Patent ID: 8113798

Claim:
A turbomachine comprising: a housing; a rotor mounted radially and axially in the housing, said rotor having a shaft and at least one impeller attached to the shaft; two radial bearings, said bearings being adapted to mount the rotor in the housing; two tilt segment bearings having tilt segments and acting in opposite directions, said tilt segment bearings adapted to axially mount the rotor in the housing, wherein each of said tilt segment bearings interacts with an assigned contact surface of the shaft; at least two force measurement devices, wherein for each of said two tilt segment bearings acting in opposite directions, at least one of said force measurement devices is provided, wherein said force measurement devices operate independently of each other and are each assigned to a single tilt segment of a corresponding tilt segment bearing and directly detect axial force acting on the corresponding tilt segment; an electronic control device connected to each force measurement device, said electronic control device being adapted to determine a direction and amount of the axial force from a comparison of determined force values for the two tilt segment bearings, and a sealed pressure chamber formed between a rotor surface and an assigned housing surface, said pressure chamber being connected with a high-pressure line and a gas outlet by way of a feed line and a pressure regulation valve controlled by the electronic control device, wherein pressure (p) that prevails in the sealed pressure chamber exerts a force that acts on the rotor in an axial direction, and wherein the pressure in the pressure chamber is increased or reduced as a function of the measurement values of the force measurement devices, by the pressure regulation valve to minimize axial force acting on the rotor.