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公开(公告)号:US20240270398A1
公开(公告)日:2024-08-15
申请号:US18441405
申请日:2024-02-14
Applicant: PRATT & WHITNEY CANADA CORP.
Inventor: Mert CEVIK , James Robert JARVO , Keith MORGAN , Elizabeth GIOIA
Abstract: A method of operating a hybrid engine for an aircraft, the hybrid engine having a thermal engine and an electric motor. The method includes verifying, using an engine control unit of the hybrid engine, that a selected power level is under a predetermined threshold for operation of the hybrid engine in a sub-idle hybrid mode. The method further includes operating the hybrid engine in the sub-idle hybrid mode, using the engine control unit, by controlling the thermal engine to operate in a standby mode, and by controlling the electric motor to operate in an active mode wherein the electric motor provides a majority of a propulsive power to the aircraft, wherein in the standby mode the thermal engine operates in a sub-idle condition to provide at most minimal propulsive power to the aircraft.
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公开(公告)号:US20220275831A1
公开(公告)日:2022-09-01
申请号:US17188249
申请日:2021-03-01
Applicant: PRATT & WHITNEY CANADA CORP.
Inventor: Mert CEVIK , Philip A. VARNEY , Robert J. MORRIS , David BEAMISH
IPC: F16C27/04 , F01D25/16 , F16F15/023
Abstract: A dual-film damper has a housing defining an annular damper fluidly connected to a source of pressurized oil. First and second damper rings are coaxially nested within the damper cavity. A first set of spacers allows for the formation of a first oil film annulus between the first and second damper rings. A second set of spacers allows for the formation of a second oil film annulus between the second damper ring and the housing. The first and second oil film annuli have a thickness-to-length ratio (T/L) selected to provide a desired damping capacity.
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