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Matches 1 - 50 out of 22,342

Document Document Title
WO/2017/005901A1
The present invention relates to an apparatus for handling a turbomachine part, particularly during disassembling and reassembling operations. More specifically, the present invention relates to an apparatus for handling the stator cone(...  
WO/2017/007802A1
A support structure for rotating machinery is provided. The support structure may include a first main hollow support member and a second main hollow support member, each having a longitudinal axis and a square cross-section. The second ...  
WO/2017/006045A1
The invention relates to an assembly for a turbine (22) of a turbine engine, comprising a casing (32) and an annular duct (34) surrounding the casing, which can be connected to means for supplying cooling air, and having a radially inner...  
WO/2017/004725A1
A boundary layer turbine comprising a housing having an inlet and an outlet, the inlet receives a flow of pressurized fluid; a shaft extending longitudinally through the housing and journaled for rotation about its longitudinal axis rela...  
WO/2017/006927A1
Provided is a high-strength, heat-resistant, Ni-base alloy member comprising Co: 5 to 12%, Cr: 5 to 12%, Mo: 0.5 to 3.0%, W: 3.0 to 6.0%, Al: 5.5 to 7.2%, Ti: 1.0 to 3.0%, Ta: 1.5 to 6.0%, Re: 0 to 2.0%, and C: 0.01 to 0.20%. The balance...  
WO/2017/001141A1
The invention relates to a method for using a starter (1) for starting a gas turbine (100) rotor (11) at a standstill, said starter (1) having a lifting device (5) which has a hydraulically adjustable height and on which at least one bea...  
WO/2017/001029A1
The invention relates to an engine structure (200) forming an adapter for connecting a turbocharger unit (100) to a cylinder block (22) of an internal combustion engine (10). The engine structure (200) comprises a set of attachment means...  
WO/2017/003318A1
The invention relates to mechanical engineering. The rotary engine comprises a casing, in a groove of which a bladed rotor is mounted on a shaft, wherein the above-mentioned casing has at least one input opening formed along a tangent to...  
WO/2016/208211A1
The vibration reduction damper (13) according to the present disclosure is disposed in the interior of a center vent tube (12) having vent holes (12a) which penetrate in the radial direction, and is provided with a sliding part (13a) tha...  
WO/2016/206972A1
The invention relates to an automation system that determines the theoretical maximum rate of cooling of a steam turbine (2) and operates a steam generator (6) in such a way that the thermal energy of the steam does not exceed nor drop b...  
WO/2016/206974A1
The invention relates to a method for rapidly cooling a steam turbine (2), wherein ambient air is introduced into the steam turbine (2) through a valve via an evacuation unit (23), resulting in cooling of the steam turbine (2), the rate ...  
WO/2016/203767A1
This expansion turbine device is provided with a main body, a turbine impeller, a brake impeller, a rotation shaft, a hydrostatic gas bearing, a first labyrinth seal, a mixed gas discharge path, a first back pressure regulating valve, a ...  
WO/2016/203768A1
This expansion turbine device is provided with a main body, a turbine impeller, a brake impeller, a rotation shaft, a hydrostatic gas bearing, a labyrinth seal, a gas supply path, and a mixed gas discharge path, wherein the pressure of t...  
WO/2016/199422A1
An exhaust gas diffuser is provided with: a plurality of struts extending through an inner cylinder and an outer cylinder and connecting a bearing support which is disposed inside the inner cylinder and a structure which is disposed outs...  
WO/2016/201179A1
A supercharger constructed in accordance to one example of the present disclosure includes a housing, a first rotor, a second rotor and a rotor shaft assembly. The first and second rotors are received in cylindrical overlapping chambers ...  
WO/2016/201023A1
Various methods and systems are provided for controlling a tip clearance between a shroud and blade of a turbocharger turbine. In one embodiment, a method for an engine including a turbocharger comprises, selectively adjusting a flow of ...  
