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Matches 1 - 50 out of 24,679

Document Document Title
WO/2018/089057A2
A method of preventing standing waves in an installed gas turbine having a fan, having a fan speed, and a compressor, having a compressor speed, includes correcting the fan and compressor speeds for temperature and monitoring the correct...  
WO/2018/089129A1
A controllable magneto-rheological device includes an annular cylinder (70) formed by inner (72) and outer (74) walls connected at first and second opposing ends and forming an inner shaft (76) configured to receive an operational compon...  
WO/2018/082907A1
The invention relates to a sealing segment (11) for forming a sealing ring of a rotor of a gas turbine. The T-shaped sealing segment comprises a central anchoring section (13) that extends circumferentially and radially and has an adjoin...  
WO/2018/082908A1
The invention relates to a sealing segment (11) for forming a sealing ring of a rotor of a gas turbine and to a rotor equipped with corresponding sealing segments (11). The sealing segment (11) comprises a central anchoring section (13) ...  
WO/2018/085213A1
The invention relates to a turbine having variable turbine geometry for use in a combustion engine, whereby the turbine comprises a bearing housing, a turbine housing and a cartridge, which features a vane bearing ring for supporting a p...  
WO/2018/082837A1
The invention relates to a housing arrangement (10) for a turbomachine, comprising an inner housing (12), an outer housing (14) which encloses the inner housing (12) at least partially, and a sealing ring (16) for radial sealing between ...  
WO/2018/085219A1
A flanged component (70) for a gas turbine engine (100) is disclosed herein. The flanged component (70) includes a flange body (79) with a flange mating surface (71) and a plurality of threaded features. Each threaded feature (72) includ...  
WO/2018/080418A1
Clevis-type pin attachment mounting system (200) accommodates varying thermal expansion rates between ring segments (202) and other ring-segment support components within a combustion turbine engine casing (22). Through-apertures (218) i...  
WO/2018/079277A1
An air turbine driving spindle (200) is provided with a rotating shaft (1), a bearing member (50), an outer member (65), and an O ring (24). The O ring (24) supports the bearing member (50) against the outer member (65) along the radial ...  
WO/2018/079805A1
A steam turbine exhaust chamber (14) having: a casing (15); an inside flow guide section (22) provided inside the casing (15) so as to demarcate an outside boundary of a diffuser passage (18) communicating with a final-stage blade outlet...  
WO/2018/077839A1
The gas turbine system (101) comprises: a compressor section (10) with a main inlet, a main outlet, and a bleed outlet (15), a combustor section (20) with a main inlet fluidly connected to the main outlet of the compressor section (10), ...  
WO/2018/074593A1
The present invention has an outer casing (19), a first valve (28) that adjusts the opening of a first steam outlet (54), and a second valve (32) that adjusts the opening of a second steam outlet (55), said outer casing including: the fi...  
WO/2018/073996A1
A steam turbine system equipped with: a steam turbine having a turbine rotor that rotates centered around a rotary shaft extending in the axial direction, an inner compartment housing the turbine rotor, and an outer compartment housing t...  
WO/2018/074312A1
Provided is a method for bonding dissimilar metals to each other, the method comprising: dissimilar metal layer-forming steps (P2), (P3), (P4) for supplying, on the surface of a first material to be bonded that is formed of a first metal...  
WO/2018/072895A1
The invention relates to a steam strainer (30) having a sieve surface with an essentially cylindrical or conical design and having a plurality of sieve openings (34) for the passage of steam, which are formed in a sieve casing (32) of th...  
WO/2018/072860A1
The invention relates to a turbine (10) for a turbocharger, having a turbine casing (12) and having a turbine wheel (14), which is accommodated in a rotatable manner in the turbine casing (12), has a plurality of runner blades (20) and c...  
WO/2018/074592A1
A steam turbine (1): having an inner casing (3) having an inner casing main body (15) forming a first main flow path (11) to which steam (S1) is supplied from an inner introduction port (16); an outer casing (5) having an outer casing ma...  
WO/2018/073908A1
This inspection assistance device is provided with a damage drawing input unit for receiving input of a damage drawing that is a drawing expressing damage to an object of inspection, a display unit for superimposing and displaying the da...  
WO/2018/073210A1
A method of machining a tip (512) profile of a blade (130, 140) for a turbomachine is provided. The method comprises coupling the blade (130, 140) to a component (110, 112, 114, 120, 124) of the turbomachine; supporting the component (11...  
WO/2018/068880A1
The invention relates to an exhaust-gas guide section for a turbocharger, comprising an inlet channel (3), through which flow can pass, and an outlet channel (9), through which flow can pass, wherein the inlet channel (3) is connected to...  
WO/2018/071174A1
A maintenance apparatus includes a flexible carriage configured to anchor between adjacent airfoils of a turbine assembly. The maintenance apparatus includes a maintenance tool operably coupled with the flexible carriage. The maintenance...  
WO/2018/068303A1
A water wash system (10) for a gas turbine engine includes a pump (50) configured to receive a flow of wash liquid and pressurize the flow of wash liquid. The water wash system additionally includes a nozzle distribution assembly (56) fl...  
WO/2018/070797A1
A gas turbine according to the present invention comprises: a strut assembly comprising an inner ring; an inclined part comprising a first end connected to the inner ring, a second end disposed on the side opposite the first end, and a f...  
WO/2018/066643A1
This method for producing turbine vane includes a brazing step in which a turbine vane substrate having a brazing material positioned thereupon is heated to melt the brazing material and bond the same to the substrate, a stabilization st...  
WO/2018/066644A1
This method for producing turbine vane includes a brazing step in which, in a state in which the substrate of a turbine vane having a brazing material positioned thereupon is positioned within a predetermined furnace having a heater, the...  
