WO2018118217A3 - Machine rotative et ensemble buse associé - Google Patents

Machine rotative et ensemble buse associé Download PDF

Info

Publication number
WO2018118217A3
WO2018118217A3 PCT/US2017/058674 US2017058674W WO2018118217A3 WO 2018118217 A3 WO2018118217 A3 WO 2018118217A3 US 2017058674 W US2017058674 W US 2017058674W WO 2018118217 A3 WO2018118217 A3 WO 2018118217A3
Authority
WO
WIPO (PCT)
Prior art keywords
rotary machine
hook
ring
nozzle assembly
nozzle
Prior art date
Application number
PCT/US2017/058674
Other languages
English (en)
Other versions
WO2018118217A2 (fr
Inventor
Manish Mahasukhrai JOSHI
David Orus FITTS
Robert Edward DEALLENBACH
Original Assignee
General Electric Company
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from US15/383,947 external-priority patent/US20170096904A1/en
Application filed by General Electric Company filed Critical General Electric Company
Priority to EP17882534.5A priority Critical patent/EP3555426A4/fr
Publication of WO2018118217A2 publication Critical patent/WO2018118217A2/fr
Publication of WO2018118217A3 publication Critical patent/WO2018118217A3/fr

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/31Application in turbines in steam turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position
    • F05D2260/38Retaining components in desired mutual position by a spring, i.e. spring loaded or biased towards a certain position

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)

Abstract

La présente invention concerne une machine rotative. La machine rotative comprend une section turbine dotée d'un boîtier et un anneau accouplé à l'intérieur du boîtier. L'anneau présente une rainure. La machine rotative comprend également une buse accouplée à l'anneau. La buse comprend une première extrémité, une seconde extrémité et une surface portante s'étendant entre les première et seconde extrémités le long d'un axe longitudinal. La première extrémité comprend un premier crochet et un second crochet. Le premier crochet présente une première surface radialement externe, et le second crochet présente une seconde surface radialement externe. L'anneau et la première extrémité de la buse coopèrent pour former un élément anti-rotation qui s'étend à partir d'au moins l'une des surfaces radialement externes le long de l'axe et entre les crochets.
PCT/US2017/058674 2016-12-19 2017-10-27 Machine rotative et ensemble buse associé WO2018118217A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP17882534.5A EP3555426A4 (fr) 2016-12-19 2017-10-27 Machine rotative et ensemble buse associé

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/383,947 2016-12-19
US15/383,947 US20170096904A1 (en) 2012-09-13 2016-12-19 Rotary machine and nozzle assembly therefor

Publications (2)

Publication Number Publication Date
WO2018118217A2 WO2018118217A2 (fr) 2018-06-28
WO2018118217A3 true WO2018118217A3 (fr) 2018-07-26

Family

ID=62627086

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2017/058674 WO2018118217A2 (fr) 2016-12-19 2017-10-27 Machine rotative et ensemble buse associé

Country Status (2)

Country Link
EP (1) EP3555426A4 (fr)
WO (1) WO2018118217A2 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11125092B2 (en) * 2018-08-14 2021-09-21 Raytheon Technologies Corporation Gas turbine engine having cantilevered stators

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060153683A1 (en) * 2004-04-19 2006-07-13 Dube David P Anti-rotation lock
US20120148395A1 (en) * 2010-12-13 2012-06-14 General Electric Company Steam turbine singlet nozzle design for breech loaded assembly
US20130177400A1 (en) * 2012-01-05 2013-07-11 Mark David Ring Stator vane integrated attachment liner and spring damper
US20140072419A1 (en) * 2012-09-13 2014-03-13 Manish Joshi Rotary machines and methods of assembling
WO2014158293A2 (fr) * 2013-01-08 2014-10-02 United Technologies Corporation Dispositif anti-rotation de stator

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6722848B1 (en) * 2002-10-31 2004-04-20 General Electric Company Turbine nozzle retention apparatus at the carrier horizontal joint face
JP4673732B2 (ja) * 2005-12-01 2011-04-20 株式会社東芝 タービン動翼および蒸気タービン

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060153683A1 (en) * 2004-04-19 2006-07-13 Dube David P Anti-rotation lock
US20120148395A1 (en) * 2010-12-13 2012-06-14 General Electric Company Steam turbine singlet nozzle design for breech loaded assembly
US20130177400A1 (en) * 2012-01-05 2013-07-11 Mark David Ring Stator vane integrated attachment liner and spring damper
US20140072419A1 (en) * 2012-09-13 2014-03-13 Manish Joshi Rotary machines and methods of assembling
WO2014158293A2 (fr) * 2013-01-08 2014-10-02 United Technologies Corporation Dispositif anti-rotation de stator

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3555426A4 *

Also Published As

Publication number Publication date
WO2018118217A2 (fr) 2018-06-28
EP3555426A4 (fr) 2020-09-23
EP3555426A2 (fr) 2019-10-23

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