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