A flow element, for a separation device, of simple construction and stably connectable to similarly constructed flow elements, includes a disc-shaped base body including a first side and a second side opposite the first side, wherein the first and/or second side includes a plurality of channels through which, in the mounted condition of the flow element in the separation device, a fluid is guidable outwards from a central opening in the base body, which is arranged centrally in the disc-shaped base body, or from the outside towards the centrally arranged central opening, wherein the base body includes a plurality of receiving portions at least on the first side and a plurality of projections at least on the second side, wherein, in the mounted condition of the flow element, the projections are engageable with the receiving portions of a further, similarly constructed flow element that is placed on the flow element.

A flow element, for a separation device, of simple construction and stably connectable to similarly constructed flow elements, includes a disc-shaped base body including a first side and a second side opposite the first side, wherein the first and/or second side includes a plurality of channels through which, in the mounted condition of the flow element in the separation device, a fluid is guidable outwards from a central opening in the base body, which is arranged centrally in the disc-shaped base body, or from the outside towards the centrally arranged central opening, wherein the base body includes a plurality of receiving portions at least on the first side and a plurality of projections at least on the second side, wherein, in the mounted condition of the flow element, the projections are engageable with the receiving portions of a further, similarly constructed flow element that is placed on the flow element.

The present invention is a centrifuge to be used for removing ice particles from the air fed to a gas turbine system. In an embodiment, the centrifuge is comprised of three ducts defining an air-path which comprises of two bends greater than 90 degrees. In an embodiment, the first two ducts extend past the bends to provide a dead air zone to trap ice particles which have been introduced by cooling air containing moisture. The dead air zones are further provided with revolving doors which remove the ice particles from the system. In an embodiment, the centrifuge receives cold air from the compander and removes ice particles before exhausting the cold air to a gas turbine electric generator, such that the blades of the gas turbine generator are not damaged by the ice particles.

The present invention is a centrifuge to be used for removing ice particles from the air fed to a gas turbine system. In an embodiment, the centrifuge is comprised of three ducts defining an air-path which comprises of two bends greater than 90 degrees. In an embodiment, the first two ducts extend past the bends to provide a dead air zone to trap ice particles which have been introduced by cooling air containing moisture. The dead air zones are further provided with revolving doors which remove the ice particles from the system. In an embodiment, the centrifuge receives cold air from the compander and removes ice particles before exhausting the cold air to a gas turbine electric generator, such that the blades of the gas turbine generator are not damaged by the ice particles.

A centrifugal separator structure is configured for cleaning of crankcase gases from an internal combustion engine. The centrifugal separator structure includes a separator rotor configured for rotation about a centre axis arranged inside a stationary housing. The separator rotor includes an axle member configured for connection to a shaft of a driving device. A stack of separation discs is supported on the axle member. The axle member is un-journaled inside the stationary housing when the centrifugal separator structure is separate from the driving device. Further, an assembly includes the centrifugal separator structure and a driving device.

A centrifugal separator structure is configured for cleaning of crankcase gases from an internal combustion engine. The centrifugal separator structure includes a separator rotor configured for rotation about a centre axis arranged inside a stationary housing. The separator rotor includes an axle member configured for connection to a shaft of a driving device. A stack of separation discs is supported on the axle member. The axle member is un-journaled inside the stationary housing when the centrifugal separator structure is separate from the driving device. Further, an assembly includes the centrifugal separator structure and a driving device.

A rotor-type apparatus for centrifugal cleaning of crankcase gases from a combustion engine. The rotor is hydraulically driven by pressurized oil by means of a turbine wheel located in an oil collection chamber. A pressure equalizing and gas discharging conduit, which extends into the collection chamber and has an upper aperture located above a liquid level of the oil in the collection chamber during the operation, is connected to an outlet conduit for the propellant oil from the collection chamber.

A rotor-type apparatus for centrifugal cleaning of crankcase gases from a combustion engine. The rotor is hydraulically driven by pressurized oil by means of a turbine wheel located in an oil collection chamber. A pressure equalizing and gas discharging conduit, which extends into the collection chamber and has an upper aperture located above a liquid level of the oil in the collection chamber during the operation, is connected to an outlet conduit for the propellant oil from the collection chamber.

A centrifugal air-oil separator system for a gas turbine engine system is described. The air-oil separator system has a rotatable shaft and the shaft includes an axially extending bore formed at least partially through the shaft. A gear is integral to or mounted on an outer surface of the shaft. The air-oil separator system also includes a bolt-on breather mounted on the shaft and independent from and in contiguous contact with the gear to assist in separating the oil from the air. Various types of materials may be utilized in the construction of the air-oil separator system.

A centrifugal air-oil separator system for a gas turbine engine system is described. The air-oil separator system has a rotatable shaft and the shaft includes an axially extending bore formed at least partially through the shaft. A gear is integral to or mounted on an outer surface of the shaft. The air-oil separator system also includes a bolt-on breather mounted on the shaft and independent from and in contiguous contact with the gear to assist in separating the oil from the air. Various types of materials may be utilized in the construction of the air-oil separator system.