Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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03/19/2008 | CN101144542A Shaft seal using shingle compliant-plate members |
03/18/2008 | US7344357 Methods and apparatus for assembling a rotary machine |
03/13/2008 | WO2008028792A1 Turbine engine and method of operating the same |
03/13/2008 | US20080063529 Undercut fillet radius for blade dovetails |
03/13/2008 | US20080063517 Fan case abradable drainage trench and slot |
03/13/2008 | DE102006038753A1 Anordnung zur Laufspaltoptimierung für Turbomaschinen Arrangement for running gap optimization of turbomachinery |
03/12/2008 | EP1898054A1 Gas turbine |
03/12/2008 | EP1898050A2 Attenuation and sealing system for turbine blades |
03/12/2008 | CN201034029Y Novel low-pressure saturated steam engine |
03/12/2008 | CN100374706C Process for replacing an abradable on the fan case of a turbojet |
03/12/2008 | CN100374689C Method and device for sealing variable blade component of gas-turbine |
03/11/2008 | US7341426 Gas turbine engine blade tip clearance apparatus and method |
03/11/2008 | US7341425 Axial flow compressor |
03/11/2008 | US7341380 Installation layout for two coaxial shaft lines |
03/08/2008 | CA2600788A1 Turbine blade tip gap reduction system for a turbine engine |
03/08/2008 | CA2600170A1 Fan case abradable |
03/08/2008 | CA2598329A1 Rim seal for a gas turbine engine |
03/07/2008 | CA2599799A1 Fan case abradable drainage trench and slot |
03/06/2008 | WO2008025749A1 Sealing means of adjustable guide vanes |
03/06/2008 | US20080056890 Simple axial retention feature for abradable members |
03/06/2008 | US20080056889 Angel wing abradable seal and sealing method |
03/05/2008 | EP1895108A2 Angel wing abradable seal and sealing method |
03/05/2008 | EP1895107A1 Exhaust gas turbine with segmented shroud ring |
03/05/2008 | EP1895106A1 Sealing of variable guide vanes |
03/05/2008 | EP1895095A1 Turbine engine and method of operating the same |
03/05/2008 | EP1893846A1 Ring seal attachment system |
03/05/2008 | CN101135378A Variable clearance positive pressure packing ring and carrier arrangement with coil type spring |
03/05/2008 | CN101135248A Variable clearance positive pressure packing ring and carrier arrangement with leaf springs |
03/04/2008 | US7338253 Resilient seal on trailing edge of turbine inner shroud and method for shroud post impingement cavity sealing |
02/29/2008 | CA2598259A1 Simple axial retention feature for abradable members |
02/28/2008 | WO2007079940A3 Method and device for the recuperation of energy from the heat content of a process gas flow |
02/28/2008 | US20080048399 Leaf Seal Arrangement |
02/27/2008 | EP1892442A1 Brush seal for a turbomachine |
02/27/2008 | EP1892381A2 Sealing arrangement |
02/27/2008 | EP1891303A2 A turbine part of a turbocompressor and a method of avoiding carbon build-up in the turbine part of a turbocompressor |
02/27/2008 | EP1891301A1 Adjusting shaft arrangement of a turbocharger |
02/27/2008 | CN101131101A Angel wing abradable seal and sealing method |
02/26/2008 | US7334984 Turbine shroud assembly with enhanced blade containment capabilities |
02/26/2008 | US7334983 Integrated bladed fluid seal |
02/26/2008 | US7334980 Split ring retainer for turbine outer air seal |
02/26/2008 | US7334799 Sealing device for a turbocharger |
02/26/2008 | US7334331 Methods and apparatus for machining components |
02/26/2008 | US7334328 Method of manufacturing axis seals having reduced gas leakage properties and a rotary machine using axis seals |
02/26/2008 | US7334311 Method of forming a nested can brush seal |
02/21/2008 | WO2008020002A1 Brush seal for a turbo-machine |
02/21/2008 | WO2008019657A2 Arrangement for optimising the running clearance for turbomachines |
02/21/2008 | US20080044284 Segmented fluid seal assembly |
02/21/2008 | US20080044278 Rotor disc assembly with abrasive insert |
