Unison Industries, Inc.

Dattu Gv Jonnalagadda

Gordon Tajiri

Yanzhe Yang

Emily Marie Phelps

Michael Thomas Kenworthy

Joseph Richard Schmitt

Merin Sebastian

Sandeep Kumar

Jason Levi Burdette

Shiloh Montegomery Meyers

Sharad Pundlik Patil

Karthick Vilapakkam Gourishankar

Derek Thomas Dreischarf

Lakshmi Krishnan

Daniel Dyer

Nagendra Baddam

Bruce Patrick Graham

Walter Arthur Hundley

Armando Bringas

Mark Phillip Drake

Jason L Burdette

Elizabeth Turner

An air turbine starter that includes a housing defining an interior having a primary air flow path. A rotatable turbine member located in the interior includes a plurality of circumferentially spaced blades that extend into the primary air flow path. A containment assembly couples to the housing and circumscribes at least a portion of the plurality of circumferentially spaced blades. The containment assembly includes a tube and a laminate.

Air turbine starter with containment assembly

An electroforming system and method for electroforming a component includes an electroforming reservoir with a housing with at least one inlet and at least one outlet, and at least one anode chamber within the housing and fluidly coupled to the at least one inlet. An anode can be located within the at least one anode chamber.

Electroforming system and method

An electroforming system and method for electroforming a component includes an electroforming reservoir with a housing defining a fluid passage. An electroforming chamber can be located within the housing and fluidly coupled to the fluid passage via a set of apertures in at least one wall of the electroforming chamber.

A flexible joint assembly for a joint between a first duct and a second duct for providing a flow of fluid, such as bleed air in an aviation implementation. The flexible joint includes a bellows supported by a mounting assembly having a first support and a second support, each surrounding a portion of the bellows. A set of flexures provided on a joint ring of the joint assemblies can operably couple the first support and the second support.

Gimbaled flexure for spherical flex joints

A nickel-cobalt material and method of forming includes forming a doped nickel-cobalt precursor material. The method also includes heat treating the doped nickel-cobalt precursor material, wherein the heat treating includes at least heating within a temperature zone below the onset temperature for grain growth in the doped nickel-cobalt precursor material.

Nickel-cobalt material and method of forming

An apparatus and method of forming a heat exchanger including a thermally compliant material and geometry with a core having a first set of flow passages and a second set of flow passages passing through the core. A first manifold of high temperature and strength material defines a fluid inlet for the first set of flow passages and a second manifold of high temperature and strength material defines a fluid inlet for the second set of flow passages. At least one of the first and second manifolds can include an in-situ compliant portion to provide for compliance during thermal expansion of the heat exchanger.

Heat exchanger assembly

A duct for a turbine engine, such as a gas turbine engine, can be utilized to carry a fluid from one portion of the engine to another. The duct can include a metallic tubular element having one of a varying wall thickness, a varying cross section, or a tight bend. Such a duct can be formed utilizing additive manufacturing or metal deposition on an additively manufactured mandrel.

Turbine engine duct

A tunable compliant mount structure for an engine such as a turbine engine can include a fluid conduit coupled to a fan casing by a connector. At a junction between the connector and the fluid conduit, a compliant mount structure can provide compliance and can be tuned to operate under variable stresses at the junction. The compliant mount structure can include a set of nested convolutions to provide compliance. The geometry of the convolutions can be used to tune the compliance, stiffness, or directionality. The tunable compliant attachment structure provides for additive in-situ manufacturing at the fluid conduit.

Tunable compliant attachment structure

A valve and a heat exchanger apparatus for a gas turbine engine include a valve body having a valve seat and an actuation component including a plate formed from a set of metal layers and responsive to a change in at least one of a thermal condition and a pressure exerted thereon such that the plate moves and the valve moves between an opened and a closed position where a portion of the plate engages with the valve seat.

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Ponnur, India

Dattu Gv Jonnalagadda