.

An axially swaged fitting for use in permanently coupling tubes together. The swaged fitting may be useful in coupling metal hydraulic lines to one another in an airplane. According to one embodiment, the swaged fitting includes a sleeve with a hard metal surface and a swaging ring with a soft metal surface, such that during the swaging process the soft metal surface of the swaging ring is deformed.

Axially swaged fitting

Described herein is a novel method and apparatus for preventing spark propagation from a hydraulic joint to a surrounding medium, such as a fuel source. The hydraulic joint includes a fitting and a tube. A tip seal may be placed about the edge of the hydraulic fitting or a sleeve may be placed about the joint, each resulting in an independent mechanical barrier between the joint and surrounding medium, thereby preventing spark propagation to the surrounding medium.

A method for improving conductance on hydraulic fittings by incorporating a soft metal interlayer between the fitting and a hydraulic tube, wherein the soft metal interlayer is located in an area where the fitting engages the hydraulic tube upon swaging or installation under pressure.

Growing community of inventors

Lynnwood, WA, United States of America

Benjamin A Johnson