02/21/2008 | US20080042366 Compliant Plate Seals for Turbomachinery |
02/21/2008 | CA2660368A1 Arrangement for optimizing the running clearance for turbomachines |
02/20/2008 | EP1890059A1 Compliant plate seals for turbomachinery |
02/20/2008 | EP1890011A1 Axial flow turbine with slotted shroud |
02/20/2008 | EP1890010A2 Ceramic turbine shroud assembly |
02/20/2008 | EP1890009A2 Turbine shroud thermal distortion control |
02/20/2008 | EP1890008A2 Rotor blade |
02/20/2008 | EP1888905A1 Seal arrangement for a fan rotor assembly of a tip tubine |
02/20/2008 | EP1888880A1 Gas turbine with a gap blocking device |
02/20/2008 | CN201025075Y Low diameter gas sealer for steamship engine |
02/20/2008 | CN101126449A Compliant plate seals for turbomachinery |
02/20/2008 | CN101126329A A variable clearance packing ring |
02/20/2008 | CN101126328A Steam turbine low-pressure end outer vapor lock axial direction positioning device |
02/20/2008 | CN100370114C Steam seal gland of steam turbine |
02/19/2008 | US7331755 Method for coating gas turbine engine components |
02/14/2008 | WO2008017681A1 Axial turbine with slotted cover ring |
02/14/2008 | US20080038108 Axial Flow Turbine with Overspeed Preventing Device |
02/14/2008 | US20080036155 Ferrofluid Seal Unit Used on Vertical Thermal Processing Furnace System for Semiconductor Wafer |
02/13/2008 | EP1887191A2 Cooling of a shroud hanger assembly of a gas turbine engine |
02/13/2008 | CN100368712C Sealer |
02/13/2008 | CN100368657C Labyrinth seal in a stationary gas turbine |
02/13/2008 | CN100368656C Combined honeycomb and brush type airtight packing of steam sealing device |
02/07/2008 | US20080031730 Bearing for variable pitch stator vane |
02/07/2008 | US20080029968 Nested can brush seal |
02/07/2008 | DE102007035236A1 Turbinenschaufelspitzendeckband Turbine blade tip shroud |
02/06/2008 | CN100366866C Turbine bucket damper pin |
02/05/2008 | US7326033 Turbomachine blade |
02/05/2008 | CA2291606C Dual-contact brush seal |
01/31/2008 | WO2008011864A1 Gas turbine with a peripheral ring segment comprising a recirculation channel |
01/31/2008 | US20080025842 Turbine vane with removable platform inserts |
01/31/2008 | CA2657190A1 Gas turbine with a peripheral ring segment comprising a recirculation channel |
01/30/2008 | EP1882822A2 Cooled exhaust liner assembly for a gas turbine |
01/30/2008 | EP1882814A2 Turbine vanes with airfoil-proximate cooling seam |
01/30/2008 | EP1882086A2 Gland leakage seal system |
01/30/2008 | EP1299620B1 Sealing system for gas turbine |
01/30/2008 | CN101113677A Air suction labyrinth type seal element |
01/29/2008 | US7322101 Turbine engine disk spacers |
01/24/2008 | US20080019836 Damping Arrangement for Guide Vanes |
01/23/2008 | EP1881160A2 Seal for an annulus filler between fan blades |
01/23/2008 | EP1881159A1 A fan blade for a gas turbine engine |
01/23/2008 | CN101109082A Ultra-temperature BaPr2Ti3+xO10+Y sealing coating material and method of preparing the same |
01/22/2008 | US7320574 Turbomachine |
01/22/2008 | US7320468 Sealing arrangement |
01/22/2008 | CA2461699C Hybrid ceramic material composed of insulating and structural ceramic layers |
01/22/2008 | CA2243032C Apparatus for heating or cooling a circular housing |
01/17/2008 | US20080014077 Seal between relatively moveable members |
01/17/2008 | US20080012237 Dynamic seal for use in high-speed turbomachinery |
01/17/2008 | DE10357690B4 Verwenden thermischer Bildgebung zum Verhindern von Wirkungsgradverlust bei einer Dampfmaschine Using thermal imaging for preventing loss of efficiency in a steam engine |
01/16/2008 | EP1878880A1 Cross flange seal for a pressure vessel, especially for a turbomachine casing |
01/16/2008 | EP1878876A2 Gas turbine abradable seal |
01/16/2008 | EP1878875A2 A seal arrangement |
01/16/2008 | EP1432571B1 Hybrid ceramic material composed of insulating and structural ceramic layers |