WO/2016/198806A1
The invention relates to an assembly comprising: - a turbomachine exhaust case (110) that includes an external sleeve and an internal sleeve inside the former, both sleeves extending concentrically about a turbomachine axis, and also inc...  
WO/2016/199319A1
[Problem] To provide a turbine that has a simple structure, that is composed of a CMC and achieves a wide range of gas flow passages while suppressing thermal stress acting on turbine stator blades, and that can consequently realize furt...  
WO/2016/198216A1
An assembly/disassembly apparatus (1) for flanged mechanical device comprising: a main body (2) provided with a rear abutment sector (21) having at least a seat (22); a coupling pin (4) housed in part in the seat (22) and extending from ...  
WO/2016/194593A1
Provided is an air turbine drive spindle in which movement of the thrust position of a rotating shaft is sufficiently inhibited. The air turbine drive spindle is provided with: a rotating shaft (1) comprising a shaft section (1A) and a t...  
WO/2016/193596A1
A device for cooling a rolling bearing (112), in particular for a turbine engine, the device comprising an annular bearing support (124) comprising a substantially cylindrical wall (134) of which an inner peripheral face (136) is configu...  
WO/2016/194677A1
A sealing device for minimizing leakage of a fluid flowing through an annular gap between a stationary member and a rotating member of a rotating machine comprises an annular fixed fin provided to the annular gap, and an annular movable ...  
WO/2016/193173A1
A combined bearing (25) for a turbomachine (1) is disclosed. The combined bearing (25) comprises in combination: a radial bearing member (28), a thrust bearing member (26) and a bearing-fluid impeller (49) of a bearing-fluid boosting pum...  
WO/2016/193112A1
The invention relates to a method for cleaning a jet engine by means of a cleaning medium that contains solids, which are introduced into the engine by means of at least one dispensing device (11). According to the invention, the cleanin...  
WO/2016/195022A1
[Problem] To provide a heat utilizing device with which it is possible to achieve a further reduction in size while improving ease of maintenance, ease of assembly, and reliability. [Solution] This heat utilizing device is provided with ...  
WO/2016/189223A1
The present invention relates to a turbine ring assembly including a plurality of ring sectors (1) made of a composite material having a ceramic matrix forming a turbine ring, and a ring-supporting structure (2) including two annular fla...  
WO/2016/190760A1
A flow mixing lobe (54) for an exhaust diffuser (30) includes a first flange member (64) having a first leading end (72), a first trailing end (73), and an intermediate portion (74) extending therebetween. A second flange member (65) inc...  
WO/2016/189234A1
Turbine engine unit for lubricating a bearing holder A turbine engine unit is provided, including: an inter-turbine housing that includes a hub (1) including a bearing holder, a ferrule (2) extending around and at a distance from the hub...  
WO/2016/189224A1
The invention relates to a turbine ring assembly which comprises a plurality of ring sectors (10) made of a composite material with a ceramic matrix forming a turbine ring (1) and a ring-supporting structure (3) including two flanges (32...  
WO/2016/189222A1
A turbine ring assembly comprises a plurality of ring sectors (10) made of ceramic matrix composite material, forming a turbine ring (1) and a ring support structure (3) secured to a turbine casing (30) and comprising two annular flanges...  
WO/2016/189026A1
The present invention concerns a method for assembling equipment on a support (100) of a turbo-machine. The method comprises the step of mechanically assembling the equipment to a part (101) of said support (100) by means of a fastening ...  
WO/2016/189215A1
A turbine ring assembly comprises a plurality of ring sectors (10) made from a ceramic matrix composite material forming a turbine ring (1) and a ring support structure (3) comprising two annular flanges (32, 36), each ring sector (10) h...  
WO/2016/184409A1
A miniature turbine generator, comprising a turbine machine (1), a cooling fan (2), a motor (3), two radial bearings (4a, 4b) and a thrust bearing (5), the radial bearings (4a, 4b) being mixed-type dynamic pressure gas radial bearings, t...  
