Abstract: The invention relates to an impeller for a turbomachine, in particular a radial turbomachine. The impeller has a number of blades which are held spaced apart from one another on the circumference of the impeller. The blades are designed with a radially running S-shaped contour.

Abstract: The invention relates to an impeller for an axial fan, having an impeller body, which has an outer impeller shell and a carrier disc having a hub for connection for conjoint rotation to a drive shaft. A multiplicity of radially outward-pointing blades, which each have a blade root and a vane, is arranged on the carrier disc. Each blade root has a fastening portion accommodated with positive engagement between two fastening segments each arranged opposite one another on both sides of the carrier disc. The two opposite fastening segments and the carrier disc each have at least two through-holes for accommodating a long sleeve and a short sleeve. The fastening portion can be clamped firmly between the two opposite fastening segments with the aid of screw bolts, in each case inserted through the sleeves, and nuts, wherein each blade root is guided in a respective recess of the carrier disc.

Abstract: An apparatus for hydraulically adjusting the blades of an impeller of an axial-flow fan, comprising an adjustment cylinder that on both sides of a piston displaceably disposed in the cylinder has a first chamber and a second chamber respectively provided with a connection to control oil lines connected to four-way valves. Not only a feed line leading to one of the control oil lines, but also a return line connected to the other control oil line, is each divided into two parallel branch lines. Two redundant four-way valves are provided, each being disposed in one of the parallel branch lines. Disposed in each branch line of each control oil line, between the respective connection and the respective four-way valve, is a seat valve that closes by spring force.

Abstract: A device for measuring the displacement travel of a hydraulic displacement mechanism for blades of an impeller of an axial-flow fan, wherein the displacement mechanism includes as components a displacement cylinder and a piston rod having a piston, one of the components being axially displaceable and the other component not being axially displaceable. Respective spindles of the blades are secured to a displacement disk to which is connected the axially displaceable component of the displacement mechanism. An oil transfer element surrounds an extension of the piston rod that extends out of the displacement cylinder. A magnetostrictive displacement-measuring device that includes a sensor housing with a wave guide, sensor head, and an annular magnet is coupled to the displacement mechanism. The sensor housing and the sensor head are connected to the oil transfer element. Either the oil transfer element or one of the displacement mechanism components is axially displaceable relative to the other component.

Abstract: An axial fan comprising an impeller provided with a supporting ring on which is disposed an adapter. Spindles are rotatably mounted in the supporting ring, and adjustable blades are connected to the spindles. A support is provided for each spindle and is comprised of a roller bearing that rests against an inner side of the supporting ring, and of a bushing that rests against an inner side of the adapter. A tubular nut is threaded onto the outer end of the spindle to fix it in the supporting ring.

Abstract: An axial fan comprising an impeller provided with a supporting ring on which is disposed an adapter. Spindles are rotatably mounted in the supporting ring, and adjustable blades are connected to the spindles. A support is provided for each spindle and is comprised of a roller bearing that rests against an inner side of the supporting ring, and of a bushing that rests against an inner side of the adapter. A tubular nut is threaded onto the outer end of the spindle to fix it in the supporting ring.