GB1499379A - Turbomachines - Google Patents

Turbomachines

Info

Publication number
GB1499379A
GB1499379A GB16783/75A GB1678375A GB1499379A GB 1499379 A GB1499379 A GB 1499379A GB 16783/75 A GB16783/75 A GB 16783/75A GB 1678375 A GB1678375 A GB 1678375A GB 1499379 A GB1499379 A GB 1499379A
Authority
GB
United Kingdom
Prior art keywords
blade
stem
slot
platform
groove
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
GB16783/75A
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 GB1499379A publication Critical patent/GB1499379A/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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32Locking, e.g. by final locking blades or keys
    • F01D5/326Locking of axial insertion type blades by other means
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Fire-Extinguishing Compositions (AREA)
GB16783/75A 1974-11-27 1975-04-23 Turbomachines Expired GB1499379A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US527586A US3904317A (en) 1974-11-27 1974-11-27 Bucket locking mechanism

Publications (1)

Publication Number Publication Date
GB1499379A true GB1499379A (en) 1978-02-01

Family

ID=24102083

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16783/75A Expired GB1499379A (en) 1974-11-27 1975-04-23 Turbomachines

Country Status (9)

Country Link
US (1) US3904317A (fr)
JP (1) JPS5848729B2 (fr)
CA (1) CA1037870A (fr)
DE (1) DE2516061C2 (fr)
FR (1) FR2292856A1 (fr)
GB (1) GB1499379A (fr)
IT (1) IT1037743B (fr)
NL (1) NL7504670A (fr)
NO (1) NO147427C (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2322418A (en) * 1997-01-03 1998-08-26 Westinghouse Electric Corp Turbomacine blade locking arrangement

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH581783A5 (fr) * 1975-01-30 1976-11-15 Bbc Sulzer Turbomaschinen
US4135857A (en) * 1977-06-09 1979-01-23 United Technologies Corporation Reduced drag airfoil platforms
JPS5482505A (en) * 1977-12-14 1979-06-30 Hitachi Ltd Steam turbine
US4451959A (en) * 1980-12-29 1984-06-05 Elliott Turbomachinery Company, Inc. Methods for securing a rotor blade within a rotor assembly and removing a rotor blade therefrom
US4400137A (en) * 1980-12-29 1983-08-23 Elliott Turbomachinery Co., Inc. Rotor assembly and methods for securing a rotor blade therewithin and removing a rotor blade therefrom
US4676723A (en) * 1986-03-26 1987-06-30 Westinghouse Electric Corp. Locking system for a turbine side entry blade
US4820126A (en) * 1988-02-22 1989-04-11 Westinghouse Electric Corp. Turbomachine rotor assembly having reduced stress concentrations
US4915587A (en) * 1988-10-24 1990-04-10 Westinghouse Electric Corp. Apparatus for locking side entry blades into a rotor
US5242270A (en) * 1992-01-31 1993-09-07 Westinghouse Electric Corp. Platform motion restraints for freestanding turbine blades
GB9412963D0 (en) * 1994-06-28 1994-09-28 Rolls Royce Plc Gas turbine engine fan blade assembly
GB2299834B (en) * 1995-04-12 1999-09-08 Rolls Royce Plc Gas turbine engine rotary disc
US20040115059A1 (en) * 2002-12-12 2004-06-17 Kehl Richard Eugene Cored steam turbine bucket
GB2397854A (en) * 2003-01-30 2004-08-04 Rolls Royce Plc Securing blades in a rotor assembly
GB2406144A (en) * 2003-09-19 2005-03-23 Rolls Royce Plc Gas turbine engine blade retention system using a key
DE102004054930A1 (de) * 2004-11-13 2006-05-18 Mtu Aero Engines Gmbh Rotor einer Turbomaschine, insbesondere Gasturbinenrotor
JP4886735B2 (ja) * 2008-05-26 2012-02-29 株式会社東芝 タービン動翼組立体および蒸気タービン
JP5149831B2 (ja) * 2009-02-12 2013-02-20 三菱重工コンプレッサ株式会社 タービン動翼の固定構造及びタービン
US8714929B2 (en) * 2010-11-10 2014-05-06 General Electric Company Turbine assembly and method for securing a closure bucket
US20130052024A1 (en) * 2011-08-24 2013-02-28 General Electric Company Turbine Nozzle Vane Retention System
US9051845B2 (en) * 2012-01-05 2015-06-09 General Electric Company System for axial retention of rotating segments of a turbine
CN106015086B (zh) * 2016-06-02 2018-11-09 东方电气集团东方汽轮机有限公司 一种压气机叶片在叶轮轮槽中的轴向锁定结构
FR3056630B1 (fr) * 2016-09-26 2018-12-07 Safran Aircraft Engines Disque aubage monobloc de soufflante pour turbomachine d'aeronef
CN113623270B (zh) * 2021-08-24 2024-04-16 中国联合重型燃气轮机技术有限公司 锁紧装置及含有该锁紧装置的压气机、燃气轮机
JP2023090250A (ja) * 2021-12-17 2023-06-29 三菱重工コンプレッサ株式会社 蒸気タービンのロータ、蒸気タービン、及び動翼の固定方法

