General Electric Company

Thomas Michael Moors

Jon Conrad Schaeffer

Jianqiang Chen

Aaron Alpheus Yarbrough

Christopher Daniel Caruso

David Vincent Bucci

David A Williams

Surinder Singh Pabla

Michael Douglas Arnett

Amir Riahi

Arthur Samuel Peck

Joseph J Jackson

Vinod Kumar Pareek

Gabriel Della-Fera

Eric Michael Shain

Jane Marie Lipkin

Shannon B Geiger

The present disclosure is directed to pre-cured composites for use in manufacturing rotor blade components of a wind turbine. In one embodiment, the pre-cured composites are pultruded composites having a continuous base portion with a plurality of integral protrusions extending from the continuous base portion, and a fabric layer cured with the continuous base portion. Further, adjacent protrusions are separated by a gap.

Pre-cured composites for rotor blade components

A method of forming a component having an internal passage defined therein includes positioning a jacketed core with respect to a mold. The jacketed core includes a hollow structure formed from a first material, an inner core disposed within the hollow structure, and a core channel that extends from at least a first end of the inner core through at least a portion of inner core. The method also includes introducing a component material in a molten state into a cavity of the mold, such that the component material in the molten state at least partially absorbs the first material from the jacketed core within the cavity. The method further includes cooling the component material in the cavity to form the component. The inner core defines the internal passage within the component.

Method and assembly for forming components having internal passages using a jacketed core

Various embodiments include an infusion bolt and methods of manufacturing such a bolt. In one embodiment an infusion bolt includes: a head having an axially accessible opening extending therethrough; and a shaft extending from the head, the shaft having: an inner cavity fluidly connected with the axially accessible opening of the head; a radially outer surface surrounding the inner cavity; and a set of axially extending apertures along the radially outer surface, the set of axially extending apertures fluidly connected with the inner cavity and the axially accessible opening in the head.

Infusion bolt, method of use and method of manufacture

Embodiments of the present disclosure relate generally to systems and methods for manufacturing an airfoil component. The system can include: a geometrical mold; an elongated flexible sleeve having a closed-off interior and positioned within the geometrical mold, wherein the elongated flexible sleeve is further positioned to have a desired geometry; an infusing channel in fluid communication with the closed-off interior of the elongated flexible sleeve and configured to communicate a resinous material thereto; a vacuum channel in fluid communication with the closed-off interior of the elongated flexible sleeve and configured to vacuum seal the closed-off interior of the elongated flexible sleeve; and a glass fiber layer positioned within the closed-off interior of the elongated flexible sleeve.

System and method for manufacture of airfoil components

A rotatable engine component, coating and method of coating the rotatable component includes a substrate, a transitional zone applied to the substrate, and an abradable zone applied to the transitional zone. During operation of an engine in a turbine, the abradable zone is consumed upon contact with a static portion of the engine preventing damage to the rotatable component.

Rotatable component, coating and method of coating the rotatable component of an engine

A precipitation-hardened stainless steel alloy comprises, by weight: about 14.0 to about 16.0 percent chromium; about 6.0 to about 8.0 percent nickel; about 1.25 to about 1.75 percent copper; greater than about 1.5 to about 2.0 percent molybdenum; about 0.001 to about 0.025 percent carbon; niobium in an amount greater than about twenty times that of carbon; and the balance iron and incidental impurities. The alloy has an aged microstructure and an ultimate tensile strength of at least about 1100 MPa and a Charpy V-notch toughness of at least about 69 J. In one embodiment, the aged microstructure includes martensite and not more than about 10% reverted austenite. In another embodiment, the alloy includes substantially all martensite and substantially no reverted austenite. The alloy is useful for making turbine airfoils.

High corrosion resistance precipitation hardened martensitic stainless steel

A system for performing an in-situ polarization scan of a component surface includes a sensor connected to the component surface at a sensor connection, and the sensor generates a signal reflective of a current flow at the sensor connection. A power supply connected to the component surface at an electrical connection produces a voltage potential at the electrical connection. An electrolyte coats the sensor connection and the electrical connection. A method for performing an in-situ polarization scan of a component surface includes sensing a current flow on the component surface, generating a voltage potential on the component surface, and placing an electrolyte over at least a portion of the component surface.

System and method for performing a polarization scan in situ

A shaped rotor wheel, a turbo machine including the rotor wheel, and a method for producing the same are disclosed. In an embodiment, a rotor wheel is provided which includes at least one disk member and at least one spacer member, and is a capable of carrying and axially spacing one or more stages of blades. Also disclosed is a method for producing such a rotor wheel using metal powders as a starting material, and processing the metal powder using powder metallurgy techniques.

Shaped rotor wheel capable of carrying multiple blade stages

A precipitation-hardened stainless steel alloy comprises, by weight: about 14.0 to about 16.0 percent chromium; about 6.0 to about 7.0 percent nickel; about 1.25 to about 1.75 percent copper; about 0.5 to about 2.0 percent molybdenum; about 0.025 to about 0.05 percent carbon; niobium in an amount greater than about twenty times to about twenty-five times that of carbon; and the balance iron and incidental impurities. The alloy has an aged microstructure and an ultimate tensile strength of at least about 1100 MPa and a Charpy V-notch toughness of at least about 69 J. The aged microstructure includes martensite and not more than about 10% reverted austenite and is useful for making turbine airfoils.

A method for fabricating a turbine bucket and an apparatus facilitate reducing tip shroud creep. The method includes providing a turbine bucket that includes a tip shroud including at least one seal rail. The method also includes coupling at least one cutter tooth to the tip shroud, wherein the at least one cutter tooth is fabricated from an abradable material that enables the at least one cutter tooth to be removed from the tip shroud during operation of the turbine engine.

Growing community of inventors

Simpsonville, SC, United States of America

Thomas Michael Moors