General Electric Company

Mra Systems, Inc.

General Electric Company Polska Sp. Z O.o.

Other

Wendy Wenling Lin

Robert William Davidoff

Steven Sebastian Burdgick

Trevor Howard Wood

David Patrick Calder

Michael Moses Martinez

Rudramuni Kariveerappa Majjigi

David Herman

Nicholas Joseph Kray

Kishore Ramakrishnan

Nikolai N Pastouchenko

Graham Frank Howarth

Timothy Richard DePuy

Christophe Lanaud

Aaron Goldsholl

Shanmugam Murugappan

Arthur William Sibbach

Andrew Michael Roach

Elzbieta Kryj-Kos

Adegboyega Masud Makinde

Guy Wayne DeLeonardo

Piotr Jerzy Kulinski

Aaron Todd Sellinger

Patrick Keene Clements

Ruolong Ma

Pawel Adam Lewicki

Daniel R Olson

David William Crall

Kenneth Paul Zarnoch

Scott Roger Finn

Todd Alan Anderson

Danian Zheng

Herbert S Chao

Stefaan Guido Van Nieuwenhove

Douglas Duane Ward

Richard David Cedar

Kevin Joseph Barb

Shatil Sinha

Viswanadha Gupta Sakala

Egbert Geertsema

Scott Michael Miller

Lawrence Donald Willey

Charles Richard Evans

Rainer Koeniger

Raghuveer Chinta

George T Seeger

Grama Narasimhaprasad Praveen

Amitabh Bansal

Mohamad Sultan

Derek D Black

Stephen G Grupinski

Lara Liou

Jason Testa

Rachel Marie Suffield

Joseph T Begovich, Jr

Nathan R Woodward

Casey Lauren Berschback

Hannah Rice James

Laura Liou

Damain Hendrix

Alexander Joseph Vallee

Nathan Woodward

An acoustic core may include an array of resonant cells configured as a plurality of resonant cell groups. The resonant cell groups may include a plurality of resonant cells configured as a partitioned resonant cell that include a converging resonant cell and a diverging resonant cell. The converging resonant cell and the diverging resonant cell may be defined by a plurality of cell walls integrally formed with one another and a partition integrally formed with the plurality of cell walls. The partition may at least partially delimit the converging resonant cell from the diverging resonant cell. The converging resonant cell may define an upper resonant space delimited by the partition and a top face of the array of resonant cells. The diverging resonant cell may define a lower resonant space delimited by the partition and a bottom face of the array of resonant cells.

Tools and methods for forming acoustic cores

A system and method for bonding together a facesheet and an acoustic screen of an acoustic liner using a solid adhesive film having a first adhesive side opposite a second adhesive side are provided. The system includes a solid adhesive film having a first adhesive side opposite a second adhesive side; an acoustic screen bonded to the first adhesive side of the solid adhesive film; and a facesheet bonded to the second adhesive side of the solid adhesive film. The method includes bonding the facesheet to the first adhesive side of the solid adhesive film and bonding the acoustic screen to the second adhesive side of the solid adhesive film.

Solid adhesive film for acoustic liner and method

A method of electroforming an airfoil comprising an airfoil body. The method comprising electroforming a metal edge shell over a filler, located at a leading edge of the airfoil body, and over the airfoil body. The filler can be encapsulated within the metal edge shell and the metal edge shell has a sculpted leading edge defining a non-linear pattern.

Engine airfoil metal edge

Acoustic cores and tools and methods for forming the same

An acoustic liner is provided. The acoustic liner includes a face sheet, a back sheet spaced from the face sheet, and a core layer defining a cellular structure disposed between the face sheet and the back sheet. The core layer includes a plurality of first resonant cells coupled to the back sheet. Each of the first resonant cells includes a first cell wall coupled to the back sheet along a first cell wall base edge, the first cell wall extending from the back sheet toward the face sheet, the first cell wall further coupled to the face sheet along a first cell wall top edge, wherein the first cell wall of each of the first resonant cells comprises a surface extension that extends from a surface of the first cell wall.

Continuous degree of freedom acoustic cores

An acoustic core has a plurality of cell walls formed of an additive-manufacturing material and a resonant space defined by the plurality of cell walls. At least some of the resonant cells have sound-attenuating protuberances formed of an excess amount of the additive-manufacturing material having been intentionally introduced to the cell walls and protruding into the resonant space with a semi-random orientation and/or size.

Acoustic cores with sound-attenuating protuberances

A coated component having a composite substrate and a coating system disposed thereon is provided. The coating system is substantially non-porous such that hydrocarbon fuel or other carbonaceous fluids are prevented from contacting and impregnating the polymer matrix composite material. The coating system can include an aluminum layer or a film layer comprising a polyethylene film or a polypropylene film. Also provided is a composite fan casing for a gas turbine engine having a polymer matrix composite substrate and a coating system disposed thereon. Methods for forming a containment assembly of a gas turbine engine are provided.

