Solar Turbines Inc.

Caterpillar Inc.

Roy Thomas Collins

Marco Ezra Leon

Jonathan Bendert

Fabrice Mario Murgia

Thompson Hoang An Pham

Neal Watkins

Cody Wayne Allen

Paul F Cameron

Anthony James Grichnik

Michael Seskin

Chad Holcomb

Robert Eleazar Mendoza

Ricardo Montes

Louis James Bertsch, Iv

Saliha Kenyon Lacoursiere

Steven Howard DeMoss

Julien Doumecq-Lacoste

Marco Perez

A system for monitoring a health of one or more seals includes a flow control valve, and a controller. The flow control valve is located upstream of the seal and disposed in fluid communication therewith. The flow control valve is configured to maintain a pre-determined fluid pressure between the flow control valve and the seal. The controller is communicably coupled to the flow control valve. The controller is configured to receive a position of the flow control valve, and determine the health of the seal based on the received position of the flow control valve.

System for monitoring health of a seal

A method for calibrating a fuel control valve assembly including a valve and an actuator is disclosed. The method includes determining an encoder offset by actuating the valve until a predetermined value for the effective flow area is measured to obtain an actual calibration encoder count and comparing the actual calibration encoder count to an initial calibration encoder count. The method also includes adjusting an alignment encoder count and a maximum encoder count by an amount of the encoder offset. The method further includes associating the adjusted alignment encoder count with an alignment command value and the adjusted maximum encoder count with a maximum command value.

Actuator to valve calibration of a fuel control valve assembly

Display screen or portion thereof with icon

A method for controlling a gas turbine engine fuel control valve during low flow conditions includes positioning the fuel control valve in an operating position. The method also includes determining a fuel control valve flow sensor flow rate while in the operating position and determining a corrected effective flow area ('Cda') of the fuel control valve. The method further includes generating Cda versus command data with the corrected Cda and the operating position and inserting the generated Cda versus command data into the nominal Cda versus command data set when nominal Cda versus command data is not known at the operating position.

Low flow correction for gas turbine engine fuel valve characteristics

A method of operating a drive system for a load is disclosed. The drive system may have an electric motor/generator and a gas turbine engine. The engine may have a combustor, and main and pilot flow paths via which fuel is supplied to the combustor. The engine may be operable in low and standard emissions modes. A proportion of the fuel that is supplied to the combustor via the pilot flow path may be greater in the standard emissions mode than in the low emissions mode. The method may include determining an engine power requirement of the load, and whether the engine power requirement of the load is sufficiently large to operate the engine in the low emissions mode. Additionally, the method may include operating the electric motor/generator if the engine power requirement of the load is not sufficiently large to operate the engine in the low emissions mode.

Hybrid gas turbine engine&#x2014;electric motor/generator drive system

A method is provided for a control system. The method may include obtaining data records associated one or more input variables and one or more output parameters, and selecting one or more input parameters from the one or more input variables. The method may also include generating a computational model indicative of interrelationships between the one or more input parameters and the one or more output parameters based on the data records, and determining desired respective statistical distributions of the one or more input parameters of the computational model.

Control system and method

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San Diego, CA, United States of America

Roy Thomas Collins