General Electric Company

Aaron Todd Williams

Robert Patrick Tameo

Michael Anthony Thomas

Charles Eric Lavender

Mark Issac Snyder

So Young Kim

Robert John Parks

Michael Eric Figard

John Lawrence Noon

Alexander Kaber Carroll

Jennifer Ruth Cooper

Sundar Murugappan

Mark Michael D'Andrea

Thomas Michael Regan

Courtney L Albers

Marcus Joseph Ottaviano

Christopher Scott Sensing

Samuel Levulis

Nathan Tyler Woods

Jeffrey Robert Winters

A dynamic human machine interface system includes a mission commander application (MCA) unit including a control processor, the MCA active on one vehicle of a plurality of mission member vehicles, the MCA unit in communication with a data store, the control processor accessing executable instructions that cause the control processor to direct operations of components of the MCA unit, an alternate scenario evaluation unit accessing at least one of mission parameter records and flight member data records in the data store to recalculate mission parameters, a dynamic video interface unit to render the recalculated mission parameters on a mission control dashboard (MCD), the MCD presented to the mission commander on a display unit of the one vehicle, the MCD including a plurality of display pane areas selectable by a user interaction with an interactive interface, and each display area configurable by the user interaction to change content of the display pane.

Decision support system for air missioncommander dynamic mission re-planning

A balance weight for a turbine rotor includes: a block-like centerbody; a pair of resilient spring arms extending laterally from opposite sides of the centerbody, the centerbody and the spring arms collectively defining an arcuate shape; at least one locating structure extending from a radially outer surface of the balance weight; and a limit tab extending radially inward from a distal end of each of the spring arms.

Trapped spring balance weight and rotor assembly

A balance weight for a turbine rotor includes: (a) a block-like centerbody; (b) a pair of resilient spring arms extending laterally from opposite sides of the centerbody, the centerbody and the spring arms collectively defining an arcuate shape; and (c) at least one locating structure extending from a radially outer surface of the balance weight.

A gas turbine engine centrifugal compressor axial forward thrust apparatus bleeds impeller tip aft bleed flow from between an annular centrifugal compressor impeller of a high pressure rotor and a diffuser directly downstream of the impeller. The apparatus then uses the aft bleed flow to pressurize an annular cavity extending radially between an inner combustor casing and the rotor and extending axially between forward and aft thrust balance seals. Forward and aft thrust balance lands are in sealing engagement with the forward and aft thrust balance seals on the high pressure rotor respectively. An annular stator plenum in fluid communication with the annular cavity is bounded in part by a forward end wall having conical diffusion holes therethrough which may be axially or circumferentially or axially and circumferentially angled. The forward thrust balance seal may be on an aft conical arm of the impeller.

Centrifugal compressor forward thrust and turbine cooling apparatus

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West Chester, OH, United States of America

Aaron Todd Williams