JP2013139811A5 - - Google Patents

Download PDF

Info

Publication number
JP2013139811A5
JP2013139811A5 JP2012283887A JP2012283887A JP2013139811A5 JP 2013139811 A5 JP2013139811 A5 JP 2013139811A5 JP 2012283887 A JP2012283887 A JP 2012283887A JP 2012283887 A JP2012283887 A JP 2012283887A JP 2013139811 A5 JP2013139811 A5 JP 2013139811A5
Authority
JP
Japan
Prior art keywords
fluid
passage
turbine
turbine airfoil
cavity
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2012283887A
Other languages
English (en)
Japanese (ja)
Other versions
JP6405077B2 (ja
JP2013139811A (ja
Filing date
Publication date
Priority claimed from US13/342,556 external-priority patent/US8961111B2/en
Application filed filed Critical
Publication of JP2013139811A publication Critical patent/JP2013139811A/ja
Publication of JP2013139811A5 publication Critical patent/JP2013139811A5/ja
Application granted granted Critical
Publication of JP6405077B2 publication Critical patent/JP6405077B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2012283887A 2012-01-03 2012-12-27 タービン及び流体から粒状物を分離するための方法 Active JP6405077B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/342,556 2012-01-03
US13/342,556 US8961111B2 (en) 2012-01-03 2012-01-03 Turbine and method for separating particulates from a fluid

Publications (3)

Publication Number Publication Date
JP2013139811A JP2013139811A (ja) 2013-07-18
JP2013139811A5 true JP2013139811A5 (enExample) 2016-02-04
JP6405077B2 JP6405077B2 (ja) 2018-10-17

Family

ID=47603013

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012283887A Active JP6405077B2 (ja) 2012-01-03 2012-12-27 タービン及び流体から粒状物を分離するための方法

Country Status (5)

Country Link
US (1) US8961111B2 (enExample)
EP (1) EP2612992B1 (enExample)
JP (1) JP6405077B2 (enExample)
CN (1) CN103184888B (enExample)
RU (1) RU2012158329A (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8535006B2 (en) * 2010-07-14 2013-09-17 Siemens Energy, Inc. Near-wall serpentine cooled turbine airfoil
CN104204412B (zh) * 2012-03-22 2016-09-28 通用电器技术有限公司 涡轮叶片
US9650905B2 (en) * 2012-08-28 2017-05-16 United Technologies Corporation Singlet vane cluster assembly
US10227930B2 (en) 2016-03-28 2019-03-12 General Electric Company Compressor bleed systems in turbomachines and methods of extracting compressor airflow
US10669896B2 (en) 2018-01-17 2020-06-02 Raytheon Technologies Corporation Dirt separator for internally cooled components
GB2572170A (en) * 2018-03-21 2019-09-25 Rolls Royce Plc Removing entrained particles
US11391161B2 (en) * 2018-07-19 2022-07-19 General Electric Company Component for a turbine engine with a cooling hole

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3362155A (en) 1965-03-29 1968-01-09 Gen Electric Axial flow separator
US3309567A (en) 1965-10-22 1967-03-14 Berkey Photo Inc Pulse discharge lamp circuit
US3338049A (en) 1966-02-01 1967-08-29 Gen Electric Gas turbine engine including separator for removing extraneous matter
US4685942A (en) 1982-12-27 1987-08-11 General Electric Company Axial flow inlet particle separator
DE68906594T2 (de) * 1988-04-25 1993-08-26 United Technologies Corp Staubabscheider fuer eine luftgekuehlte schaufel.
US5700131A (en) * 1988-08-24 1997-12-23 United Technologies Corporation Cooled blades for a gas turbine engine
GB2228540B (en) * 1988-12-07 1993-03-31 Rolls Royce Plc Cooling of turbine blades
SE527932C2 (sv) * 2004-02-27 2006-07-11 Demag Delaval Ind Turbomachine Ett rotorblad eller en ledskena för en rotormaskin, såsom en gasturbin
GB0524735D0 (en) * 2005-12-03 2006-01-11 Rolls Royce Plc Turbine blade
US7695243B2 (en) * 2006-07-27 2010-04-13 General Electric Company Dust hole dome blade
US7665965B1 (en) * 2007-01-17 2010-02-23 Florida Turbine Technologies, Inc. Turbine rotor disk with dirt particle separator
GB2452327B (en) * 2007-09-01 2010-02-03 Rolls Royce Plc A cooled component
FR2943092B1 (fr) * 2009-03-13 2011-04-15 Snecma Aube de turbine avec un trou de depoussierage en base de pale
US8176720B2 (en) * 2009-09-22 2012-05-15 Siemens Energy, Inc. Air cooled turbine component having an internal filtration system

Similar Documents

Publication Publication Date Title
JP2013139811A5 (enExample)
JP2013245678A5 (enExample)
JP2012082822A5 (enExample)
JP2015090108A5 (enExample)
JP2010043645A5 (enExample)
JP2010249496A5 (enExample)
JP2013217580A5 (enExample)
JP2014114814A5 (enExample)
WO2013103409A3 (en) Gas turbine with optimized airfoil element angles
JP2014088874A5 (enExample)
WO2018009261A3 (en) Ceramic matrix composite airfoil cooling
JP2014234824A5 (enExample)
RU2012158328A (ru) Узел турбины (варианты) и способ снижения потока текучей среды между элементами турбины
JP2012036890A5 (enExample)
WO2013090144A3 (en) Gas turbine engine exhaust diffuser including circumferential vane
JP2014077441A5 (enExample)
JP2014185633A5 (enExample)
JP2014521015A5 (enExample)
JP2015063994A5 (enExample)
JP2011241827A5 (enExample)
CA2845555C (en) Air dryer cartridge with integrated check valve
JP2008025578A5 (enExample)
WO2015012918A3 (en) Gas turbine engine airfoil trailing edge suction side cooling
WO2015130384A3 (en) Fan nacelle inlet flow control
WO2007120162A3 (en) Particle separator for a gas turbine engine