Honeywell International Inc.

Eric Bridges

Mark C Morris

Jason Smoke

Cristopher Frost

Steven Whitaker

John McClintic

Joseph Yanof

Partha Das

Walter Lee Meacham

Christopher Zollars

Patrick Flynn

Raymond J Knorr

Alan Margolis

Scott J Marshall

Jennifer Battista

Victor Cabilan

Edward (Edd) M Brady

Carlos Enrique Murrieta

Jason Vizcaino

Gas turbine engines and methods for reducing spool thrust in a combustor section thereof are provided. The engines include an impeller, a shaft coupled to the impeller, an inner cavity downstream of the impeller, a thrust bearing assembly mechanically coupled to the shaft, a seal assembly having a seal land, and a controller. The controller is configured to detect a loss of oil event to the thrust bearing assembly and, in response, actuate the seal assembly to move the seal land toward a downstream face of the impeller to form a continuous axial seal about the inner cavity, vent gases from the inner cavity to decrease pressure therein to an extent less than an operating gas pressure thereof, and maintain the axial seal and the pressure within the inner cavity and thereby reduce the axial loads on the shaft.

Gas turbine engines and methods for reducing spool thrust in a combustor section thereof

Gas turbine engines and methods for reducing spool thrust in a turbine section thereof are provided. The engines include a turbine disk, a shaft coupled to the turbine disk, an inner cavity downstream of the turbine disk, a thrust bearing assembly mechanically coupled to the shaft, a seal assembly having a seal land, and a controller. The controller is configured to detect a loss of oil event to the thrust bearing assembly and, in response: actuate the seal assembly to move the seal land toward a downstream face of the turbine disk to form a continuous axial seal about the inner cavity, supply a pressurized gas to the inner cavity to increase pressure in therein to an extent greater than an operating pressure thereof, and maintain the axial seal and the pressure within the inner cavity and thereby reduce the axial loads on the shaft.

Gas turbine engines and methods for reducing spool thrust in a turbine section thereof

A fluid level sensor for sensing a level of a fluid within a toroid-shaped tank includes a float ring, a float structure, a gauge shaft, and a tiller arm. The float ring rotate s within the toroid-shaped tank about a first rotational axis. The float structure exhibits buoyancy in the fluid disposed within the toroid-shaped tank and supplies a force to the float ring based on the level of the fluid within the toroid-shaped tank. The gauge shaft is mounted for rotation about a second rotational axis and rotates about the second rotational axis to a position representative of the level of the fluid within the toroid-shaped tank. The tiller arm supplies the rotational drive force to the gauge shaft when the float ring rotates.

Fluid level sensor for a toroid-shaped tank

An anisotropic vibration isolation mounting assembly includes at least two three-parameter vibration isolators each having a first end configured for attachment to a rotating member assembly or a rotating member assembly housing and each having a second, opposing end configured for attachment to the rotating member assembly housing where the first end is configured for attachment to the rotating member assembly or to a system interface member where the first member is configured for attachment to the rotating member assembly housing. The at least two three-parameter vibration isolators are tuned anisotropically to minimize the transmission of vibrations during operation of the rotating machine.

Three parameter damper anisotropic vibration isolation mounting assembly

A compact removal feature comprises a plurality of recesses, such as radius slots, on an inner diameter (ID) of a bearing inner ring. The removal tool can engage the removal feature and remove the entire bearing assembly without damage to the parts. The placement of the removal feature on the bearing inner ring ID allows for a reduction in inner ring length (and weight) while maintaining bearing assembly integrity.

Removal tool and method of removing a bearing assembly

A bearing assembly comprising a centrifugal debris trap for removing contamination debris from lubrication fluid prior to lubrication of the bearing assembly components is provided. The centrifugal debris trap comprises an annular groove on an inner race such that with sufficient centrifugal force, contamination debris in the lubrication oil is forced into the groove and held there. Removal of contamination debris from the lubrication oil prevents damage to bearing balls and races of the bearing assembly, thus reducing bearing fatigue. A method for lubricating bearing assembly components using the bearing assembly of the present invention is also provided.

Preloaded duplex ball bearing design

A centrifugal debris trap includes a cylindrical chamber bound by an inner surface of a continuous wall radially disposed about a center axis at a first inner diameter, and having a first wall end and a second wall end; and a plurality of grooves between the first and second wall ends, extending radially outward from the inner surface into a portion of the continuous wall, and each having a groove outer diameter that is greater than the first inner diameter. The cylindrical chamber is sealed at the first wall end by a back plate attached about a circumference of the first wall ends, and is open at the second wall end through a ring attached thereto about a circumference of the second wall end. The ring has a ring opening radially disposed about the center axis, and a second inner diameter less than the first inner diameter.

Multi-stage centrifugal debris trap

A shaft coupling is made from carbon-carbon composite to achieve significantly higher temperature capability, combined with lubricity and high strength, allowing its use in hot, non-lubricated sections of gas turbine engines, where previously, these couplings could not be used. The coupler may be cylindrical for joining the facing ends of co-axial shafts is made from carbon-carbon composite with a female spline in a coupling bore and a male spline on the coupling outer surface. Variations of the torque carrying geometry include involute splines, circular splines, square drive, hex drives, serrations, or double-D drives. By fabricating the coupler from carbon-carbon (or carbon-graphite) composite, metallic shaft mating splines are provided with a coupler that has exceptionally high temperature capabilities (>2500 F.), high strength, and can be impregnated with graphite or other dry lubricants to reduce frictional heat generation and reduce spline wear. The useful temperature limit of the coupler may preferably exceed that of the mating shaft ends.

Oil-less shaft coupling utilizing carbon-carbon composite and method of fabrication thereof

A touchdown bearing and actuator ring assembly for selectively biasing a ball bearing into direct engagement with a rotating shaft subject to significant axial thrust forces. The Actuator ring assembly includes a pair of relatively rotatable ring members abutting the bearing assembly. Confronting faces of the ring members include protuberances. As the ring members undergo relative rotation, the protuberances come into alignment, wedging-apart the ring members and biasing the bearing assembly into contact with the rotating shaft. A disengagement actuator selectively rotates the ring members in the opposite direction until the protuberances are out of alignment, allowing a restraining spring to bias the bearing assembly away from the rotating shaft. The present invention provides an assembly capable of quickly and repeatedly engaging and disengaging the touchdown bearing with the rotating shaft, using a minimum of envelop space and weight.

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Tempe, AZ, United States of America

Eric Bridges