Composite component with oil barrier coating

An airfoil for a gas turbine engine defining a spanwise direction, a root end, a tip end, a leading edge end, and trailing edge end is provided. The airfoil includes: a body extending along the spanwise direction between the root end and the tip end, the body formed of a composite material; and a sculpted leading edge member attached to the body positioned at the leading edge end of the airfoil, the sculped leading edge member formed at least in part of a metal material and defining a non-linear patterned leading edge of the airfoil.

An acoustic core includes an array of resonant cells. The array may include a plurality of coupled resonant cells respectively defining an antecedent resonant space and a subsequent resonant space, with at least one cell wall having one or more wall-apertures defining a pathway between the antecedent resonant space and the subsequent resonant space. The array may include a plurality of high-frequency resonant cells respectively defining a high-frequency resonant space and being matched with respective ones of the plurality of coupled resonant cells. A cross-sectional dimension of the one or more wall-apertures defining the pathway between the antecedent resonant space and the subsequent resonant space may be less than a cross-sectional dimension of the antecedent resonant space and/or a cross-sectional dimension of the subsequent resonant space. The array may include a plurality of partitioned resonant cells that have a partition integrally formed with at least one of a corresponding one or more cell walls and transecting the corresponding resonant space with at least one surface of the partition having an interface angle that is oblique or perpendicular relative to a plane parallel to a top face and/or a bottom face of the array of resonant cells.

Acoustic liners with low-frequency sound wave attenuating features

A system and method for separating a layer from a layer assembly when the layer assembly includes a backing layer and a material layer. The system includes an automated machine having a controller and an end effector. A separating tool is attached to the end effector of the automated machine. The separating tool includes a displacing member, with an outer face, configured to establish a void between the backing layer and the material layer by displacing a portion of the backing layer. The separating layer also includes a securing member configured to establish a mechanical connection with a displaced portion of the backing layer.

Systems and methods of automated film removal

An acoustic liner may include an acoustic core having an array of resonant cells, and an acoustic screen disposed across the array of resonant cells. The resonant cells include a plurality of cell walls and a resonant space defined by the plurality of cell walls. The acoustic core may include a folded acoustic core. Additionally, or in the alternative, at least some of the resonant cells may include an oblique polyhedral cellular structure and/or a multitude of sound-attenuating protuberances. The acoustic screen may include a reticulate membrane and a support lattice.

Acoustic liners with enhanced acoustic absorption and reduced drag characteristics

Methods for manufacturing composite components having complex geometries are provided. In one exemplary aspect, a method includes laying up each of a plurality of laminates to an initial shape with a substantially planar geometry or a gently curved geometry. Then, a laid up laminate is formed to a final shape for each predefined section defined by the composite component to be manufactured. Thereafter, the laminates formed to their respective final shapes are stacked to build up the complex geometry of the composite component. Next, the composite component can be cured and finish machined as necessary to form the completed composite component.

Methods for manufacturing composite components

An acoustic liner and a method of attenuating noise are provided. The acoustic liner includes a face sheet, a back sheet spaced from the face sheet, and a core layer extending between the face sheet and the back sheet. The core layer includes a plurality of resonant cells, each resonant cell including at least one cell wall coupled to the back sheet along a cell wall base edge. The at least one cell wall extends from the back sheet at an angle toward the face sheet. The at least one cell wall further coupled to the face sheet along a cell wall top edge. The resonant cell is formed in a predetermined shape and contains a volume in a space defined by the at least one cell wall, the back sheet, and the face sheet. The cell wall base edge length is greater than the cell wall top edge length.

A method of making a 3D tube and the 3D tube made thereby. The method comprises: inserting a deflated pre-formed bladder into the 3D tube; and inflating the pre-formed bladder to deform the 3D tube and make the 3D tube have a substantially similar shape as that of the pre-formed bladder inflated.

Method of making 3D tube and 3D tube made thereby

Containment assemblies and methods for forming containment assemblies of gas turbine engines are provided. For example, a containment assembly comprises a containment case including a plurality of coated fibers. Each coated fiber comprises a fiber surrounded by a ceramic material such that the ceramic material coats the fiber. As another example, a containment assembly comprises an inner case and a containment case comprising a plurality of coated fibers. Each coated fiber comprises a fiber surrounded by a ceramic material such that the ceramic material coats the fiber. The containment case includes a greater proportion of the coated fibers at an inner surface of a layer of the containment case than at a location within the containment case that is radially outward from the inner surface. Methods for forming a containment assembly of a gas turbine engine are provided.

Containment case having ceramic coated fibers

Growing community of inventors

Montgomery, OH, United States of America

Wendy Wenling Lin