Patent classifications
B04B2005/125
HIGH SPEED CLEANING OF A CENTRIFUGAL SEPARATOR
A centrifugal separator for cleaning gas containing contaminants includes a stationary casing, enclosing a separation space through which a gas flow is permitted, a gas inlet extending through the stationary casing and permitting supply of the gas to be cleaned, a rotating member including a plurality of separation members arranged in said separation space and being arranged to rotate around an axis of rotation, a gas outlet configured to permit discharge of cleaned gas and including an outlet opening through a wall of the stationary casing, a drainage outlet configured to permit discharge of liquid impurities separated from the gas to be cleaned, and a drive member, for rotating the rotating member. The centrifugal separator further includes a control unit configured to control the drive member to rotate the rotating member at a first speed during a separation phase and at a second speed, which is higher than the first speed, during a cleaning phase to remove clogging on or between said separation members, wherein the cleaning phase is shorter in time than the separation phase.
CRANKCASE VENTILATION SYSTEMS INCLUDING INTEGRATED SENSORS AND CONTROLLER
A rotating crankcase ventilation system comprises a housing comprising an inlet and an outlet, a motor comprising a stator and a rotor, and a shaft. A first end of the shaft is coupled to the rotor and configured to rotate in response to rotation of the rotor. A filter element is coupled to the shaft. A sensor is configured to measure at least one operating parameter of the rotating crankcase ventilation system. A controller is operatively coupled to the sensor and the motor, the controller configured to receive the at least one operating parameter and selectively adjust operation of the motor to adjust rotation of the rotor, and thereby, the filter element based on the at least one operating parameter.
Separator
A separator includes a rotor, a plurality of flow channels each of which has an inlet and an outlet for gas and are in a vicinity of a rotation axis of the rotor, an air current producer configured to cause gas to flow through the plurality of flow channels, a driving device configured to rotate the rotor to rotate the plurality of flow channels around the rotation axis, and a discharger for allowing discharge of solid materials suspended in airstream produced in each of the plurality of flow channels, in a direction away from the rotation axis.
GAS TURBINE SYSTEM
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.
OIL SEPARATOR
An oil separator includes: a rotor having an inner peripheral space and configured to be rotated by introducing, into the inner peripheral space, oil for separation and processing-target gas containing mist oil so that the mist oil is separated from the processing-target gas; and a case having an internal space and an inlet hole communicating with the internal space, the internal space housing a separation chamber having the rotor, the case including a plurality of convex portions on an inner wall surface which constitutes the internal space, the plurality of convex portions arranged adjacently in a direction along the inner wall surface, and extending in an up-down direction.
A CENTRIFUGE ROTOR FOR A CENTRIFUGAL SEPARATOR, A CENTRIFUGAL SEPARATOR, A METHOD OF SEPARATION, AND A CONICAL DISK
A centrifuge rotor for a centrifugal separator for separation of a relatively heavy phase of a fluid from a relatively light phase of the fluid is disclosed. The centrifuge rotor includes a stack of conical disks, and has a central axis of rotation. Each conical disk has an outward surface and an inward surface. The stack of conical disks includes a plurality of interspaces between adjacent conical disks. The interspaces include first interspaces for separation of the relatively heavy phase from the relatively light phase, and second interspaces. A check valve device is provided in each second interspace for closing the second interspace in an inward direction towards the central axis, and permitting opening of the second interspace in an outward direction. Also a centrifugal separator, a method for separation and a conical disk are disclosed.
Gas turbine system
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.
Stackable disc-shaped flow element and separation device
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.
GAS TURBINE SYSTEM
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.
ROTOR OF A CENTRIFUGAL SEPARATOR
A rotor of a centrifugal separator, wherein the rotor comprises a central shaft on which an axially movable plate stack, formed by multiple plates, is arranged. A stack base is arranged on the shaft under the plate stack. A stack cap is arranged in an axially moveable manner on the shaft above the plate stack. The rotor includes a compression spring surrounding the shaft, with a first end supported on the shaft and a second end supported on the stack cap, pressing the plate stack together. The rotor includes a sleeve-like extension arranged on the stack cap, projecting into the plate stack and surrounding the shaft with a separation. The compression spring is located inside the extension, at least over a majority of the axial length thereof. A support surface for the second end of the compression spring, is arranged on a base of the extension.