Abstract: A turbomachine, in particular, a compressor, having a housing and having at least one housing insert accommodated therein and having a fitting piece for the adjustment of a gap dimension between the housing and the housing insert, wherein the housing comprises, for the adjustment of the gap dimension, a horizontally adjustable guide element into which the fitting piece is inserted, is provided.

Abstract: A multi-stage integrally geared compressor includes a first process stage, a second process stage and a gearbox for coupling the two process stages to each other at different rotational speeds. The gearbox further couples a compressor drive shaft to the two process stages at a further rotational speed, which is different from the rotational speeds of the process stages.

Abstract: A casing is provided having a longitudinal axis of a turbomachine, the axis extending along a rotor. The casing includes at least one jacket part extending along the longitudinal axis and at least one end-face cover. The cover is surrounded by the jacket part at least with a part of the axial extension of the cover. In order to reduce the need for radial clearance, without compromising the availability or safety of the operation of the machine, the cover has radial clearance with respect to the jacket part and at least two separate guide elements of the cover are provided on the jacket part in two different circumferential positions with respect to the longitudinal axis. The respective guide elements are designed such that they block a respective movement of the cover in the circumferential direction at least unidirectionally.

Abstract: A pressure vessel including a lid, wherein the lid is fixed to a corresponding lid receptacle, wherein the lid has a first bearing surface that extends in the circumferential direction and interacts in a sealing manner with a second bearing surface on the pressure vessel, wherein fixing elements are provided for fixing the lid to the pressure vessel. The fixing elements are wedge-shaped, rest on an abutment surface of the pressure vessel and on a contact surface of the lid such that, when the fixing element is moved in a direction that causes a wider section of the wedge shape to be located between the abutment surface and the contact surface, the bearing surfaces are brought closer together or braced against each other.

Abstract: A separating apparatus for separating out particles, especially liquid droplets from a gas flow which comprises the particles, comprising a flow channel which conducts the gas flow and has at least one deflection region for deflecting the gas flow, and a collecting vessel for accommodating the particles, the flow channel also having a branch leading to the accommodation vessel for separating the particles out of the gas flow, is in accordance with the invention, characterized in that, in addition to the branch, a line opens into the accommodation vessel and connects the accommodation vessel to the flow channel in a fluid-conducting manner.