General Electric Company

White Consolidated Industries, Inc.

William Andrew Parker

Sivaraman Vedhagiri

Gerald Wilson Grove

Mark David D'Ambruoso

David Martin Johnson

Roger C Walker

Gregory Allan Crum

Joseph Leonard Moroso

Eric David Roush

Dwight Eric Davidson

Jesse Edwin Trout

Philip Michael Caruso

Robert Lester Brooks

Yang Liu

Ravi Meenaksh

Eric Scicchitano

Michael John Barno

Stephen Chiaco

A gas turbine engine is provided comprising a compressor with an insulated cooling circuit. The compressor comprises a compressor casing having a compression chamber and at least one stator and at least one rotor disposed in the compression chamber, the at least one stator comprising a stator body having a plurality of tubes for transporting cooling air through passages in the stator body into the compression chamber. The plurality of tubes are surrounded by an air gap for insulating the tubes from the stator body.

Gas turbine engine with insulated cooling circuit

A system for providing air from a multi-stage to a turbine includes a turbine having a high pressure input port and a low pressure input port. The system also includes a compressor having at least one high pressure extraction air output and at least one low pressure extraction air output. A valve is fluidly connected to the at least one high pressure extraction air output, at least one low pressure extraction air output and low pressure input port of the turbine. The valve is selectively operated to fluidly connect the at least one low pressure extraction air output with the low pressure input port during normal operating conditions and fluidly connect the at least one high pressure extraction air output and the low pressure input port during a turn down condition or below design temperature operation to enhance turbine engine performance.

System for delivering air from a multi-stage compressor to a turbine portion of a gas turbine engine

A system for regulating a cooling fluid within a turbomachine. The system may include a plurality of bypass chambers, wherein each of the plurality of bypass chambers allows for the cooling fluid to pass from the compressor section to the at least one wheelspace area. The system may also include a plurality of bypass plugs, wherein each of the plurality of bypass plugs is insertable into a bypass chamber opening on each of the plurality of bypass chambers.

System for regulating a cooling fluid within a turbomachine

A method to ventilate a rotary machine housed in a compartment having a ventilation air inlet and air exhaust, a variable speed ventilation fan and a temperature sensor, wherein the method includes: sensing a temperature level of the rotary machine; applying the sensed machine temperature level to a controller for the fan; drawing ventilation flow through the compartment and over the machine; determining whether the sensed machine temperature level is above a desired temperature level of the rotary machine, wherein the desired temperature level is determined by the controller, and the controller setting an operational condition of the fan to increase the ventilation flow through the compartment if the sensed machine temperature level is above the desired temperature level.

Turbine compartment ventilation control system and method using variable speed fan

A method for detecting a fuel leak in a compartment is provided. The compartment includes at least one inlet and an exhaust outlet that is coupled in flow communication with the compartment and in flow communication with a fan. The method includes determining a fan speed, measuring a fuel leak gas concentration value, determining a fuel leak gas concentration limit value within the compartment based on the determined fan speed, comparing the measured fuel leak gas concentration value with the determined fuel leak gas concentration limit value, and generating at least one of an alarm signal and a trip signal based on the comparison.

Methods and systems for detecting gas turbine engine fuel leaks

A hermetically sealed motor compressor comprising a housing enclosing a motor stator and rotor. A vertically oriented crankshaft is connected at one end to the rotor and has an offset crankshaft journal at its other end. An oil passage is provided in the journal and an oil pick-up tube has a first straight end projecting into an oil sump. The second straight end portion is axially aligned with the rotation axis of the crankshaft. A helically twisted insert is provided in the second straight end portion and the first and second portions are connected by an S-shaped intermediate portion.

Compressor oil pick-up tube

Growing community of inventors

Greenville, SC, United States of America

William Andrew Parker