General Electric Company

General Electric Technology Gmbh

Robert Allen Baten

Kenneth Robert Austin

Vineet Sethi

Donald Gordon Laing

Jose Emmanuel Guillen

Raymond Kalok Fong

Harley Matthew Ross

Jordan Scott Warton

Raymond Ka Lok Fong

David Joseph Drobniak

Tho Vankhanh Nguyen

Richard Michael Watkins

Eric Tracy Watson

Douglas Alan Jones

Gerardo Plata Contreras

Artemio Josue Aguilar

Mario Oscar Ramirez

Doyle Jackson Marrs

Victor Gerardo Cabal Velarde

Jingmei Zhang

Jesus Elios Almendarez Mendez

Jesus Ellios Almendarez Mendez

A system includes a docking guide comprising a first alignment guide configured to couple with a first mobile unit that supports a turbine engine and a second alignment guide configured to couple with a second mobile unit that supports a generator. The first and second alignment guides are configured to guide a coupling between the first and second mobile units to help align the turbine engine with the generator.

Systems and methods for a turbine trailer mechanical docking and alignment system

A system a first mobile body configured to support a turbine engine and an auxiliary skid communicatively and fluidly coupled to the turbine engine. The auxiliary skid includes one or more interconnects configured to support a turbine engine component. The system also includes a second mobile body configured to support a generator. The first and second mobile bodies are configured to align a removable coupling between the turbine engine and the generator.

Systems and methods for a mobile power plant with improved mobility and reduced trailer count

A system includes a first mobile body configured to support a turbine engine and an air intake section coupled to the turbine engine. The system also includes a second mobile body configured to support a generator. The first and second mobile bodies are configured to guide a removable coupling between the turbine engine and the generator. The system also includes a third mobile body configured to support one or more partially assembled components associated with the turbine engine and the generator.

A system includes a load moving machine, including a frame and a movable assembly coupled to the frame. The movable assembly includes a lift portion, a rotational portion, a first translational portion, and a second translational portion.

System and method for lifting with load moving machine

A turbine ventilation system includes at least one fan configured to provide a first air flow into a gas turbine enclosure, a fan bypass configured to circumvent the at least one fan to provide a second air flow into the gas turbine enclosure, and an eductor configured to draw the first or second air flows through and out of the gas turbine enclosure.

System for ventilating a gas turbine enclosure

An air inlet silencer for turbomachines is provided. In one embodiment, the air inlet silencer includes a body, and a plurality of concentric baffles coupled to and axially surrounding the body. In another embodiment, an air inlet system for a turbomachine includes the air inlet silencer, as discussed herein, positioned within a silencer housing. The air inlet system may also include a deflector positioned within the silencer housing adjacent the air inlet silencer. In a further embodiment, a turbomachine includes a turbine coupled to a compressor, and an air inlet system, as described herein, coupled to the compressor.

Air inlet silencer for turbomachines

A system for packaging a gas turbine includes an enclosure peripherally surrounding and extending along a length of the gas turbine. The enclosure comprises first and second ends with a passage between the enclosure and the gas turbine. The system further includes means for connecting the first and second ends to an air filtration system and an exhaust system, respectively. A plurality of supports are connected to and extend radially inward from the enclosure with means for connecting the plurality of supports to the gas turbine. A method for packaging a gas turbine includes connecting the gas turbine to a plurality of supports and connecting the plurality of supports to an enclosure peripherally surrounding and extending along a length of the gas turbine. The method further includes connecting first and second ends to an air filtration system and an exhaust system, respectively.

System and method for packaging and transporting a gas turbine

A system includes an anti-icing heat recovery system, which includes a first heat exchanger, a second heat exchanger, and a variable speed fan. The first heat exchanger is configured to receive a working fluid from an exhaust section of a gas turbine engine and to transfer heat from the working fluid to a cooled intermediate heat transfer medium to generate a heated intermediate heat transfer medium. The second heat exchanger is configured to receive the heated intermediate heat transfer medium from the first heat exchanger and to transfer heat from the heated intermediate heat transfer medium to air entering the gas turbine engine. The variable speed fan is configured to urge the working fluid from the exhaust section of the gas turbine engine through the first heat exchanger.

System and method for heat recovery in a gas turbine engine

A system includes a turbomachine skid including a skid body configured to support a turbomachine and a modular transportation system. The modular transportation system includes one or more supports and one or more transportation attachments that may be removably coupled to the supports, the transportation attachments being interchangeable with one or more different transportation attachments.

System for transporting turbomachinery

A system includes a turbomachine platform including a first docking guide. The turbomachine platform supports a turbomachine skid, and the skid includes a second docking guide. The first docking guide is configured to interface with the second docking guide in order to guide the turbomachine skid between a docked position and an undocked position relative to other equipment supported by the platform.

System for aligning turbomachinery

A mount assembly for securing a machine base to a foundation including: a first block secured to the machine base; a second block secured to the foundation wherein the first and second blocks are configured for mating engagement that permits adjustment of the machine base relative to the first block and to the foundation along any of three mutually perpendicular axes.

Three axis adjustable mounting system

Methods and devices for separating oil from a mixture of oil and air are provided. In various embodiments, an air/oil separator includes a cylindrical housing that creates a circular flow path of the air and oil. Further, the air/oil separator may include various flow guides that improve the air/oil separation properties of the separator. Other embodiments include a turbine engine with a lubrication system that includes the improved air/oil separator.

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Baytown, TX, United States of America

Robert Allen Baten