Abstract: The present invention describes a rolling tool device for compression rolling of, in particular, blade elements of a rotor area of a jet engine provided with a tool carrier. The tool carrier is connectable to a carrier spindle. Furthermore, two pliers-type bodies are rotatably connected to the tool carrier. The pliers-type bodies are each provided with a rolling area, with a distance between the rolling areas being variable in dependence of the rotary movement of the pliers-type bodies. In accordance with the present invention, an axis of the carrier spindle in the state connected to the tool carrier passes between the rolling areas through a contact point present at a distance between the rolling areas equal to zero.
Type:
Grant
Filed:
April 12, 2012
Date of Patent:
May 3, 2016
Assignee:
Rolls-Royce Deutschland Ltd & Co KG
Inventors:
Goetz G. Feldmann, Karsten Roettger, Stefan Zenk
Abstract: In a method of making a sheet metal part for motor vehicles, a blank is placed with its opposite length sides between outer lower forming jaws of a die. The blank is then clamped by moving the outer lower forming jaws toward one another. Outer upper forming jaws are then moved to their closed position so that the length sides of the blank are secured in place between the lower and upper forming jaws. The lower and upper forming jaws and a press tool are then moved toward one another, and the blank is shaped to its final configuration to produce a sheet metal part.
Abstract: An Apparatus and method for forming elongated metal articles includes one or more rotating dies (1) each provided with an indentation (3). The indentation (track) is shaped so as to be complementary to the actual final shape of the resulting articles, and the dies (1) are designed and adapted to ensure/allow three rotational degrees of freedom under deformation by rotation of the dies.
Abstract: A method and apparatus for expanding and contouring honeycomb preforms into compound curved honeycomb core sheets. Honeycomb preforms are provided having a plurality of face to face, contiguous, strips bonded together at selected narrow areas such that when strips along opposite edges are moved away from each other a sheet having a repeating array of regular hexagonal cells results. Opposite edge strips are secured to two spaced arms located adjacent to a freely rotatable crowned drum having a surface contour corresponding to the desired honeycomb sheet configuration. One of said arms is pivoted about the drum axis. As the arms are moved apart, a flat partially expanded honeycomb sheet initially develops. As arm movement continues, the sheet then comes into sliding contact with the drum surface. When cell expansion is completed, during the final shaping and setting phase, the honeycomb core sheet is in full contact with the drum surface.
Abstract: A method of manufacturing a high fin density heat dissipator is disclosed in which the dissipator is extruded through a die in a partially cylindrical shape with the elongated fins arranged on the base and extending radially therefrom. The extruded dissipator is straightened under tensile and bumping forces in a manner such that the base assumes a planar shape and the fins become substantially parallel to each other. Apparatus for straightening the extruded dissipator and a die for extruding the same are illustrated and described.
Abstract: The machine according to the invention is intended for making cone shells by coiling up sheet blanks in the form of a circular sector. The machine comprises adjustable clamps for clamping the radial edges of the blank, said adjustable clamps being located on the base with a provision for turning towards each other with relation to their fixing point and for turning around their own longitudinal geometrical axis for which purpose the ends of the adjustable clamps are provided with hinges. Each adjustable clamp has also a device intended to prevent its turning around its own longitudinal geometrical axis. As a result, the machine can be used successfully for making cone shells with practically any coning angle.
Type:
Grant
Filed:
August 1, 1975
Date of Patent:
September 7, 1976
Inventors:
Rudolf Naumovich Fridman, Mark Lvovich Katalkherman, Sergei Petrovich Chistyakov