| Class / Patent application number | Description | Number of patent applications / Date published |
|---|
| 415168100 | INCLUDING MEANS FOR HANDLING WORKING FLUID LEAKAGE | 20 |
| 20090246003 | TURBOCHARGER WITH SLIDING PISTON, AND HAVING VANES AND LEAKAGE DAMS - A turbocharger having a sliding piston for regulating exhaust gas flow into the turbine wheel includes a set of first vanes mounted on a fixed first wall of the turbine nozzle and projecting axially toward an opposite second wall of the nozzle, and/or a set of second vanes mounted on the end of the piston and projecting in an opposite axial direction toward the first wall of the nozzle. For the/each set of vanes, there are leakage dams formed on the wall that is adjacent the vane tips when the piston is closed. The leakage dams are closely adjacent the vane tips and discourage exhaust gas from leaking in a generally radial direction past the vane tips as the piston just begins to open from its fully closed position. | 10-01-2009 |
| 20090246004 | Recovery of Expander-Booster Leak Gas - A seal gas recovery method including introducing a first seal gas stream to a first mechanically coupled booster/expander assembly, where the first booster/expander assembly includes a first booster, a first expander, a first shaft that mechanically couples the first booster and the first expander, and a first seal on the first shaft. The method further includes removing at least a portion of a first recoverable gas stream from the first seal, where the first recoverable gas stream includes at least a portion of a first process leak gas stream and at least a portion of a first seal gas vent stream. The method further includes introducing a second seal gas stream to a second expander assembly, where the expander assembly includes a second expander, a second shaft, and a second seal on the second shaft. The method further includes removing at least a portion of a second recoverable gas stream from the second seal, where the second recoverable gas stream includes at least a portion of a second process leak gas stream. The method further includes combining at least a portion of the first recoverable gas stream and at least a portion of the second recoverable gas stream to form a third recoverable gas stream. The method further includes introducing at least a portion of the third recoverable gas stream into the second expander. | 10-01-2009 |
| 20120134785 | AXIAL FLOW GAS TURBINE - An axial flow gas turbine ( | 05-31-2012 |
| 20130177404 | COMPRESSION DEVICE, AND A THERMODYNAMIC SYSTEM COMPRISING SUCH A COMPRESSION DEVICE - This compression device comprises first and second compressors mounted in parallel, a suction line intended to be connected to an outlet of an evaporator, first and second suction conduits arranged for putting the suction line respectively in communication with the admission orifices of the first and second compressors, and an oil level equalization conduit connecting the oil pans of the first and second compressors. The compression device further comprises an oil separator mounted on the suction line or on the second suction conduit, and an oil return conduit arranged for connecting an oil outflow orifice of the oil separator to the oil pan of the first compressor. | 07-11-2013 |
| 20140050569 | GAS SYSTEM FOR COMPRESSING A PROCESS GAS - A gas system has a first compressor stage for compressing a process gas. The first compressor stage includes an intake side and a pressure side. A seal gas is provided outside the first compressor stage in order to prevent process gas from issuing from leaks in the first compressor stage, having at least one second line for returning a gas mixture issuing from the gas system, this mixture including at least of process gas and seal gas. The at least one second line is configured for returning the issuing gas mixture to the intake side of the first compressor stage and/or to a location in the gas system upstream of the first compressor stage. | 02-20-2014 |
| 20140093359 | TURBINE INTRUSION LOSS REDUCTION SYSTEM - Systems and devices configured to reduce windage and mixing losses in a turbine by redirecting and/or aligning a direction of a leakage flow with the flowpath of the main flow of a turbine are disclosed. In one embodiment, a device includes: a base configured to connect to a diaphragm of a turbine; and a radial portion connected to the base and extending radially inboard from the base toward a rotor of the turbine, the radial portion oriented to adjust a direction of travel of a leakage flow of working fluid radially inboard at an angle complementary to a primary working fluid path of the turbine. | 04-03-2014 |
| 20140301833 | Flexible Impeller Pump - A flexible impeller pump includes improved flexible impeller geometry, an impeller shaft having protruding portions that produce a stronger and more durable connection between the impeller shaft and the flexible impeller, a smoother housing cam surface, and wear resistant surfaces that are disposed between end faces of the flexible impeller and adjacent housing end walls. | 10-09-2014 |
| 20150132114 | AXIAL TURBINE - An axial turbine includes a plurality of ribs provided in such a way as to be sandwiched between the diaphragm outer ring and the axial seal fin in the gap between the shroud and the diaphragm outer ring, the ribs being extended from the diaphragm outer ring toward the shroud in the radial direction of the rotor and in the direction of the rotation axis thereof, and a guide plate provided in such a way as to be present along the axial seal fin and a face of the diaphragm outer ring, opposed to the rotor, so as to be extended in the rotation radial direction of the rotor. | 05-14-2015 |
| 20150300323 | SYSTEM AND METHOD FOR COLLECTING FLUID LEAKING FROM A WIND TURBINE COMPONENT - A system and method for collecting fluid leaking from a component of a wind turbine are disclosed. In one aspect, the system may include a flexible sheet ( | 10-22-2015 |
| 20150369075 | ROTATING FLUID MACHINE - Provided is a rotating fluid machine capable of holding down a decrease rate of a circumferential velocity of a leakage fluid in an interspatial flow passage and thereby controlling an unstable fluid force. A steam turbine includes: an interspatial flow passage | 12-24-2015 |
| 415168200 | Leakage through seal between runner or shaft and static part | 10 |
| 20110058933 | DEVICE AND METHOD FOR REDIRECTING A LEAKAGE CURRENT - A device for redirecting a leakage current flowing between a stator and a rotor is disclosed. The device includes a sealing element for interrupting the leakage current, an outlet opening disposed on the rotor, and a guide which is configured to direct the leakage current past the sealing element to the outlet opening. | 03-10-2011 |
