GB1018168A - Improvements in stator assembly - Google Patents

Improvements in stator assembly

Info

Publication number
GB1018168A
GB1018168A GB50878/63A GB5087863A GB1018168A GB 1018168 A GB1018168 A GB 1018168A GB 50878/63 A GB50878/63 A GB 50878/63A GB 5087863 A GB5087863 A GB 5087863A GB 1018168 A GB1018168 A GB 1018168A
Authority
GB
United Kingdom
Prior art keywords
segment
segments
vanes
shrouds
adjacent
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
GB50878/63A
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB1018168A publication Critical patent/GB1018168A/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
    • F01D9/041—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
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
GB50878/63A 1962-12-28 1963-12-24 Improvements in stator assembly Expired GB1018168A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US248071A US3142475A (en) 1962-12-28 1962-12-28 Stator assembly

Publications (1)

Publication Number Publication Date
GB1018168A true GB1018168A (en) 1966-01-26

Family

ID=22937552

Family Applications (1)

Application Number Title Priority Date Filing Date
GB50878/63A Expired GB1018168A (en) 1962-12-28 1963-12-24 Improvements in stator assembly

Country Status (3)

Country Link
US (1) US3142475A (de)
DE (1) DE1286333B (de)
GB (1) GB1018168A (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0058532A2 (de) * 1981-02-17 1982-08-25 Mitsubishi Jukogyo Kabushiki Kaisha Düse für Axialturbine
GB2251034A (en) * 1990-12-20 1992-06-24 Rolls Royce Plc Shrouded aerofoils

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3252212A (en) * 1963-07-25 1966-05-24 Chrysler Corp Method of selectively matching a turbine wheel and turbine nozzle assembly
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
US4492517A (en) * 1983-01-06 1985-01-08 General Electric Company Segmented inlet nozzle for gas turbine, and methods of installation
US6234750B1 (en) * 1999-03-12 2001-05-22 General Electric Company Interlocked compressor stator
US7172388B2 (en) * 2004-08-24 2007-02-06 Pratt & Whitney Canada Corp. Multi-point seal
US7195453B2 (en) * 2004-08-30 2007-03-27 General Electric Company Compressor stator floating tip shroud and related method
CN101858229A (zh) * 2010-04-29 2010-10-13 中国燃气涡轮研究院 发动机热定心承力型导向器
EP2735707B1 (de) * 2012-11-27 2017-04-05 Safran Aero Boosters SA Leitrad einer axialen Turbomaschine mit segmentiertem Innendeckband und zugehöriger Verdichter

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA615110A (en) * 1961-02-21 General Motors Corporation Vane ring assembly
DE846342C (de) * 1944-11-26 1952-08-11 Maschf Augsburg Nuernberg Ag Turbinenleitapparat aus keramischen Werkstoffen
DE826673C (de) * 1945-04-04 1952-01-03 Maschf Augsburg Nuernberg Ag Leitapparat mit keramischen Leitschaufeln
BE487116A (de) * 1946-07-16
GB679916A (en) * 1949-04-29 1952-09-24 Geoffrey Bertram Robert Feilde Improvements in gas turbines
FR1003299A (fr) * 1949-12-13 1952-03-17 Rateau Soc Perfectionnement aux turbines à gaz et autres turbo-machines axiales
US2772069A (en) * 1951-10-31 1956-11-27 Gen Motors Corp Segmented stator ring assembly
GB778300A (en) * 1954-08-19 1957-07-03 Rolls Royce Improvements in or relating to axial-flow compressors and turbines
DE1067971B (de) * 1955-10-18 1959-10-29
US3069135A (en) * 1957-10-03 1962-12-18 Gen Motors Corp Vane ring assembly

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0058532A2 (de) * 1981-02-17 1982-08-25 Mitsubishi Jukogyo Kabushiki Kaisha Düse für Axialturbine
EP0058532A3 (de) * 1981-02-17 1983-04-27 Mitsubishi Jukogyo Kabushiki Kaisha Düse für Axialturbine
GB2251034A (en) * 1990-12-20 1992-06-24 Rolls Royce Plc Shrouded aerofoils
GB2251034B (en) * 1990-12-20 1995-05-17 Rolls Royce Plc Shrouded aerofoils

Also Published As

Publication number Publication date
DE1286333B (de) 1969-01-02
US3142475A (en) 1964-07-28

Similar Documents

Publication Publication Date Title
US3892497A (en) Axial flow turbine stationary blade and blade ring locking arrangement
GB1306575A (en) Segmented seal assembly for axial flow turbines
US4369016A (en) Turbine intermediate case
GB1295025A (de)
US3938906A (en) Slidable stator seal
US4863343A (en) Turbine vane shroud sealing system
GB1008526A (en) Axial flow bladed rotor, e.g. for a turbine
US2609176A (en) Turbine nozzle guide vane construction
GB617475A (en) Improvements relating to gas-turbine engines
SE7910211L (sv) Turbinmantelaggregat
GB1484936A (en) Gas turbine engines
GB1523668A (en) Turbomachinery stator assembly
GB1461965A (en) Axial flow turbine structure
GB1199974A (en) Turbine Blade Seal Assembly
US2903237A (en) Stator construction for axial-flow fluid machine
US3519366A (en) Turbine diaphragm seal structure
GB741794A (en) Improvements in turbine nozzles
KR970075266A (ko) 배출가스 터보과급기의 배출가스 터빈
US2955800A (en) Turbomachine stator assembly
GB1109457A (en) Segmented diaphragm assembly for turbines
GB1344221A (en) Vane rings
GB1018168A (en) Improvements in stator assembly
US2801075A (en) Turbine nozzle
GB853997A (en) Improvements in gas turbine nozzle structures
GB1142951A (en) An arrangement for radially positioning a first annular member relatively to a second annular member