Bearing arrangement for a machine element having a bearing having an outer bearing race radially fixed by a cylindrical cutout in the mounted state of the bearing arrangement; a locking element having an annular radial portion and at least one axial portion; and the annular radial portion of the locking element cooperates with a region of the outer bearing race on a first axial side of the outer bearing race to secure the outer bearing race at the first axial side; and at least one securing element which, in a mounted state of the bearing arrangement, is in operative engagement with the at least one axial portion of the locking element and with the machine element such that the locking element secures the outer bearing race at the first axial side.

Support assembly for movable, rotating or sliding shafts, having a bearing unit, a casing and a cover for fluid sealing an opening of an internal seat of the casing; the cover having an annular coupling portion towards a radially outer lateral surface of the casing, the annular coupling portion being provided radially on the inside with at least one pair of teeth projecting radially towards the inside of the cover and spaced circumferentially from each other; the radially outer lateral surface of the casing being provided with an annular groove for receiving the teeth of the cover, which in turn is provided circumferentially with an alternating plurality of depressions and projections; the annular groove having at least one pair of mechanical stops of the at least one pair of teeth of the cover, the mechanical stops extending in a radial direction with respect to corresponding depressions to be flush with the lateral surface of the casing.

An aerial vehicle includes an airframe; vertical propulsion units, and a controller. The vertical propulsion units are mounted to the airframe and include propellers oriented to provide vertical propulsion to the aerial vehicle. The vertical propulsion units are physically organized in quadrants on the airframe with each of the quadrants including two or more of the vertical propulsion units. The controller is coupled to the vertical propulsion units to control operation of the vertical propulsion units. At least two of the vertical propulsion units in each of the quadrants are adapted to counter-rotate from each other during flight of the aerial vehicle.

An interconnectable locking module having a first portion including an external surface defining a bulbous connector extending along a longitudinal axis; a second portion opposite of the first portion, the second portion includes an interior surface defining a hollow receptacle, and an opposite exterior surface defining a circumferential flange having a tapered channel. The tapered channel includes a channel opening and an opposite closed end. The module also includes a locking ring having an interior circumferential surface insertable over the bulbous connector and engageable with the circumferential flange. The locking ring includes a tab insertable into the channel opening and slidable against a tapered channel surface. A plurality of interconnectable locking module may be joined in series to provide an assembly such as a physical model representing a prototype conduit or a path for a conduit.

A bearing arrangement for supporting an endless screw of a steering gear on a gear housing of the steering gear. The bearing arrangement including a radial bearing rotationally connected to the endless screw. A resilient retention element connecting the radial bearing to the gear housing. The retention element is connected at the radial bearing side to an outer face of an outer bearing ring and fixed to the outer face of the outer bearing ring in an axially non-movable manner with respect to a longitudinal center axis of the radial bearing.

The invention relates to fastening elements for connecting transmission means such as tie rods, Bowden cables or the like to lever elements, in particular for motor vehicle locks, and to connecting arrangements equipped with such fastening elements. In order to allow reliable mounting and a structurally simple manufacture of the fastening elements, the fastening element is provided with a bayonet contour in such a manner that the fastening element, when mounted, is hinged to the lever element so as to be swiveled about a swivel axis. Owing to the swivelability and secure fastening to the lever element, the fastening element is particularly suitable for use in an actuation-force transmission chain between a motor vehicle lock and an actuating element for actuating said motor vehicle lock.

A ball and socket joint assembly is disclosed herein. The assembly includes a ball including a stud head and a shank, a socket including a cavity configured to receive the stud head, a retention surface, and a plurality of retention portions, and an interlocking member including a plate portion having an engagement surface that, in use, interfaces with the retention surface and the plurality of retention portions to achieve an interlocked position between the interlocking member and the socket.

An unlocking device has a release lever that is connected pivotably to a carrier element and is in each case connected via Bowden cables to a catch hook for clip elements in a vehicle hood. The catch hook is moved by the Bowden cables that are actuated via the release lever, counter to the spring force of a spring element into an unlocking position for opening the vehicle hood.

A technique for controlling vertical propulsion units of an aerial vehicle includes determining whether an initial thrust command output vector results in a thrust command clipping of one of the vertical propulsion units. The vertical propulsion units are physically organized into propulsion rings including an inner ring and an outer ring. Torque associated with the initial thrust command output vector is transferred from each the vertical propulsion units in the outer ring to the vertical propulsion units in the inner ring when the thrust command clipping of one of the vertical propulsion units in the outer ring occurs. A revised thrust command output vector is determined after transferring the torque. The vertical propulsion units are driven according to the revised thrust command output vector.

A support assembly for a moveable, rotating, or sliding shaft includes a casing and a cover. The casing includes a front edge defining an opening and a radially external lateral surface having an annular seat. The annular seat includes an annular groove axially spaced from the front edge and connected to a number of axial grooves that interrupt at least part of the front edge. The cover includes an annular coupling portion extending toward the radially external lateral surface of the casing. The annular coupling includes at least one pair of teeth formed on a radially inside surface of the annular coupling portion and projecting radially inward, each pair of teeth spaced circumferentially from each other, and a plurality of radially internal projections. A bottom wall of the annular groove includes a plurality of depressions alternating with a plurality of projections.