Abstract:
Zur Verkürzung der Prozesskette beim Materialabnehmenden Bearbeiten, insbesondere einer Kurbelwelle (1), nach der Grobbearbeitung, und insbesondere nach dem Härten, wird erfindungsgemäß vor allem die Kombination aus Drehfräsen oder Singlepoint-Drehen als erstem Schritt und nachfolgendem Feinbearbeitungsschritt mittels Finishen, elektrochemischem Ätzen, vorgeschlagen
Abstract:
Zur Verkürzung der Prozesskette beim materialabnehmenden Bearbeiten, insbesondere einer Kurbelwelle (1), nach der Grobbearbeitung und insbesondere nach dem Härten, wird erfindungsgemäß vor allem die Kombination aus Umfangsdrehfräsen als erstem Schritt und nachfolgendem Trockenschleifen als zweitem Schritt vorgeschlagen.
Abstract:
A liquid phase diffusion welding method for a metallic part capable of increasing the quality and productivity of a joint part by achieving the shortage of welding time, the uniformization of welding structure, and increases in the tensile strength and fatigue strength of a joint to increase the quality and reliability thereof. An amorphous alloy foil for liquid phase diffused welding is disposed on the fusion face of a metal material. As a primary welding, the amorphous alloy foil and the metal material are fused and press-welded to each other by a resistance welding to form the joint part. As a second welding, the joint part is re-heated to the melting point of the amorphous alloy foil or higher and then the temperature is maintained until the solidification of the joint part is completed.
Abstract:
A crankshaft having a crankpin, a crank journal, and a crank arm for linking the crankpin and the crank journal, includes a pin fillet portion located between the crankpin and the crank arm; and a journal fillet portion located between the crank journal and the crank arm. At least one of the crankpin and the crank journal has a diameter of no less than about 20 mm and no more than about 40 mm. At least one of the pin fillet portion and the journal fillet portion contains a quench-hardened layer having a thickness of no less than about 1 mm and no more than about 2 mm in the vicinity of a surface thereof. The crankpin and the crank journal substantially do not contain any quench-hardened layer having a thickness exceeding about 2mm in the vicinity of a surface thereof.
Abstract:
The invention relates to a method for assembling a camshaft by using a shaft (10) and a plurality of cams (21-26) comprising respectively an opening for the shaft. According to the invention, the cams are disposed in a tight manner in a storage element (40), in such a way that they are orientated towards each other in a predefined rotative position, the openings thereof for the shaft being orientated in a coaxial manner. The shaft is then introduced into the cam packet and arranged consecutively with respect to each individual cam by displacement in the longitudinal direction thereof. The cams are secured one after the other on the shaft. The required rotation of the cams can be obtained in a simple manner by longitudinal displacement of the shaft and also by optionally rotating the shaft at a certain angle.
Abstract:
Standard camshafts, produced by an internal high-pressure forming method (IHU) and whereof the cam rings (1) are fixed on a hollow shaft by force-closure and form-closure, said rings being produced in accordance with their function in a separate process, have the drawback that the cam rings are deformed, mainly in the tip zone (2) of the cams, can result in cracking or breaking. The invention is characterized in that the cam ring is produced in terms of its material properties such that in its outer zone (3) the material is hard and resilient over a specific length while exhibiting nevertheless low plastic deformation, the zone located beneath being relatively flexible and plastically deformable. The inventive camshafts are used almost exclusively in motor vehicles engines.
Abstract:
A procedure is described for the repair of gas turbine engine turbine components which involves the repair of cracks and other defects and the replacement of worn or eroded material followed by the laser melting of a thin layer of metal on the surface of the component in those areas requiring reconfiguration to return to the original dimensions. The reconfiguration by laser melting is also useful for new articles which are out of tolerance, and generally for shaping objects from metal sheet or plate.
Abstract:
Die Erfindung betrifft eine Vorrichtung (1) zum Laserstrukturieren von Naben (2) von Ventiltriebbauteilen (3). Erfindungswesentlich ist dabei, dass - zumindest ein Ladungsträger (4) zum Bevorraten und Bereitstellen von zumindest zwei Ventiltriebbauteilen (3) vorgesehen ist, - zumindest ein Laser (5) zum Laserstrukturieren einer Nabe (2) des Ventiltriebbauteils (3) vorgesehen ist, - zumindest ein Roboterarm (6) mit wenigstens einer Greifeinrichtung (7) zum Greifen, Positionieren und Halten zumindest eines Ventiltriebbauteils (3) während des Laserstrukturierens vorgesehen ist, wobei der Roboterarm (6) zudem zum Entnehmen zumindest eines Ventiltriebbauteils (3) aus dem Ladungsträger (4) und Zuführen desselben zum Laser (5) ausgebildet ist. Hierdurch kann eine kürzere Taktzeit erreicht werden.
Abstract:
The invention relates to a method for producing a sintered part having a highly precise molded part height, the sintered part being produced from a first sintered joining part (3) that has a first joining surface (4) and a second sintered joining part (7) that has at least a second joining surface. The method comprises at least the following steps: joining the first sintered joining part and the second sintered joining part, the first joining surface (4) being oriented such that it faces the second joining surface (8); pressing the first sintered joining part and the second sintered joining part against each other under axial compression pressure exerted by a pressing tool, the highly precise molded part height being brought about by pressing the parts against each other; removing the sintered part from the pressing tool as a sintered part having a highly precise molded part height. The invention also relates to a parts set (1) of sintered joining parts.