WO/2016/185732A1
A guide surface which expands to the outer peripheral side as the guide surface extends from the upstream side to the downstream side is formed on a support section. A guided surface which expands to the outer peripheral side as the guid...  
WO/2016/184408A1
An ultra-high speed turbine generator, comprising a turbine machine (1), a cooling fan (2), a motor (3), two radial bearings (4a, 4b) and a thrust bearing (5), the radial bearings (4a, 4b) being groove-type dynamic pressure gas radial be...  
WO/2016/184678A1
The invention concerns a steam turbine foundation (10) adapted to support a steam turbine system (100). The steam turbine foundation (10) comprises a base plate (12), a first support (20), a second support (30) and a third support (40). ...  
WO/2016/185361A1
A turbine (100) for expanding a working fluid in an organic Rankine cycle, comprising a casing (10), inside of which at least a statoric group is accommodated, a turbine shaft (15) contained inside a tube member (20) and carrying at leas...  
WO/2016/182461A1
A rotor turning system (100) for turning a rotor is provided. The system (100) includes a rotary driver (110) including a rotating drive shaft (112). A removable rotor grasping element (120) is configured to frictionally grasp at least a...  
WO/2016/180690A1
The invention relates to a method for cleaning a compressor (10), having at least one compressor stage (11, 12, 13) and serving to compress an operating medium (14), wherein, in at least one compressor stage (11, 12, 13) of the compresso...  
WO/2016/181307A1
The invention relates to a turbine, in particular a combustion gas turbine, which drives a high-speed generator for generating electricity, said turbine having a high efficiency. The turbine has at least one combustion chamber (6), which...  
WO/2016/180808A1
A containment sleeve (23) of a turbomachinery bearing (22), the sleeve (23) comprising a body defining a surface (23A) configured to support a turbomachinery bearing (22), and at least a first (25A) and a second hole (25B) opening on sai...  
WO/2016/180697A1
The invention relates to a compressor (10) for compressing a working medium, comprising at least one rotor-side rotor-blade ring (12, 13) and at least one stator-side guide-vane ring (15, 16), wherein the or each rotor-blade ring has a p...  
WO/2016/177880A1
A turbomachinery gasket (20) comprising at least a first curved elongated element having a coupling part (22) configured to cooperate with a tubular assembly (30) in order to keep the gasket (20) in position on the tubular assembly (30),...  
WO/2016/178664A1
An improved layout of cooling fluid conduits in a turbine transition duct is provided. The transition duct (10) may include a transition body made with a multi-panel arrangement (12, 14) that defines a passage to route a hot combustion g...  
WO/2016/177644A1
There is disclosed a turboshaft engine (10) having a principal rotational axis and comprising a power turbine (16), a tail bearing housing (18) and an exhaust collector (19) arranged in axial flow series along said axis. The tail bearing...  
WO/2016/179608A2
An intershaft seal assembly (30) for use between an inner shaft (32) and an outer shaft (31) rotatable within a turbine engine is presented. The seal assembly (30) includes a sealing ring (33), an inner ring (39), and a pair of end rings...  
WO/2016/174341A1
The invention relates to a turboshaft engine for a helicopter, comprising a case (5) inside which a gas generator (6) and a turbine (7) are accommodated, the turbine (7) being mounted on a power shaft (8) that extends along a longitudina...  
WO/2016/175753A1
A fuel delivery system (10) for a gas turbine engine (12) that employs a technique for purging fuel delivery tubes (82). The fuel delivery system includes a multifunction valve (64) that has a flow through position (66) and a bi-directio...  
WO/2016/169751A1
The invention relates to a lifting and transport apparatus (1) for lifting and transporting a heavy load (2), comprising a frame (4) that can be moved back and forth at least in a horizontal displacement direction (X), the frame having f...  
WO/2016/170165A1
The gas turbine engine (3) comprises a compressor section (9) configured for compressing combustion air, a combustor section (15) and a turbine section (21). The turbine section (21) comprises a turbine rotor (41) with a bladed wheel (43...  

Matches 1 - 50 out of 22,342