General Electric Company

General Electric Technology Gmbh

Donald Gordon Laing

Robert Allen Baten

Balakrishnan Ponnuraj

Vineet Sethi

Mehdi Milani Baladi

Ravinder Yerram

Jose Emmanuel Guillen

Kenneth Robert Austin

Raymond Kalok Fong

Gerardo Plata

Jorge Mario Rochin Machado

Eric Tracy Watson

Gerardo Plata Contreras

Charles Michael Booth

Przemyslaw Sebastian Drezek

Fernando Lopez-Parra

Ramune Auzelyte

Timothy Martin Christensen

Jose Francisco Estrada

Harish Chandra Dhingra

Oswaldo Alberto Sanchez

Yalid Mariluz Lopez Moctezuma

Stephen Matthew Biffle

A gas turbine system includes a plenum that includes an inlet and an outlet. The inlet is configured to receive a flow of oxidant and the outlet is configured to direct the flow of oxidant in a downstream direction. Additionally, a support system is coupled to the plenum and to a cone. The support system enables the cone to move along the support system from a first position to a second position. The cone includes an upstream end and the upstream end is removably coupled to the outlet of the plenum in the first position. When the cone is in the first position, the cone is configured to direct the flow of oxidant in the downstream direction to a gas turbine engine. The upstream end is disposed upstream of the outlet and is decoupled from the outlet when the cone is in the second position.

System for oxidant intake

A system includes a modularized air inlet system. The modularized air inlet system includes an air filter house section configured to receive air via an air inlet. The modularized air inlet system also includes a transition/silencer section configured to direct the air from the modularized air inlet system, via an air outlet, into an air inlet plenum coupled to a gas turbine engine enclosure. The modularized air inlet system is configured to couple directly to the air inlet plenum and the gas turbine enclosure without an expansion joint disposed between the modularized air inlet system and the air inlet plenum.

Compact gas turbine air inlet 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 diffuser removal tool for displacing an exhaust diffuser from a gas turbine engine is provided, which includes a pair of support arms, a clamp and wedge assembly coupled to an exhaust diffuser, and a lead screw assembly coupled between the support arms and to the clamp and wedge assembly via a wedge of the clamp and wedge assembly. The tool also includes a pair of linear bearing assemblies coupled to the support arms and to the clamp and wedge assembly via wedges of the clamp and wedge assembly. The lead screw assembly is configured to displace the diffuser in an axial direction relative to a longitudinal axis of the gas turbine engine while the linear bearing assemblies are configured to both enable the displacement of the diffuser in the axial direction while vertically supporting the diffuser to maintain alignment between the diffuser and the gas turbine engine.

Diffuser removal tool

A system includes a gas turbine engine and a multipurpose gas turbine engine support frame couple to the gas turbine engine. The multipurpose gas turbine support frame is configured to support the gas turbine engine during both operation and transport of the gas turbine engine.

Multipurpose support system for a gas turbine

The present application provides a radial diffuser exhaust system for use with a gas turbine engine. The radial diffuser exhaust system may include a radial diffuser positioned within an asymmetric exhaust collector. The asymmetric exhaust collector may include a closed end chamber and an exhaust end chamber. The closed end chamber may have a first size, the exhaust end chamber may have a second size, and the first size may be smaller than the second size.

Radial diffuser exhaust system

The present application provides an integrated bottoming cycle system for use with a gas turbine engine. The integrated bottoming cycle system described herein may include a compressor/pump, a cooling circuit downstream of the compressor/pump, a bottoming cycle heat exchanger, a heating circuit downstream of the bottoming cycle heat exchanger, and a number of turbine components in communication with the cooling circuit and/or the heating circuit to maximize the overall plant efficiency and economics.

Gas turbine engine with integrated bottoming cycle system

A system, including a superconductive heat transfer assembly, including, a first superconductive heat transfer pipe, a second superconductive heat transfer pipe, and a superconductive heat transfer contact switch configured to open and close a gap between the first superconductive heat transfer pipe and the second superconductive heat transfer pipe.

Superconductive heat transfer system

The present application provides a modular enclosure for use with an equipment platform and a turbo-machine. The modular enclosure may include a first number of walls attached to a number of legs of the equipment platform and a second number of walls attached to the legs of the equipment platform. The first number of walls may include a number of pivotable panels. The second number of walls may include an access aperture therein. The equipment platform may provide a roof for the modular enclosure.

Growing community of inventors

Houston, TX, United States of America

Donald Gordon Laing