General Electric Company

Ge Infrastructure Technology, LLC

Jordan Scott Warton

Jorge Mario Rochin Machado

Michael Anthony Acosta

Miroslaw Pawel Babiuch

Ashish Agrawal

Robert Allen Baten

Gerardo Plata Contreras

David Garza-Maldonado

Frank Ociel Meza Koslowski

George Frederick Frey

Richard Michael Watkins

Tuy C Huynh

Paul Roberts Scarboro

Jorge Mario Rochin-Machado

A system includes a modular exhaust collector configured to be arranged in a first orientation or a second orientation. The modular exhaust collector is configured to receive an exhaust flow along an inlet axis, to direct the exhaust flow along a first direction through an outlet when in the first orientation, and to direct the exhaust flow along a second direction through the outlet when in the second orientation. The modular exhaust collector includes an exhaust passage to receive the exhaust flow, a plurality of compressor discharge (CD) ports, a plurality of flow ports, a bottom face opposite the outlet with a first drain, and a first side wall with a second drain between the bottom face and the outlet. Each CD port is disposed a first radial distance from the inlet axis, and each flow port is disposed a second radial distance from the inlet axis.

Turbine exhaust collector

A system includes an air cooling system having a heat exchanger, a fan, and a mount. The heat exchanger includes an inlet, an outlet, and a heat exchange conduit between the inlet and the outlet. The inlet is configured to couple to a bleed system of a gas turbine system to extract a bleed flow. The heat exchanger is configured to cool the bleed flow along the heat exchange conduit in a surrounding air to produce a cooled bleed flow. The outlet is configured to couple to a fuel purge system of the gas turbine system to supply the cooled bleed flow as a fuel purge flow. The fan is configured to force an airflow from the surrounding air through the heat exchanger. The mount is configured to mount the air cooling system outside of an enclosure surrounding the gas turbine system.

System and method for air cooling fuel purge flow

A system includes an exhaust collector tunnel () configured to mount inside an exhaust collector () of a gas turbine (). The exhaust collector tunnel () has a tunnel wall () configured to extend around a turbine shaft () of the gas turbine (). The tunnel wall () has a variable diameter () along at least a portion of a length of the exhaust collector tunnel ().

Exhaust collector conversion system and method

A system includes a bleed system configured to direct a bleed flow from a compressor section to an exhaust section of a gas turbine engine. The bleed system includes a first bleed conduit section configured to couple to the compressor section, a second bleed conduit section configured to couple to the exhaust section, and a first rotatable joint coupling together adjacent conduits of the first and second bleed conduit sections. The second bleed conduit section has components configured to rotate between a plurality of configurations relative to the first bleed conduit section and the compressor section via the first rotatable joint. The plurality of orientations corresponds to a plurality of exhaust outlet orientations of the exhaust section, and the components of the second bleed conduit section are the same in each orientation.

System and method for reconfiguring a bleed system

A system () includes a modular exhaust collector () configured to be arranged in a first orientation () or a second orientation (). The modular exhaust collector () is configured to receive an exhaust flow along an inlet axis (), to direct the exhaust flow along a first direction () through an outlet () when in the first orientation (), and to direct the exhaust flow along a second direction () through the outlet () when in the second orientation (). The modular exhaust collector () includes an exhaust passage () to receive the exhaust flow, a plurality of compressor discharge (CD) ports (), a plurality of flow ports (), a bottom face () opposite the outlet () with a first drain (), and a first side wall () with a second drain () between the bottom face () and the outlet (). Each CD port () is disposed a first radial distance () from the inlet axis (), and each flow port () is disposed a second radial distance () from the inlet axis ().

A restraint assembly includes a plurality of tensile restraints and a plurality of restraints. Each tensile restraint of the plurality of tensile restraints is configured to couple to a respective anchor plate of a plurality of anchor plates disposed on one or more foundations, and a mobile system. The mobile system is disposed on the one or more foundations. Each restraint includes a rigid element configured to couple to a respective anchor plate of the plurality of anchor plates, and to interface with or couple to a respective location on the mobile system.

Mobile power generation restraint assembly

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.

Growing community of inventors

Pasadena, TX, United States of America

Jordan Scott Warton