General Electric Company

Haley Marie Boyd

Jason Dean Fuller

Nicholas Demianovich

Robert Joseph Loeven, Ii

Daniel Alvin Kleewein

Logan Rose

Robert Joseph Loeven Ii

A gas turbine engine that includes a stage of guide vanes, a compressor downstream from the stage of guide vanes, and a combustor downstream from the compressor. The combustor includes a primary combustion zone and a secondary combustion zone downstream from the primary combustion zone. The primary combustion zone includes an exit configured to channel combustion gases towards the secondary combustion zone. A controller is communicatively coupled with the stage of guide vanes, the controller configured to monitor a temperature at the exit of the primary combustion zone, and selectively open and close the guide vanes to maintain the temperature within a predefined temperature range.

Gas turbine engine and methods of controlling emissions therefrom

Techniques for moving a component of an imaging system are described herein. The techniques may include an apparatus having a component bracket to attach to an imaging system component disposed within a gantry of the imaging system. The apparatus may include a platform bracket to attach to a movable platform of the imaging system, wherein the component bracket and the platform bracket are to be coupled to each other.

Moving a component of an imaging system

Growing community of inventors

Greer, SC, United States of America

Haley Marie Boyd