An apparatus comprising a shaft for a gas turbine engine, the shaft comprising a shaft flange; a turbine rotor for the gas turbine engine, the turbine rotor comprising a turbine rotor flange configured to couple to the shaft flange; and a stub shaft comprising a stub shaft flange configured to couple to the shaft flange. The stub shaft is concentric with the shaft and configured to have a first interference fit around a portion of the turbine rotor.

Embodiments of golf clubs with grooves and methods of manufacture thereof are described herein. In one embodiment of a golf club described herein, the golf club has a head with a body. The body has a strike face with channels and at least one insert located within at least one of the channels. At least one of the channels comprises a single groove, and the insert forms at least a portion of the single groove. At least one of the channels comprises an opening on the strike face that is narrower than a bottom of the at least one of the channels. Other embodiments and related methods are also disclosed herein.

Tool holder has a first section adapted to be connected to a machining center and a tool holding section comprising a bore with a surface defining an inner diameter of the bore. Dispersed around the surface of the bore and at least partially embedded in the surface of the bore is a joining compound having a Young's modulus greater than a Young's modulus of the surface of the bore.

Disclosed is a method for producing a rod antenna for a vehicle, wherein a coil spring (10) is connected on at least one of its two ends to an antenna component, and wherein the connection between the coil spring (10) and the antenna component is established by expanding the inner diameter of the coil spring (10), by at least partially sliding the antenna component into the expanded coil spring (10), and by subsequently returning the coil spring towards the original inner diameter for securing purposes. The invention is characterized in that a wire (18) is inserted into the intermediate region between the coil spring (10) and the antenna component when the coil spring (10) is expanded.

Disclosed is a method for producing a rod antenna for a vehicle, wherein a coil spring (10) is connected on at least one of its two ends to an antenna component, and wherein the connection between the coil spring (10) and the antenna component is established by expanding the inner diameter of the coil spring (10), by at least partially sliding the antenna component into the expanded coil spring (10), and by subsequently returning the coil spring towards the original inner diameter for securing purposes. The invention is characterized in that a wire (18) is inserted into the intermediate region between the coil spring (10) and the antenna component when the coil spring (10) is expanded.

A device for mounting at least one receiving element on a shaft may include at least one holder for holding a receiving element having a cut-out for receiving a shaft. A moveable guide slide may be configured to move the shaft in a first direction through the cut-out in the receiving element. A tailstock may be configured to move counter to the first direction. The tailstock may include a tailstock tip configured to couple to an end face of the shaft. A vibration generator may be arranged in the tailstock for vibrating the shaft.

A method is provided for connecting a first component to a second component. The first component has a deformation region, wherein the deformation region is at least partially heated in a first step. An inner die for the plastic deformation is provided in a second method step. The first component is plastically deformed in the deformation region in order to connect the first component to the second component in a third step, and wherein the deformation region is at least partially contacted by the inner die in the second step.

A method of monitoring tube integrity of a high-speed transportation system. The high-speed transportation system includes at least one tube structure having at least one track, at least one capsule configured for travel through the at least one tube structure between a plurality of stations, a propulsion system adapted to propel the at least one capsule through the structure, and a levitation system adapted to levitate the capsule within the structure. The tube structure is maintained as a low-pressure environment. The method includes directing a vehicle having at least one sensor along a tube path; and detecting a plume of air leaked from the low-pressure environment using the at least one sensor.

The invention relates to a process for the preparation of bent glazed modules comprising a metal framework and a panel comprising a laminated glazing comprising glass substrates separated by an interlayer made of polymer material, the panel being bent, after the laminated glazing has been assembled, by a force which causes it to take the shape of the metal framework and then held in this shape by a holding means, the bending being carried out while the interlayer is at a temperature between 30 and 80 C. The invention reduces the loads necessary for the bending and also the shear stresses between the interlayer made of polymer material and the glass substrates, which reduces the risks of delamination.

To provide a fitting member, an annular member, a joined member and a method of manufacturing the joined member, which prevent occurrence of a not-joined portion. A fitting member 10 has a fitting protrusion 10p which is protruded outward on an outside face 10s. An annular member 20 contains a space 20h in which the fitting member 10 is to be fitted. An annular member 20 has an annular protrusion 20p on an inside face 20f. When the fitting member 10 is fitted into the space 20h at a predetermined depth, the fitting protrusion 10p and the annular protrusion 20p fill not-joined portions which may be generated assuming that they are not provided. A joined member 30 is produced by fitting the fitting member 10 into the space 20h at the predetermined depth, so that a contact portion between the fitting member 10 and the annular member 20 is joined in solid phase.