GB2425155B - A mounting arrangement - Google Patents

A mounting arrangement

Info

Publication number
GB2425155B
GB2425155B GB0507405A GB0507405A GB2425155B GB 2425155 B GB2425155 B GB 2425155B GB 0507405 A GB0507405 A GB 0507405A GB 0507405 A GB0507405 A GB 0507405A GB 2425155 B GB2425155 B GB 2425155B
Authority
GB
United Kingdom
Prior art keywords
mounting arrangement
mounting
arrangement
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.)
Expired - Fee Related
Application number
GB0507405A
Other versions
GB0507405D0 (en
GB2425155A (en
Inventor
Crispin David Bolgar
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB0507405A priority Critical patent/GB2425155B/en
Publication of GB0507405D0 publication Critical patent/GB0507405D0/en
Publication of GB2425155A publication Critical patent/GB2425155A/en
Application granted granted Critical
Publication of GB2425155B publication Critical patent/GB2425155B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB0507405A 2005-04-13 2005-04-13 A mounting arrangement Expired - Fee Related GB2425155B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0507405A GB2425155B (en) 2005-04-13 2005-04-13 A mounting arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0507405A GB2425155B (en) 2005-04-13 2005-04-13 A mounting arrangement

Publications (3)

Publication Number Publication Date
GB0507405D0 GB0507405D0 (en) 2005-05-18
GB2425155A GB2425155A (en) 2006-10-18
GB2425155B true GB2425155B (en) 2007-09-19

Family

ID=34611013

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0507405A Expired - Fee Related GB2425155B (en) 2005-04-13 2005-04-13 A mounting arrangement

Country Status (1)

Country Link
GB (1) GB2425155B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10287919B2 (en) 2012-09-28 2019-05-14 United Technologies Corporation Liner lock segment

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006050907A1 (en) 2006-10-28 2008-05-15 Man Turbo Ag Guide device of a turbomachine and vane for such a guide device
FR2922950B1 (en) * 2007-10-31 2014-05-09 Snecma CARTRIDGE OF ABRADABLE MATERIAL
GB0922422D0 (en) 2009-12-23 2010-02-03 Rolls Royce Plc Annulus Filler Assembly for a Rotor of a Turbomachine
US8454303B2 (en) * 2010-01-14 2013-06-04 General Electric Company Turbine nozzle assembly
US8864446B2 (en) 2011-05-23 2014-10-21 Siemens Energy, Inc. Wear pin gap closure detection system for gas turbine engine
EP2696039B1 (en) * 2012-08-10 2015-07-29 MTU Aero Engines GmbH Gas turbine stage
EP3085900B1 (en) 2015-04-21 2020-08-05 Ansaldo Energia Switzerland AG Abradable lip for a gas turbine

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB856599A (en) * 1958-06-16 1960-12-21 Gen Motors Corp Improvements relating to axial-flow compressors
US4239451A (en) * 1978-06-01 1980-12-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Device to fasten a seal to the guide vanes of a turbine engine
JPS6189908A (en) * 1984-10-11 1986-05-08 Central Res Inst Of Electric Power Ind Ceramics-metal composite vane structure
JPH07324601A (en) * 1994-05-31 1995-12-12 Mitsubishi Heavy Ind Ltd Diaphragm structure for steam turbine
US5586864A (en) * 1994-07-27 1996-12-24 General Electric Company Turbine nozzle diaphragm and method of assembly
JP2001123803A (en) * 1999-10-21 2001-05-08 Toshiba Corp Seal device, steam turbine and power plant equipped with the same

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB856599A (en) * 1958-06-16 1960-12-21 Gen Motors Corp Improvements relating to axial-flow compressors
US4239451A (en) * 1978-06-01 1980-12-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Device to fasten a seal to the guide vanes of a turbine engine
JPS6189908A (en) * 1984-10-11 1986-05-08 Central Res Inst Of Electric Power Ind Ceramics-metal composite vane structure
JPH07324601A (en) * 1994-05-31 1995-12-12 Mitsubishi Heavy Ind Ltd Diaphragm structure for steam turbine
US5586864A (en) * 1994-07-27 1996-12-24 General Electric Company Turbine nozzle diaphragm and method of assembly
JP2001123803A (en) * 1999-10-21 2001-05-08 Toshiba Corp Seal device, steam turbine and power plant equipped with the same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10287919B2 (en) 2012-09-28 2019-05-14 United Technologies Corporation Liner lock segment

Also Published As

Publication number Publication date
GB0507405D0 (en) 2005-05-18
GB2425155A (en) 2006-10-18

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20130413