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公开(公告)号：US09895643B2
公开(公告)日：2018-02-20
申请号：US14735517
申请日：2015-06-10
发明人： Rikard Håkansson
CPC分类号： B01D47/06 , B01D3/008 , B01D53/504 , B01D53/79 , B01D2247/04 , B01D2247/08 , B01D2247/10 , B01D2251/404 , B01D2258/0283 , F23J15/003 , F23J2215/20 , F23J2215/50 , F23J2219/40 , Y02E20/326
摘要： A wet scrubber (1) useful for cleaning a process gas comprises at least a first spray level system (20) and a second spray level system (26) arranged vertically above the first spray level system (20) in a wet scrubber tower (2). The first spray level system (20) comprises at least one gas-liquid contacting plate (38) which is operative for deflecting absorption liquid, that has been atomized by means of the second spray level system (26) and flowing downward in the wet scrubber tower (2), so deflected absorption liquid (AL) may contact process gas (F) contacted by absorption liquid atomized by the first spray level system (20).
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公开(公告)号：US09890651B2
公开(公告)日：2018-02-13
申请号：US14467752
申请日：2014-08-25
发明人： Sarah Heaven , Shyam Mavani , Jiwen Tao , Stacie Tibos , Vasileios Stefanis , Sascha Justl , Rudolf Kellerer
CPC分类号： F01D11/006 , F01D5/30 , F01D11/00 , F01D11/005 , F05D2240/57 , F05D2240/81 , F05D2250/75
摘要： The invention refers to a blade of a rotary flow machine including an airfoil having a suction surface and a pressure surface joining each other along a trailing and a leading edge. A radially outward directed airfoil tip and a radially inward directed end joining an inner platform connect the airfoil to a shank at a radial end of the airfoil and providing, at least one shank pocket radially encircled by an axially extending portion of the platform. At least one radially extending rim extends from the trailing edge side of the shank and has an essentially radially orientated first slot for receiving a seal. A mount extends radially inwardly from said shank pocket. The first slot has a first aperture on a shank surface orientated in an axial direction.
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公开(公告)号：US09876415B2
公开(公告)日：2018-01-23
申请号：US14657251
申请日：2015-03-13
CPC分类号： H02K15/14 , H02K5/04 , H02K5/14 , Y10T29/49009 , Y10T29/53143
摘要： A tool for assembly of an inner enclosure of a generator or a machine comprises a first part and a second part. The first part comprises a plate with one edge constructed to form a first half-ring. The second part comprises a second half-ring corresponding to the first half-ring of the first part. Upon assembly of the first part and the second part, the first half-ring and the second half-ring form a full-ring to encompass a shaft of the generator or the machine and to connect to an inner enclosure of the generator or the machine.
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公开(公告)号：US20180020560A1
公开(公告)日：2018-01-18
申请号：US15548732
申请日：2015-02-09
发明人： Roman RAUBO , Marek RAUBO
CPC分类号： H05K5/0256 , H05K5/0021 , H05K5/0221 , H05K5/0247 , H05K7/02 , H05K7/1432
摘要： The invention relates to an assembly of modules for an electrical circuit comprising: a module support for at least two modules and at least two modules, each module comprising two complementary connectable sub-modules. The module support comprises for each sub-module at least an alignment member adapted to individually align the sub-module during its installation on the module support in such way to connect it to complementary sub-module already installed on the module support to form one of the modules. The invention also relates on a module support, a module and a Flexible Alternative Current Transmission Systems.
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公开(公告)号：US09825511B2
公开(公告)日：2017-11-21
申请号：US14488607
申请日：2014-09-17
CPC分类号： H02K15/0006 , H02K1/18 , H02K15/024 , Y10T29/49009
摘要： The method for repairing a stator having a damaged part includes providing the stator with a seat, removing the damaged part of the stator, connecting the inserts replacing the damaged part of the stator to the seat, and fixing the inserts.
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公开(公告)号：US09822981B2
公开(公告)日：2017-11-21
申请号：US14493839
申请日：2014-09-23
发明人： Andrea Ciani , Hanspeter Knoepfel
摘要： The invention relates to a mixing arrangement for mixing a fuel with a stream of oxygen containing gas flowing along an axis in an axial channel, especially in the second combustor of a gas turbine with sequential combustion. The mixing is improved and the mixing length reduced by said mixing arrangement comprising an injector with at least one injector ring, which is passed by said stream of gas inside and outside.
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公开(公告)号：US09816380B2
公开(公告)日：2017-11-14
申请号：US14199644
申请日：2014-03-06
发明人： Michel Floch , Arnaud Buguin , Julien Lemaire
CPC分类号： F01D5/22 , B23P15/04 , F01D5/141 , F01D5/225 , F01D5/3023 , F01D5/3053 , F05D2220/31 , Y10T29/49321
摘要： Low-pressure turbine rotors for a thermoelectric power station include an interconnection of slender blades. The rotor includes blades bearing caps being roughly in the shape of a chevron.
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公开(公告)号：US09810160B2
公开(公告)日：2017-11-07
申请号：US14088494
申请日：2013-11-25
发明人： Wolfgang Lang , Jürgen Hoffmann
IPC分类号： G01K11/22 , G01N25/20 , G01K13/00 , G01K3/00 , F02C9/28 , G01M15/14 , G01K11/24 , G01K13/02 , F02C6/00
CPC分类号： F02C9/28 , F02C6/003 , F05D2270/303 , F05D2270/80 , G01K11/24 , G01K13/02 , G01K2013/024 , G01M15/14 , Y02E20/14
摘要： The disclosure relates to a method for determining a temperature in a pressurized flow path of a gas turbine comprising the steps of sending an acoustic signal from an acoustic signal emitting transducer across a section of the pressurized flow path, detecting the acoustic signal with a receiving transducer, measuring the time needed by the acoustic signal to travel from the acoustic signal emitting transducer to the receiving transducer, calculating the speed of sound, and calculating the temperature as a function of the speed of sound, the heat capacity ratio (□) and a specific gas constant (Rspec) of the gas flowing in the pressurized flow path.Besides the method, a gas turbine with a processor and transducers arranged to carry out such a method is disclosed.
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公开(公告)号：US09778218B2
公开(公告)日：2017-10-03
申请号：US14807965
申请日：2015-07-24
发明人： Scott Barham , Ken Yves Haffner , Naoki Yamada , Georg Donnert
CPC分类号： G01N27/223 , G01F1/64 , G01F1/74
摘要： A method and measurement system for measuring the wetness of a gas phase of a two phase flowing fluid. The measurement system includes a container, a liquid film measurement device and an Electrical Capacitance Tomography device.
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公开(公告)号：US09765626B2
公开(公告)日：2017-09-19
申请号：US14661661
申请日：2015-03-18
CPC分类号： F01D5/141 , F01D5/148 , F01D5/16 , F01D5/186 , F01D5/187 , F01D9/02 , F05D2220/32 , F05D2250/70
摘要： The invention refers to a gas turbine blade including an airfoil extending in radial direction from a blade root to a blade tip, defining a span ranging from 0% at the blade root to 100% at the blade tip, and extending in axial direction from a leading edge to a trailing edge, which limit a chord with an axial chord length defined by an axial length of a straight line connecting the leading edge and trailing edge of the airfoil depending on the span. The axial chord length increases at least from 80% span to 100% span.
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