F16H57/046

OIL BAFFLE FOR GAS TURBINE FAN DRIVE GEAR SYSTEM
20200284336 · 2020-09-10 ·

A method of assembling an epicyclic gear train includes providing a unitary carrier that includes spaced apart walls and circumferentially spaced mounts interconnecting the walls, spaced apart apertures provided between the mounts at an outer circumference of the carrier, gear pockets provided between the walls and mounts extending to the apertures, and a central opening in at least one of the walls, inserting an intermediate gear through the central opening and moving the intermediate gear radially into the gear pocket to extend through the aperture, inserting a baffle into the carrier, and inserting a sun gear through the central opening to intermesh with the intermediate gear.

Gearing device with at least one structural component that rotates with respect to a housing appliance

A gear device with a housing and a structural component rotatably mounted at the housing by a bearing that delimits a housing interior space. The gear device has a hydraulic fluid supply line for supplying hydraulic fluid into the interior space. A gap provides sealing between the housing and structural component. The gap is arranged radially between the housing and a further rotatable structural component or between a further housing and the structural component. A further bearing rotatably mounts the further structural component in the area of the housing or rotatably mounts the structural component at the further housing. An appliance couples the further structural component to the structural component or couples the housing to the further housing, and facilitates a relative movement between the further structural component and the structural component or between the housing and the further housing in the axial and/or radial directions.

Transmission
20200191253 · 2020-06-18 ·

A dual clutch transmission (1) includes a breather assembly (7) with a breather element (9). The breather element (9) includes at least one entry opening (24) facing a transmission interior and an outwardly facing exit opening (40). The breather assembly (7) also includes at least one oil collection element (8) arranged between the breather element (9) and an oil spray source (6).

Gear drive for air driven vehicles

A transmission (14) for connecting a propeller (15) to an engine (13) having a drive shaft (2), comprising: a first gear (3) driven by the drive shaft (2) in a first rotational direction; an idler gear (4) driven by the first gear; a third gear (5) driven by the idler gear (4); and an output shaft (6) driven by the third gear in the first rotational direction.

GEARBOX WITH INTEGRATED SUBMERSIBLE LUBRICANT PUMP
20200141482 · 2020-05-07 ·

A gear box includes a casing having an interior. A rotating component is arranged in the interior of the casing. A bearing including a rotating element, and a fixed element is connected with the casing in the interior. A submersible pump is arranged in the interior of the casing. The submersible pump includes a first housing portion extending about the rotating component fixedly mounted to the casing at the interior. A second housing portion is fixedly mounted to the casing at the interior and is aligned with the first housing portion. The first and second housing portions form a lubricant reservoir which holds lubricant. An impeller is mounted to the rotating component and arranged in the lubricant reservoir. One of the first and second housing portions includes an outlet through which the pumped lubricant is directed toward the rotating element.

POWER TRANSMISSION DEVICE FOR HELICOPTER

A transmission device includes a casing accommodating a transmission gear and having an oil sump for retaining oil. The oil in the oil sump flows from a lubrication pump through a lubrication passage and is injected to the transmission gear. A connection portion is provided in a part of the lubrication passage, which part is disposed outside the casing. A direction control valve is provided downstream of the lubrication pump and upstream of the connection portion in the lubrication passage with respect to a flow direction of the oil. The direction control valve is configured to open the lubrication passage when a hydraulic pressure in the lubrication passage exceeds a predetermined value and to close the lubrication passage when the hydraulic pressure is equal to or lower than the predetermined value.

HYBRID PRESSURIZED AND NON-PRESSURIZED LUBRICATION SYSTEM FOR AIRCRAFT GEARBOX
20200109776 · 2020-04-09 ·

In some examples, an aircraft gearbox comprises a plurality of gears and a hybrid lubrication system to lubricate the plurality of gears. The plurality of gears comprises a first gear and a second gear. The plurality of gears operable to rotate based on torque received from a driveshaft. The hybrid lubrication system comprises a pressurized lubrication system and a non-pressurized lubrication system. The pressurized lubrication system comprises a nozzle to spray a lubricant onto the first gear. The non-pressurized lubrication system comprises a reservoir to catch a portion of the lubricant from the pressurized lubrication system. The second gear is operable to disperse the lubricant across others of the plurality of gears based on the second gear rotating through the portion of the lubricant.

Oil baffle for gas turbine fan drive gear system

A turbo fan engine includes a housing that supports a compressor section. At least one compressor hub is within the compressor section. A compressor shaft is arranged in the compressor section. An epicyclic gear train is coupled to the compressor shaft. At least one compressor hub and the compressor shaft are coupled at a common attachment point. The epicyclic gear train includes a carrier. A sun gear and intermediate gears are arranged about and intermeshing with the sun gear. The intermediate gears are supported by the carrier. A baffle is supported relative to the carrier and includes a lubrication passage near at least one of the sun gear and intermediate gears for directing a lubricant on at least one of the sun gear and the intermediate gears.

Lubrication system
11879539 · 2024-01-23 · ·

An insert for supplying a fluid to splines of a drive shaft, the insert comprising an insert wall extending between a first end and a second end of the insert, a chamber surrounding the insert wall for storing a fluid, a piston having a surface configured to be exposed to the fluid, the piston configured to move between a first position and a second position within the chamber, and the piston biased toward the first position, and wherein an increase in supply of the fluid in the chamber causes the piston to move toward the second position and a decrease in supply of the fluid in the chamber causes the piston to move toward the first position.

Lubricating device of gear apparatus for vehicle

A lubricating device of a gear apparatus for a vehicle lubricates a low-rotation-side gear and a high-rotation-side gear meshing with the low-rotation-side gear. The lubricating device comprises a first tooth surface lubricating oil supply part configured to supply a lubricating oil directly to a tooth surface position located more upstream of a rotating direction of the low-rotation-side gear than a meshing position of the low-rotation-side gear with the high-rotation-side gear so as to spray some of the lubricating oil from the tooth surface position toward a tooth surface of the high-rotation-side gear, and an in-shaft lubricating oil supply part configured to supply the lubricating oil into a shaft of the high-rotation-side gear.