Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
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08/16/1994 | US5337568 Micro-grooved heat transfer wall |
08/16/1994 | CA1331491C Shrouded turbine blade vibration monitor |
08/11/1994 | DE4303137A1 Method for removing ceramic layers on metal components |
08/10/1994 | EP0609979A1 Balanced rotor for a gas turbine engine |
08/10/1994 | EP0609795A1 Ceramic insulation layer on metallic piece parts and method of manufacture |
08/09/1994 | US5336560 Gas turbine elements bearing alumina-silica coating to inhibit coking |
08/04/1994 | WO1994017303A1 Windmill blade |
08/04/1994 | WO1994017285A1 Turbine vane having dedicated inner platform cooling |
08/02/1994 | US5334462 Ceramic material and insulating coating made thereof |
08/02/1994 | US5333995 Wear shim for a turbine engine |
07/28/1994 | DE4301656A1 Blade and reinforcing strip assembly esp. for gas turbine |
07/26/1994 | US5332357 Stator vane assembly for controlling air flow in a gas turbine engien |
07/21/1994 | WO1994016200A1 Free standing turbine disk sideplate assembly |
07/21/1994 | WO1994012768A3 Coolable airfoil structure |
07/20/1994 | EP0607082A1 Turbomachine rotor with blade attachment by pins |
07/19/1994 | US5330326 Method for producing profiled parts by grinding and a turbomachine blade produced thereby |
07/19/1994 | US5330324 Annular gasket disposed at one axial extremity of a rotor and covering blade feet |
07/12/1994 | US5328331 Turbine airfoil with double shell outer wall |
07/12/1994 | US5328326 Impulse turbine with a drum rotor, and improvements to such turbines |
07/12/1994 | US5327719 Circuit for ventilating compressor and turbine disks |
07/12/1994 | CA1330638C Thermal barrier coating system |
07/09/1994 | CA2113062A1 Steam turbine vane airfoil |
07/07/1994 | WO1994015000A1 Columnar ceramic thermal barrier coating with improved adherence |
07/07/1994 | WO1994014995A1 Heat treatment to reduce embrittlement of tatanium alloys |
07/06/1994 | EP0605155A1 Steam transfer arrangement for turbine bucket cooling |
07/06/1994 | EP0605153A1 Steam and air cooling for stator stage of a turbine |
07/06/1994 | EP0605152A1 Process for producing turbine bucket with water droplet erosion protection and realted product |
07/06/1994 | EP0604754A1 Turbine rotor |
07/06/1994 | CN1025358C Method for mfg. turbine blades |
07/05/1994 | US5326647 Abradable layer for a turbo-engine and a manufacturing process |
07/05/1994 | US5326224 Cooling hole arrangements in jet engine components exposed to hot gas flow |
07/05/1994 | US5326221 Over-cambered stage design for steam turbines |
07/01/1994 | CA2103428A1 Steam transfer arrangement for turbine bucket cooling |
07/01/1994 | CA2103416A1 Steam and air cooling for stator stage of a turbine |
06/29/1994 | EP0604299A1 Blade-hub lamellar connection device, rotor blade and rotor featuring it |
06/29/1994 | CN1025175C Fan blade mount for air plane driving system |
06/24/1994 | CA2111373A1 Blade-hub linkage device with a laminate attachment, rotor blade fitted with such an attachment, and rotor equipped with such blades |
06/23/1994 | WO1994013454A1 Injection mold with heating and cooling phases |
06/22/1994 | EP0602631A1 Method of manufacturing a ring of stator blades, in particular for an axial compressor |
06/22/1994 | EP0602397A1 Instrument for machining the surface of parts inside machine bodies |
06/22/1994 | EP0431019B1 Dual-alloy disk system |
06/16/1994 | DE4242099A1 Appts., esp. gas turbine appts. - having coating on its operating parts in contact with fuel gas or waste gas to reduce pollutant emissions |
06/15/1994 | EP0601119A1 Forward skew fan with rake and chordwise camber corrections |
06/14/1994 | US5320492 Sealing and retaining device for a rotor notched with pin settings receiving blade roots |
06/14/1994 | US5320488 Turbine disk interstage seal anti-rotation system |
06/14/1994 | US5320485 Guide vane with a plurality of cooling circuits |
06/14/1994 | US5320483 Steam and air cooling for stator stage of a turbine |
06/09/1994 | WO1994012774A1 Rotor blade with platform support and damper positioning means |
06/09/1994 | WO1994012773A1 Gas turbine blade damper |
06/09/1994 | WO1994012772A1 Gas turbine blade seal |
06/09/1994 | WO1994012771A1 Turbine airfoil with diffusing pedestals in its trailing edge |
