The Boeing Company

United States of America As Represented by the Administrator of Nasa

Marcus Anthony Belcher

John W Connell

Sayata Ghose

Christopher J Wohl, Jr

John W Hopkins

Richard Allen Miller, Ii

Peter J Van Voast

Thomas Karl Tsotsis

Kay Youngdahl Blohowiak

Michael Walter Evens

Megan Nicole Watson

Benjamin Jeffrey Stephenson

Joel Patrick Baldwin

John C Osborne

Mark Albrecht

Richard John Loftis

Timothy J Luchini

Kieran Patrick Davis

Daniel R Ferriell

Stephen Howard Williams

Kristofer Logan Peterson

Collin William Childs

Edwin John Smith

Robert N Jaeger

Benjamin David Walker

Jonathan William Udell

Sara Jane Lynn

Doria Pei

Mirza Mustafayev

Varun Suri

Ignas Sabet-Kazilas

Daniel Richard Ferriell

Richard Allen Ii Miller

Richard Allen Miller

An aircraft includes external structures, and one or more thermal emitters integrated with one or more of the external structures. The one or more thermal emitters are configured to generate heat to deice the one or more external structures. The one or more thermal emitters are configured to receive electrical power from one or more of an auxiliary power unit of the aircraft, a power distribution system of the aircraft, one or more engines of the aircraft, or an external power cart that is separate and distinct from the aircraft.

Systems and methods for deicing aircraft

A method of forming a reinforced panel may include engaging a reinforcement component having a faying surface with a first portion of a heated press, engaging an uncured panel component with an opposing second portion of the press, the panel component having a faying surface complementarily-configured with respect to the faying surface of the reinforcement component, treating the faying surface of the reinforcement component such that the faying surface is active for co-bonding with respect to the panel component, actuating the press to direct the first and second portions of the press toward each other, such that the faying surfaces are complementarily engaged under pressure; and heating the first and second portions of the press to a curing temperature associated with the panel component to substantially simultaneously co-bond the faying surfaces of the reinforcement component and the panel component together, cure the panel component, and form the reinforced panel.

Method of forming a reinforced panel component

Compositions including a polyamide, and compaction rollers for an automated fiber placement machine incorporating the composition are provided. The polyamide may be a reaction product of at least one diamine and an aromatic dicarboxylic acid, a hydroxy benzoic acid, or their respective ester or acyl halide derivatives. The at least one diamine may include an amino terminated perfluorinated alkyl ether polymer or oligomer. The composition may have a thermal conductivity of from about 0.2 to about 50 Watts per meter Kelvin (WmK).

Polyamide compositions and articles incorporating the same

Compositions including a polyimide and one or more thermally conductive fillers, and compaction rollers for an automated fiber placement machine incorporating the compositions are provided. The polyimide may be a polymeric reaction product of a dianhydride and one or more diamines. The one or more diamines may include a fluorine-containing alkyl ether diamine. The one or more thermally conductive fillers may include one or more of a carbon-based filler, boron nitride, a metal, or combinations thereof. The compositions may have a thermal conductivity of from about 0.2 to about 50 Watts per meter Kelvin (WmK).

Polyimide compositions and articles incorporating the same

Compositions including a poly(arylene ether), and compaction rollers for an automated fiber placement machine incorporating the composition are provided. The poly(arylene ether) may be a reaction product of at least one disubstituted benzophenone and at least one polyol. The at least one polyol may include at least one fluorinated diol. The composition may have a thermal conductivity of from about 0.2 to about 50 Watts per meter Kelvin (WmK).

Poly(arylene ether) compositions and articles incorporating the same

A method for plasma treating a surface of a first substrate is disclosed. The method may comprise generating a plasma flume using a plasma treatment device having a nozzle. The plasma flume may emanate through a flume aperture of the nozzle at an emanation angle of about 5 degrees or less. The emanation angle may be defined as an angle between a central axis of the nozzle and a central axis of the flume aperture. The method may further comprise plasma treating the surface of the first substrate with the plasma flume by scanning the plasma flume over the surface of the first substrate. The first substrate may be one of a consolidated thermoplastic material and a cured thermoset material.

Method for plasma treating substrates and for bonding plasma treated substrates

The present disclosure is generally directed to a primer saturated carrier medium assembly including a carrier medium having a front face and an opposing rear face, a primer saturating the carrier medium between the front face and the opposing rear face, and removable film impenetrable to the primer covering opposite faces of the carrier medium. A method of applying primer to a surface includes applying a face of a primer saturated carrier medium to contact a surface, and curing the primer saturated carrier medium on the surface. A structure includes a primer saturated medium including a carrier medium having a front face and an opposing rear face, and a primer saturating the carrier medium between the front face and the opposing rear face. The structure further includes a surface adhered to the primer on one face of the primer saturated medium.

Primer saturated carrier medium assembly and method of applying to a surface

A system for treating a surface and applying adhesive to an already treated portion of the surface concurrently is presented. The system comprises surface treatment equipment, adhesive application equipment, and a common feed system. The surface treatment equipment is configured to treat the surface of an elongated member. The adhesive application equipment is configured to apply adhesive to the already treated portion of the surface. The common feed system feeds the elongated member beneath the surface treatment equipment and the adhesive application equipment concurrently.

Common feed system for surface treatment and adhesive application

Surface energy of a substrate is changed without the need for any template, mask, or additional coating medium applied to the substrate. At least one beam of energy directly ablates a substrate surface to form a predefined topographical pattern at the surface. Each beam of energy has a width of approximately 25 micrometers and an energy of approximately 1-500 microJoules. Features in the topographical pattern have a width of approximately 1-500 micrometers and a height of approximately 1.4-100 micrometers.

Modification of surface energy via direct laser ablative surface patterning

A method for preparing a pre-bond surface of a composite structure includes the steps of: (1) separating a peel ply, co-cured with a composite substrate, from the composite substrate; and (2) transferring an identifiable marking agent from the peel ply to the composite substrate upon separation of the peel ply from the composite substrate. Residue of the peel ply, transferred from the peel ply to the composite substrate upon separation of the peel ply from the composite substrate, is layered on the identifiable marking agent.

Composite structure and method for inspecting a pre-bond surface of a composite structure

A gas containment apparatus for use with an end effector including at least one plasma head includes at least one enclosing structure coupled to the end effector. The enclosing structure is configured to capture a gas produced by the at least one plasma head. The gas containment apparatus also includes a duct coupled to the at least one enclosing structure and configured to channel the gas from within the enclosing structure.

Ventilation systems for use with a plasma treatment system

Adhesion testing systems, methods of fabrication, and methods of testing are disclosed. Test systems include test coupons with non-metallic test adherends. Test coupons are configured to test bonds to the non-metallic test adherends under peeling stress and/or shearing stress. Test methods are simplified and rapid as compared to standard adhesion tests and include methods of accelerated environmental testing. Test methods also are adapted for qualitative and quantitative measurement of bond performance.

Methods and systems for rapidly testing adhesion

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Sammamish, WA, United States of America

Marcus Anthony Belcher