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB725461A (en) * 1953-04-10 1955-03-02 Parsons C A & Co Ltd Improvements in and relating to the axial locking of rotor blades for turbines and the like
US2949278A (en) * 1956-07-05 1960-08-16 Gen Motors Corp Turbine blade retention
US3198485A (en) * 1963-09-26 1965-08-03 Gen Motors Corp Turbine blade lock

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2322418A (en) * 1997-01-03 1998-08-26 Westinghouse Electric Corp Turbomacine blade locking arrangement
GB2322418B (en) * 1997-01-03 2001-05-09 Westinghouse Electric Corp Apparatus and method for locking blades into a rotor

Also Published As

Publication number Publication date
JPS5848729B2 (ja) 1983-10-31
CA1037870A (fr) 1978-09-05
US3904317A (en) 1975-09-09
NO147427C (no) 1983-04-06
NO751348L (fr) 1976-05-31
FR2292856B1 (fr) 1980-01-25
IT1037743B (it) 1979-11-20
NL7504670A (nl) 1976-05-31
NO147427B (no) 1982-12-27
FR2292856A1 (fr) 1976-06-25
DE2516061A1 (de) 1976-08-12
DE2516061C2 (de) 1983-07-28
JPS5162204A (fr) 1976-05-29

Similar Documents

Publication Publication Date Title
GB1499379A (en) Turbomachines
US4692976A (en) Method of making scalable side entry turbine blade roots
GB1386821A (en) Bladed rotors including split-nut assemblies
GB805319A (en) Improvements relating to turbine wheels
GB1482308A (en) Turbine rotating blade
GB1195171A (en) Improvements in Lock for Turbomachinery Blades.
CA2226167A1 (fr) Dispositif et methode de blocage des aubes dans un rotor
GB1022386A (en) Improvements in a rotor assembly for turbine and like bladed machines
GB1187227A (en) Improvements in Bladed Rotors for Axial Flow Compressors, Turbines and the like
GB1477763A (en) Blade assemblies
GB1509048A (en) Bladed rotor
GB1366924A (en) Compressor blades
GB903176A (en) Method of mounting a multi-blade set on a support member, for example to form a gas turbine compressor rotor
GB827264A (en) Improvements in compressor rotor
GB1326122A (en) Blade securing arrangement for compressors and or turbines
GB1492286A (en) Means of locking parts mounted on the rotor of a turbomachine
GB1498684A (en) Screw drivers
GB894704A (en) Improvements in reusable locking means for turbine or compressor rotor assemblies
US3632228A (en) Device for locking turbomachinery blades
GB1011713A (en) Bladed turbine or compressor rotors
GB1468470A (en) Turbines
GB933047A (en) Improvements in rotor assembly for gas turbine engines
GB980656A (en) Improvements in and relating to turbines and like machines
GB819433A (en) Rotor blade and rotor blade assembly for machines such as compressors or turbines
GB1102219A (en) Bladed turbine or compressor rotors

Legal Events

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