GB1011713A - Bladed turbine or compressor rotors - Google Patents

Bladed turbine or compressor rotors

Info

Publication number
GB1011713A
GB1011713A GB38511/64A GB3851164A GB1011713A GB 1011713 A GB1011713 A GB 1011713A GB 38511/64 A GB38511/64 A GB 38511/64A GB 3851164 A GB3851164 A GB 3851164A GB 1011713 A GB1011713 A GB 1011713A
Authority
GB
United Kingdom
Prior art keywords
key
blade
sept
engaging
compressor rotors
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
GB38511/64A
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation 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 Motors Liquidation Co filed Critical Motors Liquidation Co
Publication of GB1011713A publication Critical patent/GB1011713A/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

Abstract

1,011,713. Cotters. GENERAL MOTORS CORPORATION. Sept. 21, 1964 [Sept. 26, 1963], No. 38511/64. Heading F2H. [Also in Division F1] A turbine or compressor blade 8 is locked in an axially extending serrated slot 6 in the rotor periphery 4 by a metal key 20 having a stem 22 fitting in a notch 18 in the blade and a base 24 engaging a circumferential groove 14 in the rotor. The key is held in position by serrations 26, 28 engaging the serrated root 12 of the adjacent blade. The key may be a sheet metal stamping or an extrusion.
GB38511/64A 1963-09-26 1964-09-21 Bladed turbine or compressor rotors Expired GB1011713A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US311865A US3198485A (en) 1963-09-26 1963-09-26 Turbine blade lock

Publications (1)

Publication Number Publication Date
GB1011713A true GB1011713A (en) 1965-12-01

Family

ID=23208844

Family Applications (1)

Application Number Title Priority Date Filing Date
GB38511/64A Expired GB1011713A (en) 1963-09-26 1964-09-21 Bladed turbine or compressor rotors

Country Status (2)

Country Link
US (1) US3198485A (en)
GB (1) GB1011713A (en)

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 (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3575522A (en) * 1968-08-30 1971-04-20 Gen Motors Corp Turbine cooling
US3930751A (en) * 1974-07-05 1976-01-06 Carrier Corporation Bucket locking mechanism
US3904317A (en) * 1974-11-27 1975-09-09 Gen Electric Bucket locking mechanism
GB1513338A (en) * 1976-03-26 1978-06-07 Rolls Royce Rotor blade for a gas turbine engine
US4676723A (en) * 1986-03-26 1987-06-30 Westinghouse Electric Corp. Locking system for a turbine side entry blade
US5242270A (en) * 1992-01-31 1993-09-07 Westinghouse Electric Corp. Platform motion restraints for freestanding turbine blades
DE10012381A1 (en) * 2000-03-14 2001-09-20 Man Turbomasch Ag Ghh Borsig Bucket lock and method for manufacturing a paddle lock
US6416286B1 (en) * 2000-12-28 2002-07-09 General Electric Company System and method for securing a radially inserted integral closure bucket to a turbine rotor wheel assembly having axially inserted buckets
US6929453B2 (en) * 2003-12-11 2005-08-16 Siemens Westinghouse Power Corporation Locking spacer assembly for slotted turbine component
US9127563B2 (en) 2011-04-05 2015-09-08 General Electric Company Locking device arrangement for a rotating bladed stage
US9051845B2 (en) * 2012-01-05 2015-06-09 General Electric Company System for axial retention of rotating segments of a turbine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB671960A (en) * 1949-08-23 1952-05-14 Bristol Aeroplane Co Ltd Improvements in or relating to attachment means for rotor blades
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
NL99070C (en) * 1953-07-28
GB779059A (en) * 1954-07-15 1957-07-17 Rolls Royce Improvements in or relating to axial-flow fluid machines, for example compressors orturbines of gas-turbine engines

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
US3198485A (en) 1965-08-03

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