The Boeing Company

Other

The Boeing Corporation

James Patrick Irwin

Benjamin A Johnson

Robert E Fisher

Eddie Kwon

Arthur C Day

Andrew Michael Robb

Jason Philip Bommer

Robert E Fischer

David William Minteer

Erik W Dowell

Michael E Rorabaugh

Nathan Michael Kelley

John Thomas Axtell

Christopher Michael Hansom

Arvid J Berg

Carl Roy McIver

Kevin Earl McCrary

David Cohen

Peter Apolonio Coronado

Dennis Michael Lewis

Kevin O'Brien Gaw

Donald K Dabelstein

Matthew Anthony Dilligan

Wayne L Cooper

Christopher Lance Newbolt

Diego A Velasco

Dennis M Lewis

Christopher L Newbolt

(nee Ahern) Ludwig

Carl R Mciver

Peter A Coronado

Rebecca Elizabeth Ludwig

Kevin Mccrary

Rebecca Elizabeth Ahern

Kevin O'brien Gaw

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 rigid coupler for use in electrically isolating an electrically conductive fluid conveyance system is described. The rigid coupler includes a nonconductive liner having a first end configured to couple to a first adjoining section of the fluid conveyance system, and a second end, opposite said first end, configured to couple to a second adjoining section of the fluid conveyance system. A reinforcing structure circumscribes the nonconductive liner and is coupled to a portion of the nonconductive liner extending between the first and second ends of the nonconductive liner. The reinforcing structure includes a multi-axial braided fiber material impregnated with a matrix material. A fiber overwrap is hoop wound about at a least a portion of the reinforcing structure between the first and second ends of the nonconductive liner.

Static dissipative fluid conveying coupler and methods of assembling the same

A fuel line assembly for an aircraft comprises a ferrule assembly comprising a ferrule affixed to an isolation tube, which may be directly affixed to a fuel tube or affixed to an extension tube, which in turn, is affixed to the fuel tube. The ferrule assembly provides electrostatic discharge protection and lightning protection as the isolation tube maintains a separation distance from the ferrule and fuel tube, both of which are made from metal. The isolation tube is made from a dielectric material, but which may have conductive particles added to aid in the dissipation of an electrostatic charge. The electrical resistance through the isolation tube has a lower limit to arrest the flow of the induced lightning current through the assembly. The amount of lightning protection afforded can be configured. The ferrule assembly components may be affixed by using thermo-welding, adhesive, or mechanical pressure.

Method of installing fuel lines in an aircraft

An electrically conductive structural connection employs a pass through or fastener having a first diameter. A fastener hole, with a second diameter larger than the diameter of the pass through, extends through a thickness of a structure and receives the pass through. A bushing having a diameter and a thickness to fit between the first and second diameters extends though and past the thickness of said structure. When the feedthrough is compressively secured to the structure, the bushing expands radially between the first diameter and the second diameter to maintain at least one contact point between the fastener and the structure.

Electrically conductive bushing connection to structure for current path

A highly resistive wire includes a non-metallic wire material having a resistance of at least ten kilo-ohms per meter. In one embodiment, the wire material can be fashioned from a carbon-loaded plastic material, having an inclusion of carbon particles in a quantity that yields a resistance of no less than 10 kilo-ohms per meter. In another embodiment, the wire can include a plurality of strands of wire material where each of the strands is surrounded by a thin layer of conductive or semi-conductive material. The highly resistive wire can be used as a single strand, or as a bundle of strands, as wiring in a structure prone to transient electrical or electromagnetic events, such as static discharge or lightning strikes, that might otherwise lead to damage of the structure.

Highly resistive wiring for inherent safety from electromagnetic threats

Electrostatic discharge protected ferrule

A method and apparatus for conducting an electrical current between a first transport member and a second transport member. In one illustrative embodiment, a coupling assembly comprises a first fitting associated with a first end of a first transport member, a second fitting associated with a second end of a second transport member, and a seal. The seal is configured for placement around the first fitting and the second fitting when the first end of the first transport member is positioned relative to the second end of the second transport member. The seal is further configured to seal an interface between the first transport member and the second transport member. The seal is comprised of a material configured such that the seal has a level of conductivity within a selected range and such that a conductive pathway is formed between the first transport member and the second transport member.

Conductive coupling assembly

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.

Growing community of inventors

Renton, WA, United States of America

James Patrick Irwin