GB1344221A - Vane rings - Google Patents

Vane rings

Info

Publication number
GB1344221A
GB1344221A GB1919772A GB1919772A GB1344221A GB 1344221 A GB1344221 A GB 1344221A GB 1919772 A GB1919772 A GB 1919772A GB 1919772 A GB1919772 A GB 1919772A GB 1344221 A GB1344221 A GB 1344221A
Authority
GB
United Kingdom
Prior art keywords
ring
hole
segment
turbine stator
bolt
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
Application number
GB1919772A
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 Solutions GmbH
Original Assignee
MTU Friedrichshafen GmbH
MTU Motoren und Turbinen Union Friedrichshafen GmbH
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 MTU Friedrichshafen GmbH, MTU Motoren und Turbinen Union Friedrichshafen GmbH filed Critical MTU Friedrichshafen GmbH
Publication of GB1344221A publication Critical patent/GB1344221A/en
Expired legal-status Critical Current

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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)

Abstract

1344221 Turbine stator vanes MOTORENUND TURBINEN-UNION FRIEDRICHSHAFEN GmbH 25 April 1972 [3 May 1971] 19197/72 Heading FIT Each segment 11 of a segmental turbine stator vane ring has a radially inwardly extending flange 18 which is secured between a gas inlet housing 16 and a centering ring 12 by two bolts 15 or the like passing through holes 21, 22 in the flange, hole 21 containing a locating sleeve 14 surrounding the respective bolt 15 with clearance whereas hole 22 surrounds its bolt 15 with sufficient clearance to permit segment 11 to expand cir- cumferentially about the fixed point provided by sleeve 14. The gap between adjacent segments 11 is inclined substantially in the direction of the vane inlet angle and is sealed at the outer periphery by a cover ring 13 having an abutment surface 26. Similarly inclined stress relief slots 24 are provided in outer shroud 23 at alternate flow passages.
GB1919772A 1971-05-03 1972-04-25 Vane rings Expired GB1344221A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2121707A DE2121707C3 (en) 1971-05-03 1971-05-03 Guide vane ring

Publications (1)

Publication Number Publication Date
GB1344221A true GB1344221A (en) 1974-01-16

Family

ID=5806680

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1919772A Expired GB1344221A (en) 1971-05-03 1972-04-25 Vane rings

Country Status (9)

Country Link
US (1) US3824034A (en)
JP (1) JPS5218850B1 (en)
AT (1) AT311737B (en)
CH (1) CH538045A (en)
DE (1) DE2121707C3 (en)
ES (1) ES402257A1 (en)
FR (1) FR2136773A5 (en)
GB (1) GB1344221A (en)
IT (1) IT952754B (en)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1385666A (en) * 1973-07-06 1975-02-26 Rolls Royce Sealing of vaned assemblies of gas turbine engines
US4194869A (en) * 1978-06-29 1980-03-25 United Technologies Corporation Stator vane cluster
CH664191A5 (en) * 1984-01-09 1988-02-15 Bbc Brown Boveri & Cie EXTERNAL ADJUSTABLE AXIAL FIXING OF A BLADE CARRIER IN A TURBINE.
US4566851A (en) * 1984-05-11 1986-01-28 United Technologies Corporation First stage turbine vane support structure
US4643636A (en) * 1985-07-22 1987-02-17 Avco Corporation Ceramic nozzle assembly for gas turbine engine
US4721434A (en) * 1986-12-03 1988-01-26 United Technologies Corporation Damping means for a stator
FR2624914B1 (en) * 1987-12-16 1990-04-20 Snecma DEVICE FOR FIXING WITH A REVOLUTION PART TO AN ANNULAR FLANGE OF A TURBOMACHINE
US4890978A (en) * 1988-10-19 1990-01-02 Westinghouse Electric Corp. Method and apparatus for vane segment support and alignment in combustion turbines
US5149250A (en) * 1991-02-28 1992-09-22 General Electric Company Gas turbine vane assembly seal and support system
SE500743C2 (en) * 1992-04-01 1994-08-22 Abb Carbon Ab Method and apparatus for mounting axial flow machine
US5392513A (en) * 1993-12-21 1995-02-28 General Electric Co. Steampath and process of retrofitting a nozzle thereof
US5618161A (en) * 1995-10-17 1997-04-08 Westinghouse Electric Corporation Apparatus for restraining motion of a turbo-machine stationary vane
US6234750B1 (en) * 1999-03-12 2001-05-22 General Electric Company Interlocked compressor stator
DE10161292A1 (en) 2001-12-13 2003-06-26 Rolls Royce Deutschland Bearing ring for the storage of blade roots of adjustable stator blades in the high pressure compressor of a gas turbine
JP4247214B2 (en) * 2004-10-29 2009-04-02 三菱重工業株式会社 Exhaust turbine turbocharger
EP1724443A1 (en) * 2005-05-20 2006-11-22 ABB Turbo Systems AG Nozzle ring
FR2935428B1 (en) * 2008-08-26 2015-06-26 Snecma FIXED BLADE OF TURBOMACHINE WITH REDUCED MASS AND TURBOMACHINE COMPRISING AT LEAST ONE SUCH FIXED AUBAGE
US8328512B2 (en) * 2009-06-05 2012-12-11 United Technologies Corporation Inner diameter shroud assembly for variable inlet guide vane structure in a gas turbine engine
DE102010064047A1 (en) * 2010-12-23 2012-06-28 Man Diesel & Turbo Se Fluid flow machine has housing with fluid guiding housing and bearing housing that is connected with fluid guiding housing, where impeller is mounted in fluid guiding housing over central impeller shaft in rotating manner
US9181855B2 (en) * 2013-01-31 2015-11-10 Electro-Motive Diesel, Inc. Turbocharger with axial turbine stage
DE102013017713B4 (en) 2013-10-24 2022-10-27 Man Energy Solutions Se turbomachine
FR3044411B1 (en) 2015-11-27 2018-10-26 Safran Aircraft Engines TURBUMACHINE MODULE OR COMBUSTION CHAMBER TEST BENCH
US10294808B2 (en) * 2016-04-21 2019-05-21 United Technologies Corporation Fastener retention mechanism

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2905434A (en) * 1954-07-08 1959-09-22 Westinghouse Electric Corp Turbine apparatus
US3262677A (en) * 1963-11-27 1966-07-26 Gen Electric Stator assembly
US3302926A (en) * 1965-12-06 1967-02-07 Gen Electric Segmented nozzle diaphragm for high temperature turbine
US3542483A (en) * 1968-07-17 1970-11-24 Westinghouse Electric Corp Turbine stator structure

Also Published As

Publication number Publication date
DE2121707C3 (en) 1974-06-20
AT311737B (en) 1973-11-26
ES402257A1 (en) 1975-11-01
CH538045A (en) 1973-06-15
IT952754B (en) 1973-07-30
FR2136773A5 (en) 1972-12-22
DE2121707B2 (en) 1973-11-22
US3824034A (en) 1974-07-16
DE2121707A1 (en) 1972-11-16
JPS5218850B1 (en) 1977-05-24

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee