Abstract: Aircraft engines include an engine housing, a core assembly arranged within the engine housing and comprising an engine shaft arranged axially within the engine housing extending in a forward-aftward direction, and a tail cone assembly attached to an aft end of the engine housing. The tail cone assembly includes a tail cone housing and an aircraft machine arranged within the tail cone housing the aircraft machine comprising a rotor shaft. An input shaft is configured between the engine shaft and the rotor shaft and a rotor coupling configured to sealing connect the rotor shaft and the input shaft, the rotor coupling configured to providing sealing engagement between the rotor shaft and the input shaft during at least one of relative axial displacement and relative radial displacement between the rotor shaft and the input shaft.

Abstract: A system includes a permanent magnet generator (PMG) with a generator shaft defining a longitudinal axis. A brake system includes a brake shaft with a first end operatively connected to the generator shaft for selectively rotating with the generator shaft or braking to slow the generator shaft. A shear shaft is operatively connected to a second end of the brake shaft axially opposite the first end along the longitudinal axis. The brake system includes a wedge with a first position radially withdrawn from the brake shaft, and a second position radially pressed against the brake shaft for applying braking forces to the brake shaft and to the generator shaft.

Abstract: A vibration damping assembly for use with a second shaft nested within an interior of a first shaft is provided including a collar rotatable with the first shaft, and a cage rotatable with the second shaft and having at least one window formed therein. The collar and the cage are mounted concentrically. At least one damping mechanism is positioned within the at least one window. The at least one damping mechanism includes at least one flyweight and at least one support wedge. The at least one flyweight movable relative to the cage to frictionally engage an adjacent surface of the collar.

Abstract: A system includes a permanent magnet generator (PMG) with a generator shaft defining a longitudinal axis. A brake system includes a brake shaft with a first end operatively connected to the generator shaft for selectively rotating with the generator shaft or braking to slow the generator shaft. A shear shaft is operatively connected to a second end of the brake shaft axially opposite the first end along the longitudinal axis. The brake system includes a press fit sleeve engaged about the brake shaft and an actuator. The actuator is operatively connected to actuate a pawl between a first position spaced apart from the press fit sleeve for normal operation of the PMG, and a second position engaged with the press fit sleeve to apply braking forces to the press fit sleeve and to the generator shaft.

Abstract: An electric machine includes a stator winding in a stator having a winding end. A jumper has a main base end that is connected to the winding end. A first terminal branch of the jumper has a first terminal for connecting the stator electrically to a first load. A second terminal branch of the jumper has a second terminal for connecting the stator electrically to a second load. A first electrical conduction path is defined from the winding end, through the jumper to the first terminal branch to the first terminal. A second electrical conduction path is defined from the winding end, through the jumper to the second terminal branch to the second terminal. The first electrical conduction path has an electrical resistance substantially equal to that of the second electrical conduction path for electrical load balancing from the winding end to the first and second terminals.

Abstract: A governor of an integrated drive generator includes a housing, and a rotating sleeve extending at least partially through a housing opening in the housing. The rotating sleeve is configured to rotate about a sleeve axis. A gear is secured to the rotating sleeve and rotatable therewith. The gear is located at a sleeve tip of the rotating sleeve outside of the housing. One or more lubricant drain openings are located at a tip surface of the rotating sleeve. The one or more lubricant drain openings are configured to drain a flow of lubricant from the governor.

Abstract: A generator assembly for a high temperature environment that exceeds a seal temperature limit in operation can include a generator housing enclosing one or more generator components and one or more attached components sealed to the housing. The assembly can include one or more seals disposed between each of the one or more attached components and the generator housing and an oil circuit within the housing configured to circulate oil. The assembly can include one or more oil spray orifices within the housing and in fluid communication with the oil circuit. Each of the one or more oil spray orifices can be directed at an interior portion of the one or more attached components and/or an interior housing area adjacent the one or more attached components to provide oil spray thereto for cooling each of the one or more seals to maintain the one or more seals below the seal temperature limit.

Abstract: A system includes a permanent magnet generator (PMG) with a generator shaft defining a longitudinal axis. A brake system includes a brake shaft with a first end operatively connected to the generator shaft for selectively rotating with the generator shaft or braking to slow the generator shaft. The brake system includes a band with a first position radially withdrawn from the brake shaft, and a second position radially pressed against the brake shaft for applying braking forces to the brake shaft and to the generator shaft. The brake system includes an actuator operatively connected to the band to actuate the band from the first position to the second position.

Abstract: A fluid line termination fitting for a tail cone generator can include a distal body portion configured to insert into a fluid circuit opening of a tail cone generator housing and a proximal body portion configured to receive a male fluid connector. The fitting can include a radial extension disposed axially between the distal portion and the proximal portion. The radial extension can extend radially outwardly relative to the distal portion and proximal portion to limit insertion of the distal body portion into the opening of the tail cone generator housing. The fitting can include a channel structure defining a flow channel through the distal body portion and the proximal body portion. The channel structure can include a proximal channel portion in fluid communication with a proximal opening and a distal channel portion in fluid communication with a distal opening.

Abstract: A housing for a generator assembly can include an outer housing shell configured to enclose a plurality of generator components and a stator baffle disposed within the outer housing shell at a distance from an inner surface of the outer housing shell to form an air gap between the stator baffle and the outer housing shell to thermally insulate the plurality of generator components. The stator baffle can be configured to mount to a stator assembly of the generator components.

