The present document relates to an air cooling assembly comprising a transmission assembly, a coupling housing mounted on the transmission assembly, a transmission input shaft at least partially disposed within the coupling housing and defining an axial direction, an air fan mounted on the transmission input shaft, and a fan hood at least partially enclosing the coupling housing and at least partially extending over the transmission assembly in the axial direction. The fan hood is configured to guide an air flow created by the air fan for cooling the transmission assembly.

A surgical apparatus is provided. The surgical apparatus includes a surgical actuating device including a shaft supporting a first coupling member. The first coupling member includes one or more pairs of apertures. The reload includes a second coupling member including a locking assembly. The second coupling member includes a pair of spring pins positionable within the pair of apertures. The spring pins being movable from an inward position to a radial outward position. The locking assembly includes a lock plate that is moveable from a first position located between the spring pins to a second position spaced from the spring pins. In the radial outward position, the spring pins are received within the apertures of the first coupling member to secure the reload to the surgical actuating member and when the lock plate is in the first position, the reload cannot be separated from the surgical actuating device.

There is disclosed an aircraft engine assembly including an engine having an engine shaft; an output shaft; a clutch in driving engagement between the engine shaft and the output shaft. The clutch has a first component in driving engagement with the engine shaft and a second component. The clutch is operable between first and second configurations. In the first configuration, the first component is rotatable relative to the second component and the engine shaft is rotatable relative to the output shaft. In the second configuration, the first and second components are engaged with one another and the engine shaft rotates with the output shaft. A mechanical lock is operable between first and second positions. In the first position, the mechanical lock is disengaged from the first component. In the second position, the first and second components are secured for joint rotation one relative to the other.

There is disclosed an aircraft engine assembly including an engine having an engine shaft; an output shaft; a clutch in driving engagement between the engine shaft and the output shaft. The clutch has a first component in driving engagement with the engine shaft and a second component. The clutch is operable between first and second configurations. In the first configuration, the first component is rotatable relative to the second component and the engine shaft is rotatable relative to the output shaft. In the second configuration, the first and second components are engaged with one another and the engine shaft rotates with the output shaft. A mechanical lock is operable between first and second positions. In the first position, the mechanical lock is disengaged from the first component. In the second position, the first and second components are secured for joint rotation one relative to the other.

A torque transfer assembly includes a drive shaft and a driven shaft and a dielectric connector positioned between. The connector connects the drive shaft and the driven shaft and includes a body of dielectric material defining an insulating barrier between the drive and the driven shaft. The connector includes a dielectric barrier body having a first side from which a protrusion extends, the protrusion configured to engage in a correspondingly shaped recess formed in one of the drive shaft or the driven shaft, and a second side, opposite the first side, in which is formed a recess shaped to receive a correspondingly shaped protrusion extending from the other of the drive shaft or the driven shaft, the connector providing a dielectric barrier between the drive shaft and the driven shaft.

A torque transfer assembly includes a drive shaft and a driven shaft and a dielectric connector positioned between. The connector connects the drive shaft and the driven shaft and includes a body of dielectric material defining an insulating barrier between the drive and the driven shaft. The connector includes a dielectric barrier body having a first side from which a protrusion extends, the protrusion configured to engage in a correspondingly shaped recess formed in one of the drive shaft or the driven shaft, and a second side, opposite the first side, in which is formed a recess shaped to receive a correspondingly shaped protrusion extending from the other of the drive shaft or the driven shaft, the connector providing a dielectric barrier between the drive shaft and the driven shaft.

A power unit is configured for use as part of a concrete screed and includes a frame and a powered drive. The frame includes a drive housing. The powered drive is operably supported by the drive housing and is configured to rotate a rotatable concrete forming drum. The powered drive includes an electric motor and a battery operably coupled to the electric motor and configured to power the electric motor. The powered drive includes a drive shaft drivingly connectable relative to the drum, with rotation of the drive shaft causing corresponding rotation of the drum.

A torque transmitting assembly including a first drum having a plurality of teeth formed at an end thereof and a sensor component annularly extending on an inner surface of the first drum. A gear assembly axially aligns with the first drum and has a plurality of teeth intermeshing with the plurality of teeth of the drum. The gear assembly includes an annular gear and a plate axially aligning with the gear.

A torque transmitting assembly including a first drum having a plurality of teeth formed at an end thereof and a sensor component annularly extending on an inner surface of the first drum. A gear assembly axially aligns with the first drum and has a plurality of teeth intermeshing with the plurality of teeth of the drum. The gear assembly includes an annular gear and a plate axially aligning with the gear.

Exemplary embodiments are disclosed of socket adaptors for retaining impact sockets to impact tools.