06/09/1994 | WO1994012770A1 Rotor blade with integral platform and a fillet cooling passage |
06/09/1994 | WO1994012769A1 Internally cooled turbine airfoil |
06/09/1994 | WO1994012768A2 Coolable airfoil structure |
06/09/1994 | WO1994012767A1 Airfoil casting core reinforced at trailing edge |
06/09/1994 | WO1994012766A1 Coolable airfoil structure |
06/09/1994 | WO1994012765A1 Rotor blade with cooled integral platform |
06/09/1994 | WO1994012390A2 Coolable rotor blade structure |
06/07/1994 | US5318406 Multipart gas turbine blade |
06/07/1994 | US5318405 Turbine disk interstage seal anti-rotation key through disk dovetail slot |
06/07/1994 | US5318404 Steam transfer arrangement for turbine bucket cooling |
06/01/1994 | EP0447404B1 High temperature turbine engine structure |
06/01/1994 | DE4239710A1 Rotor for steam turbine and current generation - comprises a welded assembly of largely pre-processed components belonging to a modular construction system standardising the rotor parts |
05/31/1994 | US5316866 Coated superalloy component exhibiting oxidation and corrosion resistance |
05/31/1994 | US5316437 Gas turbine engine structural frame assembly having a thermally actuated valve for modulating a flow of hot gases through the frame hub |
05/26/1994 | WO1994011616A1 Cooling of the shroud of a turbine blade |
05/25/1994 | CN1087159A An angle adjustable vane suspension |
05/25/1994 | CN1024703C Turbine Blade of Titanium-based alloy and production method therefor |
05/25/1994 | CN1024702C Blading for reaction turbine blade row |
05/25/1994 | CN1024701C Gas turbine blade and forming method |
05/24/1994 | US5314309 Turbine blade with metallic attachment and method of making the same |
05/24/1994 | US5314307 Gas turbine test airfoil |
05/24/1994 | US5314301 For a gas turbine engine |
05/24/1994 | US5314282 Composite fastener |
05/24/1994 | US5314106 Method for joining steel to aluminum alloy components or titanium alloy components, and turbochargers obtained by the method |
05/24/1994 | US5313786 Gas turbine blade damper |
05/24/1994 | US5313700 Forming a flow directing element for a turbine |
05/24/1994 | CA1329848C Nonsynchronous turbine blade vibration monitoring system |
05/18/1994 | EP0597586A1 Gas turbine engine fan blade assembly |
05/17/1994 | US5312696 Method for reducing fretting wear between contacting surfaces |
05/17/1994 | US5311734 System and method for improved engine cooling in conjunction with an improved gas bearing face seal assembly |
05/11/1994 | WO1994010426A1 Process for the manufacture of a wheel for a turbine with inserted blades and wheel so obtained |
05/11/1994 | EP0596386A1 Adjustable guide vane formed of fiber reinforced plastic |
05/11/1994 | CN1086579A Axial-flow turbine |
05/10/1994 | US5310319 Free standing turbine disk sideplate assembly |
05/10/1994 | US5310318 Asymmetric axial dovetail and rotor disk |
05/10/1994 | US5310317 Rotor blade adapted in a gas turbine engine |
05/10/1994 | US5310312 Gas turbine test airfoil |
05/05/1994 | DE4237052A1 Appts. for repair welding of the tips of guide vanes and runner blades of turbomachines - incorporating notched jaws with an adjustable gap |
05/03/1994 | US5308228 Gas turbine blade comprising layers of composite material |
05/03/1994 | US5308227 Drum rotor for an impulse steam turbine having blades mounted in longitudinal grooves, and an impulse steam turbine including such a motor |
05/03/1994 | CA2013077C Turbine blades |
04/28/1994 | WO1994009264A1 An angle adjustable vane suspension |
04/28/1994 | CA2145416A1 An angle adjustable vane suspension |
04/27/1994 | EP0593736A1 Heat treatment and repair of cobalt-base superalloy articles |
04/26/1994 | US5306897 Heat treatment method and apparatus for turbine blades using flexible heater sleeve |
04/26/1994 | US5306554 Sintering mixture of shrinkable discontinuous ceramic particles and an inorganic filler which expands; counteracts stresses from consolidation; noncracking |
04/26/1994 | US5306120 System to protect against erosion a body subjected to an airflow |
04/26/1994 | US5305520 Method of making fibre reinforced metal component |
04/21/1994 | DE4335598A1 Preventing fouling and increasing power in gas turbine installation - cooling intake air to below zero by turbo cooling unit consisting of compressor, cooler and expansion turbine preceding gas turbine proper |