| 20110097198 | TURBO MACHINE EFFICIENCY EQUALIZER SYSTEM - A system for a turbo machine is provided, including one or more channels that redirect steam that leaks through the root and/or the tip regions of a stage of the turbine to mix with the high efficiency main steam flow at the pitch region of the turbine where efficiency is the highest. This redirection of the steam results in a significant performance improvement that evens out the efficiency profile resulting in higher average efficiencies. | 04-28-2011 |
| 20130064648 | WATER PUMP - A water pump includes a mechanical seal provided between a housing and a rotary shaft for preventing cooling water from leaking from a whirl chamber. The housing forms a space into which cooling water leaked from between the mechanical seal and the rotary shaft is flown and a water vent for discharging cooling water flown into the space. The housing is joined with a thermostat cover to form a reservoir communicating with the water vent. The reservoir has a drain for releasing evaporated cooling water to the air and a control wall for preventing cooling water remaining as liquid from flowing out through the drain. | 03-14-2013 |
| 20130084165 | INSTALLATION COMPRISING STEAM TURBINE MODULES WITH OPTIMIZED EFFICIENCY - An installation includes a high pressure steam turbine module, a medium pressure steam turbine module, and at least one low pressure steam turbine module, sealing devices being positioned between a rotating turbine shaft and corresponding casings of the various turbine modules, each of the modules include a main chamber in which the turbine is housed. The installation also includes a first collection chamber positioned in the casing of the high pressure module to collect the steam leaks leaving the high pressure module through its sealing device at a pressure greater than atmospheric pressure, and an injection chamber positioned in the casing of the low pressure module and connected by a first circuit to the first collection chamber such that the steam is transferred from the first collection chamber toward the injection chamber, and then toward the main chamber of the low pressure module through its sealing device. | 04-04-2013 |
| 20140037434 | SUBMERSIBLE PUMP HOUSING WITH SEAL BLEED PORTS - A submersible pump housing with seal bleed ports is provided. In an implementation, a pump housing for electric submersible pumps (ESPs), such as a centrifugal ESP, has end seals that are located inside or further inboard toward the high thrust pressure generated by the pump, than the threaded ends of the pump housing. The inboard seals contain and seal off the pump pressure and spare the threaded regions that are more pressure-vulnerable from the pump's high pressure interior, thereby increasing the pressure rating of the entire housing. Leak ports or bleed ports are provided further outboard of the end seals to relieve fluid seeping from inside the submersible pump housing past each end seal. A plate may be added to direct small amounts of fluid escaping from the end seals away from the wellbore casing in which an ESP is situated. | 02-06-2014 |
| 20150300363 | DOUBLE SEAL PUMP WITH INTEGRAL ACCUMULATOR - A double seal pump assembly is provided and comprises a pump housing having an inlet and an outlet. An impeller is in communication with the inlet and outlet. The impeller includes an impeller shaft extending outwardly from the housing. The impeller shaft is adapted to engage a drive shaft of a motor. A housing adapter is mounted onto the housing at a first seal and is configured to secure the impeller to the housing. A motor adapter is mounted to the housing adapter at a second seal thereby defining a cavity therebetween. The motor adapter is configured to mount the motor and the cavity is configured to be filled with a barrier fluid. An accumulator is in fluid communication with the cavity and is adapted to hold a reserve barrier fluid so as to maintain barrier fluid volume and pressure within the cavity. | 10-22-2015 |
| 20160130968 | PLATFORMS WITH LEADING EDGE FEATURES - A platform includes a platform body. The platform body has an airfoil support surface, an axially extending base surface opposite the airfoil support surface, and a leading edge. The leading edge includes an upstream extending flange with a raised portion and a trough portion downstream of and radially inward from the raised portion. The raised portion and the trough portion are for holding a vortex of fluid flow. The upstream extending flange includes a converging surface connecting the upstream extending flange to the base surface. The converging surface converges in a direction toward the axially extending base surface and is at an angle relative to the base surface. | 05-12-2016 |
| 20160169018 | TURBINE EXHAUST SEAL | 06-16-2016 |
| 20160186665 | GAS TURBINE SEALING - A turbine in a gas turbine engine that includes a stator blade and a rotor blade having a seal formed in a trench cavity. The trench cavity may include an axial gap defined between opposing inboard faces of the stator blade and rotor blade. The seal may include: a stator overhang extending from the stator blade toward the rotor blade so to include an outboard edge and an inboard edge and, defined therebetween, an overhang face; a rotor outboard face extending radially inboard from a platform edge, the rotor outboard face opposing at least a portion of the overhang face across the axial gap of the trench cavity; and a first axial projection extending from the rotor outboard face toward the stator blade. The stator overhang and the first axial projection of the rotor blade may be configured so to axially overlap. | 06-30-2016 |
| 415168400 | Means specific to axial flow runner | 1 |
| 20130330179 | SHROUD FOR A ROTARY MACHINE AND METHODS OF ASSEMBLING SAME - A shroud for a turbine and a method of assembling is provided. The turbine includes a housing, a rotatable shaft and a bucket extending outward therefrom. The shroud includes an alignment member which is coupled to the housing, wherein the alignment member includes a first end, a second end and a body extending between the first and second ends. The second end includes an arcuate portion to facilitate fluid flow downstream from the bucket. The shroud further includes a seal coupled to the body to facilitate sealing a gap defined between the bucket and the body. | 12-12-2013 |