WO/2018/064793A1
A wastewater collection system of a water wash system includes a collection duct configured to attach to a gas turbine engine for receiving a mixture of air and wash liquid from the gas turbine engine during washing. The wastewater colle...  
WO/2018/066392A1
This method for producing turbine vane comprises: a step for forming, on the surface of the substrate of a turbine vane formed using a Ni alloy material, an undercoat using a metal material having a higher oxidation resistance than the s...  
WO/2018/063221A1
A method includes mounting a hollow cylinder on a turntable, positioning an additive-manufacturing deposition tool at a surface of the hollow cylinder, and rotating the hollow cylinder on the turntable while depositing material on the ho...  
WO/2018/060595A1
The invention relates to a lubricated enclosure (A) for an aircraft turbine engine, comprising a drained roller bearing (28) provided with drainage orifices (34), as well as a lubricant ejector (60) intended to limit the retention of lub...  
WO/2018/063667A1
A fixture (210) for restraining a wheel (17) of a turbomachine. The fixture comprises a dovetail section (320) adapted for insertion into a dovetail slot of the wheel. A mounting section (330) is located adjacent to, or formed integrally...  
WO/2018/059764A1
Guide blade carrier, turbine casing and turbine The invention is directed to a guide blade carrier (1) for a turbine (30), the guide blade carrier (1) separating an upstream volume (32) from a downstream volume (33) within the turbine (3...  
WO/2018/054690A1
The invention relates to a device (1) for assembling and disassembling a component (11) of a gas turbine (10), comprising a rail system (20) with at least two running rails (21). A carriage (30) which can be pushed on the running rails (...  
WO/2018/055825A1
A performance estimation device according to one aspect of the present disclosure outputs, on the basis of a control input value for controlling a target device and a sensor measurement value measured by a sensor disposed in the target d...  
WO/2018/055672A1
This oil console equipment comprises: a first lubrication oil mist collection device (48) provided to a first atmospheric escape pipe (46) so as to extend vertically, the first lubrication oil mist collection device (48) including a firs...  
WO/2018/055299A1
The invention relates to a system for deoiling an air-oil pressurising mixture (11, 12) for pressurised enclosures (13) of a turbine engine, said system comprising: at least one centrifugal degasser (20); at least one mechanical casing (...  
WO/2018/054631A1
By using a water-based liquid mixture (13) containing amino acids, the cavities (10) of a hollow component (1) can be filled very easily and very quickly, while nevertheless providing the internal structure (22) with adequate protection....  
WO/2018/051080A1
A radial flow gas turbine generator (10) where the gas turbine generator (10) includes a shaft (30) having a rotor (20) of the generator (10), a compressor wheel (16) and a turbine wheel (18) fixed thereto. The shaft (30) is supported fo...  
WO/2018/052509A1
A turbomachine assembly includes annular stator (59) surrounding rotor (44) circumscribed and rotatable about centerline axis. One or more non-axisymmetric partial arc annular circular stiffeners (60) are disposed around and on stator an...  
WO/2018/051245A2
The present invention provides a turbine shaft bearing apparatus, comprising two axially spaced, inlet side and outlet side bearings for providing support to a turbine shaft to which are connected a plurality of turbine wheels such that ...  
WO/2018/051245A3
The present invention provides a turbine shaft bearing apparatus comprising inlet side and outlet side bearings for providing support to a turbine shaft to which are connected a plurality of turbine wheels such that the turbine shaft, th...  
WO/2018/046423A1
The invention relates to methods for clear position determination and identification of a turbine blade (11) of a high-pressure turbine stage (10) of a gas turbine (1), particularly an aircraft engine, in the mounted state. The method fo...  
WO/2018/046178A1
The invention relates to a gas turbine (1) having a turbine (2) comprising a turbine casing (3), an outer (4) and inner casing part (5) between which a hot gas flows when the gas turbine (1) is in operation, wherein an annular duct (6) i...  
WO/2018/047523A1
Provided is a coating method, a coating film, and a turbine shroud. The present invention includes: a slurry deposition step of depositing a slurry containing a coarsely particulate ceramic and a finely particulate ceramic on a base mate...  
WO/2018/046209A1
The invention relates to a machining device (13) for machining a rotor arranged in a turbine housing which consists of two parts, thereby forming a joint (11), in situ while the upper housing half is removed, comprising the following: - ...  
WO/2018/042649A1
This steam turbine assembling method comprises: an upper half assembling step for disposing an upper half partition plate (31) having an upper half partition plate division surface (31X), on the inner peripheral side of an upper half cas...  
WO/2018/042648A1
This steam turbine assembling method comprises: an upper half assembling step for disposing an upper half partition plate (31) having an upper half partition plate division surface (31X), on the inner peripheral side of an upper half cas...  
WO/2018/041555A1
Overall, the invention relates to a seal segment (10) for a turbine and to an assembly for sealing the gaps between seal segments (10) and stator vanes of a turbine. The seal segments comprise a plate-shaped wall (12), the first lateral ...  
WO/2018/043547A1
The present invention is provided with: a marker 6b that is provided in the rotation direction on the outer circumferential surface 6a of a rotor blade and has a different reflectance than the outer circumferential surface 6a; an optical...  
WO/2018/044266A1
An impingement cooling system for a gas turbine engine includes an initial impingement surface (10) with a centrally located opening (12). A plurality of channels (14) and plurality of sub-channels (22) extends radially outward from the ...  
WO/2018/038507A1
Disclosed is a gas turbine blade. The gas turbine blade according to one embodiment of the present invention comprises: a turbine blade (33) provided in a gas turbine; and cooling units (110), each having a cooling channel (110) for cool...  

Matches 1 - 50 out of 24,679