GB760884A - Mountings for guide blades in axial flow turbines and compressors - Google Patents

Mountings for guide blades in axial flow turbines and compressors

Info

Publication number
GB760884A
GB760884A GB29191/54A GB2919154A GB760884A GB 760884 A GB760884 A GB 760884A GB 29191/54 A GB29191/54 A GB 29191/54A GB 2919154 A GB2919154 A GB 2919154A GB 760884 A GB760884 A GB 760884A
Authority
GB
United Kingdom
Prior art keywords
groove
blade roots
pieces
spacer
blade
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
GB29191/54A
Other languages
English (en)
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.)
Sulzer AG
Original Assignee
Sulzer AG
Sulzer Freres SA
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 Sulzer AG, Sulzer Freres SA filed Critical Sulzer AG
Publication of GB760884A publication Critical patent/GB760884A/en
Expired 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
    • F01D9/042—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)
GB29191/54A 1953-10-23 1954-10-11 Mountings for guide blades in axial flow turbines and compressors Expired GB760884A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH760884X 1953-10-23

Publications (1)

Publication Number Publication Date
GB760884A true GB760884A (en) 1956-11-07

Family

ID=4534672

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29191/54A Expired GB760884A (en) 1953-10-23 1954-10-11 Mountings for guide blades in axial flow turbines and compressors

Country Status (5)

Country Link
BE (1) BE532194A (enrdf_load_stackoverflow)
CH (1) CH315987A (enrdf_load_stackoverflow)
FR (1) FR1108571A (enrdf_load_stackoverflow)
GB (1) GB760884A (enrdf_load_stackoverflow)
NL (1) NL182633B (enrdf_load_stackoverflow)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2980396A (en) * 1959-06-29 1961-04-18 Gen Electric Stator construction for turbine engines
US3975112A (en) * 1975-06-09 1976-08-17 United Technologies Corporation Apparatus for sealing a gas turbine flow path
US4889470A (en) * 1988-08-01 1989-12-26 Westinghouse Electric Corp. Compressor diaphragm assembly
FR2636378A1 (fr) * 1988-09-14 1990-03-16 Snecma Redresseur de soufflante de turboreacteur a double flux
JP2008208831A (ja) * 2007-02-27 2008-09-11 General Electric Co <Ge> ブレードシムを組立てるための方法及び装置
CN109072706A (zh) * 2016-05-09 2018-12-21 赛峰航空器发动机 用于包括分配器、涡轮机的结构元件和连接装置的涡轮机的组件
JP2019152119A (ja) * 2018-03-01 2019-09-12 三菱日立パワーシステムズ株式会社 静翼セグメント、及びこれを備えている蒸気タービン

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2980396A (en) * 1959-06-29 1961-04-18 Gen Electric Stator construction for turbine engines
US3975112A (en) * 1975-06-09 1976-08-17 United Technologies Corporation Apparatus for sealing a gas turbine flow path
US4889470A (en) * 1988-08-01 1989-12-26 Westinghouse Electric Corp. Compressor diaphragm assembly
FR2636378A1 (fr) * 1988-09-14 1990-03-16 Snecma Redresseur de soufflante de turboreacteur a double flux
JP2008208831A (ja) * 2007-02-27 2008-09-11 General Electric Co <Ge> ブレードシムを組立てるための方法及び装置
CN109072706A (zh) * 2016-05-09 2018-12-21 赛峰航空器发动机 用于包括分配器、涡轮机的结构元件和连接装置的涡轮机的组件
CN109072706B (zh) * 2016-05-09 2021-06-08 赛峰航空器发动机 用于包括分配器、涡轮机的结构元件和连接装置的涡轮机的组件
JP2019152119A (ja) * 2018-03-01 2019-09-12 三菱日立パワーシステムズ株式会社 静翼セグメント、及びこれを備えている蒸気タービン
CN110446828A (zh) * 2018-03-01 2019-11-12 三菱日立电力系统株式会社 静叶扇形体及具备该静叶扇形体的蒸汽轮机
CN110446828B (zh) * 2018-03-01 2021-08-06 三菱动力株式会社 静叶扇形体及具备该静叶扇形体的蒸汽轮机
JP7011952B2 (ja) 2018-03-01 2022-01-27 三菱パワー株式会社 静翼セグメント、及びこれを備えている蒸気タービン
US11492919B2 (en) * 2018-03-01 2022-11-08 Mitsubishi Heavy Industries, Ltd. Vane segment and steam turbine comprising same

Also Published As

Publication number Publication date
BE532194A (enrdf_load_stackoverflow)
CH315987A (de) 1956-09-15
FR1108571A (fr) 1956-01-16
NL182633B (nl)

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