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Matches 1 - 50 out of 8,077

Document Document Title
WO/2017/067635A1
The invention relates to a controller for an exhaust gas turbocharger comprising an exhaust gas pipe section (2) through which a flow can pass, a bearing section, and a flow-through air guiding section (13), wherein the exhaust gas pipe ...  
WO/2017/069925A1
A trip valve for a steam turbine is provided and a method for upgrading the trip valve. The trip valve (200) includes a valve body (202) defining a cavity (204), a first port (206) and a second port (208). The first and second ports are ...  
WO/2017/063833A1
The invention relates to an adjusting device (1) for actuating an actuator (2) of a turbocharger (7), having - an actuating drive (3) for generating an actuating force; and - a coupling device (4) which is mechanically coupled to the act...  
WO/2017/061421A1
A power generation apparatus 1 has a Rankine cycle 2 in which an evaporator 30 for evaporating a working fluid by a heat source, an expander 40 for expanding the working fluid, a condenser 50 for condensing the working fluid by a cooling...  
WO/2017/060228A1
A valve assembly for use to regulate a flow of steam in a flowpath of a turbine. The valve assembly can be configured with a body 200 that circumscribes a rotor. The body is disposed upstream of the rotor blades. In one implementation, t...  
WO/2017/058726A1
A pneumatic trip system for a turbine includes a valve member; a valve stem connected to the valve member; and an actuator assembly connected to the valve stem. The actuator assembly includes a cylinder; a piston connected to the valve s...  
WO/2017/057260A1
A steam generation device (1) is provided with a sunlight collection device (2) that heats a fluid by sunlight and a gas-liquid drum (31) for storing the liquid and steam of the fluid. The fluid is continuously circulated between the sun...  
WO/2017/051450A1
Waste heat recovery equipment is provided with: an exhaust gas economizer that recovers heat from exhaust gas exhausted from a diesel main engine body to generate main steam; a steam turbine driven by the main steam; an organic fluid hea...  
WO/2017/051672A1
An output device 1 is mounted in a vehicle and has a Rankine cycle 2 wherein a pump 20 that rotates and thereby circulates an operating fluid in the circulation flow path 10, an evaporator 30 that evaporates the operating fluid by means ...  
WO/2017/050501A1
The invention relates to a turbine for an exhaust turbocharger, which exhaust turbocharger has a turbine housing, in which a first and a second flow channel are provided, each of which has an inlet region and an outlet region, wherein a ...  
WO/2017/048568A1
A cartridge for use in a pulse energy enhanced turbine of a turbocharger. At least first and second fixed separating blades (12) are provided between a nozzle ring (6) and a disk (29), the separating blades (12) maintaining separation of...  
WO/2017/048611A1
A number of variations may include a product comprising: a vane lever comprising a first end; a second end; a top surface; and a bottom surface; and an opening defined by an inner surface which extends through the top surface and the bot...  
WO/2017/047356A1
A variable nozzle unit is used in a turbine having a gas inflow passage sandwiched between a first flow passage wall surface and a second flow passage wall surface, the first and second flow passage wall surfaces facing each other, the g...  
WO/2017/048149A1
The invention relates to the energy sector. A device for converting the energy of a drop in the pressure of a gaseous working fluid comprises a housing, a consumer of the mechanical energy generated, and an expansion turbine with a blade...  
WO/2017/036972A1
The invention relates to an exhaust gas turbocharger (11) for an internal combustion engine (10) comprising a first exhaust gas duct (12) and a second exhaust gas duct (13) which are provided to guide the exhaust gases to different cylin...  
WO/2017/038371A1
This gas turbine is provided with an exhaust diffuser (5) in which is formed an exhaust passage (Pe) for channeling exhaust gas from a turbine, and a cooling device (6) for cooling a structure in the exhaust diffuser (5) that faces the e...  
WO/2017/040022A1
The present invention relates to a turbocharger comprising a bearing housing, a turbine housing which is connected to the bearing housing, and a cartridge. The cartridge comprises a blade bearing ring and a disk, wherein a plurality of b...  
WO/2017/030533A1
The subject matter of this specification can be embodied in, among other things, a method for controlling a valve includes providing a valve having an actuator configured to move a valve member between an open valve position and a closed...  
WO/2017/029689A1
The turbine (21) is equipped with: a casing (30); a turbine rotor (90) which is disposed inside the casing (30) so as to penetrate therethrough; rotor vanes (100) which are implanted along the circumference of the turbine rotor (90); an ...  
WO/2017/030027A1
In the present invention a turbine control panel (TCP) (57) performs a pressure-changing operation wherein the pressure of steam introduced into a steam turbine is changed. In addition, a load capacity value calculation unit (70) with wh...  
WO/2017/023559A1
An anti-ice valve, a turbine engine including an anti-ice valve assembly and a method of operating an anti-ice valve where an anti-ice valve has a housing and a valve element configured to control a flow of hot bleed air through the hous...  
WO/2017/013360A1
The invention concerns an aircraft propelled by a turbine engine having contrarotating fans (7, 8), the turbine engine being incorporated at the rear of a fuselage (1) of the aircraft, in the extension of same and comprising at least two...  
WO/2017/013326A1
The invention relates to a stage of variable-pitch blades (110) for a turbine engine, each blade including an impeller (114) which comprises: a first radially inner frustoconical surface (150) in which the cone angle is flared radially i...  
WO/2017/013364A1
The invention relates to an aircraft including a fuselage (1) and a propulsion assembly. Said propulsion assembly includes at least one fan rotor (7, 8) placed behind the fuselage (1) as an extension thereof along a longitudinal axis (XX...  
WO2017008683A1
Aa variable geometry turbine (VGT) for turbochargers incorporates a turbine nozzle having a plurality of vanes, each vane having an airfoil with an inner disc and an outer disc. A first nozzle plate incorporates pockets to receive the in...  
WO/2017/005470A1
The invention relates to an exhaust-gas turbocharger (1) for an internal combustion engine (2) having an intake duct (3) for air and having an exhaust duct (5) and having a turbine (6) arranged in the exhaust duct and having a compressor...  
WO/2017/006010A1
Variable-pitch blade control ring (44) for a turbomachine, comprising an annular body (42) configured to be mounted with the ability to rotate on an annular casing (16) of the turbomachine, said body comprising means (46) of connection t...  
WO/2016/207513A1
The invention relates to a system for controlling variable-setting blades (14) for a turbine engine, which includes at least one control ring (36) mounted rotatably mobile about an annular casing (16) with axis of revolution A, at least ...  
WO/2016/203157A1
The invention relates to a hub (2) of an intermediate casing (1) for a bypass turbomachine comprising: - a bleed stream duct (18), - a bleed valve, comprising a mobile door at the inlet orifice to the bleed stream duct (18), - a set of b...  
WO/2016/203980A1
This compressed air energy storage power generation device 2 is provided with: motors 26a, 26b which are driven by fluctuating input power; a compressor 4 which is mechanically connected to the motors 26a, 26b, and which compresses air; ...  
WO/2016/203979A1
This compressed air energy storage power generation device 2 is provided with: an expansion-side heat medium temperature sensor 40 for measuring the temperature of a heat medium supplied to an expansion-side heat exchanger 16; an expansi...  
WO/2016/198854A1
A flow-control assembly for guiding a flow of fluid having a variable mass flow rate onto a turbine comprising: a turbine comprising a blade and configured to rotate about an axis of rotation; and a flow-guidance element in fluid communi...  
WO/2016/199600A1
A variable geometry turbocharger according to the present invention is provided with a turbine having a variable nozzle unit, and a compressor. The variable nozzle unit has: a unit main body part that is fixed to a turbine housing and ro...  
WO/2016/192890A1
The invention relates to an operating method for a gas turbine (1) by partial-load operation, comprising the following steps: setting of a power setpoint value (LS) for a predefined temperature value (T0); determining the two operating c...  
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/2016/174358A1
The invention relates to a variable pitch stator blade for a turbo machine, comprising an aerofoil, a pivot member configured to cause the blade to pivot relative to a turbo machine casing, and a plate situated between the pivot member a...  
WO/2016/174175A1
A gas turbine drive system in mechanical drive configuration is described. The gas turbine drive system comprises a gas turbine engine (1) drivingly connected to a driven turbomachine (3). The gas turbine engine includes a dry low NOx em...  
WO/2016/170114A1
A turbomachine airfoil component (15) is disclosed, having a leading edge (15L) and a trailing edge (15T). The airfoil component comprises a hole (21) extending from an inlet (21A) positioned at the leading edge (15L) towards the interio...  
WO/2016/166191A4
The invention relates to a guide vane adjustment device for a turbomachine, for rotation about a radial guide vane axis of a plurality of guide vanes that are grouped to a vane ring. Said guide vane adjustment device comprises an input s...  
WO/2016/166191A3
The invention relates to a guide vane adjustment device for a turbomachine, for rotation about a radial guide vane axis of a plurality of guide vanes that are grouped to a vane ring. Said guide vane adjustment device comprises an input s...  
WO/2016/165950A1
The invention relates to a guide vane adjusting device for a turbomachine, namely for rotating multiple guide vanes grouped into a guide vane assembly about guide vane rotational axes of the guide vanes of the guide vane assembly, said r...  
WO/2016/162105A1
The invention relates to a controller for an exhaust gas conductive portion, through which a flow can pass, of a turbocharger. The controller (13) is designed to open and close a bypass channel (11) in the exhaust gas conductive portion ...  
WO/2016/162139A1
The invention relates to a device (100) for detecting the rotational angle of the position of a plurality of adjustable guide vanes (11) of a gas turbine (10), comprising at least three rotational angle sensors (1, 2, 3) at different loc...  
WO/2016/162106A1
The invention relates to a regulating device for an exhaust-gas-conducting section of an exhaust-gas turbocharger, wherein the regulating device (19) is designed for guiding a flow of a fluid into a bypass duct (22), which is formed in t...  
WO/2016/156310A1
The invention relates to a wastegate valve system for an exhaust-gas turbocharger comprising a housing (30), which forms a valve seat, a valve body (28), and an actuating device, by means of which the valve body (28) can be pressed onto ...  
WO/2016/156744A1
The invention relates to an oil jet (10) for a turbine engine, comprising a body (16) including a circulation pipe (18) intended for the flow of a pressurised fluid. The body (16) of the jet (10) comprises a first portion (24) and a seco...  
WO/2016/151849A1
A turbine rotor blade according to an embodiment of the present invention comprises: a hub part that is connected to one end of a rotating shaft; a plurality of main blades that are provided on a peripheral surface of the hub part so as ...  
WO/2016/146282A1
The invention relates to a turbocharger (2) for a motor vehicle, comprising a housing (4) and a valve seat (12) in the housing (4); the valve seat (12) is retained in an interlocking manner in the housing (4) by means of at least one ela...  
WO/2016/136506A1
The present invention is provided with: a steam introduction path (74a) which extracts steam from a steam extraction section (59e) at a midway position of a superheater (37); a steam return path (74b) which returns the steam to a stream ...  
WO/2016/135831A1
Provided is a gas turbine starting device (4) comprising the following: a planetary gear mechanism (11) that includes a sun gear (16), a planetary carrier (18) disposed on the outer circumference of the sun gear (16), and an inner gear (...  

Matches 1 - 50 out of 8,077