A belt drive mechanism with gear back-up comprises a driving pulley to which a driving gear is attached, a driven pulley to which a driven gear is attached, a drive belt drivingly connected between the driving and driven pulleys, and a back-up gear disposed between the driving and driven gears. When the drive belt is engaged with the driving and driven pulleys, teeth of the back-up gear are spaced apart from teeth of the driving and driven gears, and at least a portion of the teeth of the back-up gear are interposed between the teeth of the driving and driven gears. Thus, in a normal state, the drive belt is driven by the driving pulley and drives the driven pulley. However, in case of belt failure, the back-up gear is driven by the driven gear attached to the driving pulley and drives the driven gear attached to the driven pulley instead of the drive belt.

A belt drive mechanism with gear back-up comprises a driving pulley to which a driving gear is attached, a driven pulley to which a driven gear is attached, a drive belt drivingly connected between the driving and driven pulleys, and a back-up gear disposed between the driving and driven gears. When the drive belt is engaged with the driving and driven pulleys, teeth of the back-up gear are spaced apart from teeth of the driving and driven gears, and at least a portion of the teeth of the back-up gear are interposed between the teeth of the driving and driven gears. Thus, in a normal state, the drive belt is driven by the driving pulley and drives the driven pulley. However, in case of belt failure, the back-up gear is driven by the driven gear attached to the driving pulley and drives the driven gear attached to the driven pulley instead of the drive belt.

Powered limb prostheses with multi-stage transmissions are provided.

Powered limb prostheses with multi-stage transmissions are provided.

A phaser system is provided. The system includes a first gear connected to a first plate, and a second gear connected to a second plate. A phaser assembly includes at least one piston plate, and axial displacement of the at least one piston plate is configured to adjust a phase between the first gear and the second gear. A hydraulic fluid actuator assembly is also provided that includes a hydraulic fluid circuit including an advance chamber defined on a first side of the at least one piston plate and a retard chamber defined on a second side of the at least one piston plate. A valve selectively pressurizes the advance chamber or the retard chamber such that the at least one piston plate is axially displaced.

Constant velocity joints or homokinetic joints are used for the continuous transmission of rotational movements and torques. They transmit the rotational movement of a driving shaft to a shaft to be driven without changing the speed or torque. The transmission takes place independently of the speed, torque, or the value of a diffraction angle and independently of the speed at which this diffraction angle changes. Constant velocity joints with a diffraction angle of 90° are equipped with specially shaped gear pairs, which are held together by a spring-loaded inner joint. In this joint transmission, a diffraction angle of 90° is achieved while the shafts to be connected to fixedly mounted bevel- and spur gear pairs are connected to each other, so that no spring-loaded inner joint is needed. Therefore, high engine speeds and high torques can be transmitted.

A power transmission device includes a first power transmission path for transmitting a driving force of a motor to one driven shaft, and a second power transmission path for transmitting the driving force of the motor to another driven shaft. At least one of the first power transmission path or the second power transmission path includes a first intermediate rotor fixed to an output shaft of the motor, a second intermediate rotor rotated by the first intermediate rotor and moving arcuately along an outer circumference of the first intermediate rotor, a driving shaft rotated by the second intermediate rotor and transmitting the driving force to the one driven shaft or the another driven shaft. The driving shaft is configured to move in a direction perpendicular to an axial center direction of the driving shaft in accordance with movement of the second intermediate rotor around the first intermediate rotor.

The invention relates to a stabilization bearing system for a geared turbofan engine, in particular an aircraft engine, with a stabilization bearing for an input shaft device to an epicyclic gearbox device of the geared turbofan engine, the stabilization bearing being located axially in front of an input shaft device location bearing system.

The invention relates to a stabilization bearing system for a geared turbofan engine, in particular an aircraft engine, with a stabilization bearing for an input shaft device to an epicyclic gearbox device of the geared turbofan engine, the stabilization bearing being located axially in front of an input shaft device location bearing system.

A gear includes at least one gear tooth and an electrode mounted to the at least one gear tooth along a contact face of the at least one gear tooth. A flowable dielectric material is positioned on the contact face of the at least one gear tooth. The dielectric material is structured to be movable along the contact face of the at least one gear tooth responsive to a gravity force.