Abstract: A generator assembly having: a generator; a generator case surrounding the generator and defining a case aperture; an output lead carrying power generated by the generator away from a stator of the generator; a first connector electrically connected to the output lead; an inner dielectric mount surrounding the first connector and disposed within the case aperture; an outer dielectric mount connected to the inner dielectric mount to define an overlapping portion where the outer and inner dielectric mounts overlap each other; a second connector contained in and surrounded by the outer dielectric mount, the outer dielectric mount configured to connect the output leads to a feeder cable via the first and second connectors; a first elastomeric moisture seal located between the inner and outer dielectric mounts at the overlapping portion; and a second elastomeric moisture seal located between the second connector and an inner surface of the outer dielectric mount.

Abstract: Aircraft engines include an engine housing, a core assembly arranged within the engine housing and comprising an engine shaft arranged axially within the engine housing extending in a forward-aftward direction, and a tail cone assembly attached to an aft end of the engine housing. The tail cone assembly includes a tail cone housing and an aircraft machine arranged within the tail cone housing the aircraft machine comprising a rotor shaft. An input shaft is configured between the engine shaft and the rotor shaft and a rotor coupling configured to sealing connect the rotor shaft and the input shaft, the rotor coupling configured to providing sealing engagement between the rotor shaft and the input shaft during at least one of relative axial displacement and relative radial displacement between the rotor shaft and the input shaft.

Abstract: A system includes a permanent magnet generator (PMG) with a generator shaft defining a longitudinal axis. A brake system includes a brake shaft with a first end operatively connected to the generator shaft for selectively rotating with the generator shaft or braking to slow the generator shaft. A shear shaft is operatively connected to a second end of the brake shaft axially opposite the first end along the longitudinal axis. The brake system includes a press fit sleeve engaged about the brake shaft and an actuator. The actuator is operatively connected to actuate a pawl between a first position spaced apart from the press fit sleeve for normal operation of the PMG, and a second position engaged with the press fit sleeve to apply braking forces to the press fit sleeve and to the generator shaft.

Abstract: A system includes a permanent magnet generator (PMG) with a generator shaft defining a longitudinal axis. A brake system includes a brake shaft with a first end operatively connected to the generator shaft for selectively rotating with the generator shaft or braking to slow the generator shaft. A shear shaft is operatively connected to a second end of the brake shaft axially opposite the first end along the longitudinal axis. The brake system includes a wedge with a first position radially withdrawn from the brake shaft, and a second position radially pressed against the brake shaft for applying braking forces to the brake shaft and to the generator shaft.

Abstract: An engine includes an engine casing and a shaft defining an axis of rotation. The shaft extends through the engine casing. A nose cone is rotatably coupled to the shaft and has a hollow interior. A generator is arranged at least partially within the hollow interior of the nose cone. The generator includes a rotor and a stator. The rotor is rotatably coupled to the shaft. A heat exchanger is mounted adjacent to the generator within the hollow interior of the nose cone. The heat exchanger is fluidly coupled to the generator.

Abstract: A sealing assembly of an input shaft includes a support structure, a bearing assembly, and an input seal. The input seal including an input seal housing having a first portion and a second portion. The first portion is arranged adjacent the bearing assembly. At least one face plate anti-rotation pin is coupled to the input seal housing and positioned adjacent the input shaft. A face plate is positioned adjacent the second portion. The face plate is configured to directly contact the input shaft.

Abstract: A clutch assembly includes a clutch pack, and a rotating control piston selectably engageable with the clutch pack via movement of the clutch piston along an axis of rotation of the control piston. The clutch piston includes a piston member engageable with the clutch pack, a cover plate installed into the piston member to define an enclosed volume, and an axially fixed chamber divider positioned in the enclosed volume to divide the enclosed volume into a control pressure chamber and a pressure balancing chamber. Both the control pressure chamber and the pressure balancing chamber are filled with hydraulic fluid, and the control piston is moved between a disengaged position and an engaged position via modulation of hydraulic pressure in the control pressure chamber.

Abstract: An aircraft oil management system includes a generator, pump, and pump control system. The generator is mechanically coupled to a prime mover via a the rotor shaft and is configured to output three-phase power. The pump is mechanically decoupled from the rotor shaft and delivers oil to the generator. The pump control system drives the pump independent of a rotational speed of the rotor shaft.

Abstract: A generator shaft assembly including a primary shaft, a disconnect shaft housed within the primary shaft, where a first end of the disconnect shaft is configured to couple with the primary mover and a second end of the disconnect shaft is configured to mate with the generator. A retainer ring housed within the primary shaft having at least a landing and a groove on an inner surface thereof and a retainer member positioned between the landing of the retainer ring and an outer surface of the disconnect shaft configured to limit axial motion of the disconnect shaft relative to the primary shaft.

Abstract: A shaft system includes an outer shaft including an inner surface defining a conduit and an inner shaft extending within the conduit. The inner shaft includes a radially extending passage having a first end and a second end. A centrifugal force activated damper extends between the outer shaft and the inner shaft. The centrifugal force activated damper includes a first member arranged between the inner shaft and the inner surface at the first end of the radially extending passage, a second member arranged between the inner shaft and the inner surface at the second end of the radially extending passage, and a connecting member extending through the radially extending passage. Rotation of the shaft system causes the first member and the connecting member to shift away from the second member into the inner surface of the outer shaft.