GB1011713A - Bladed turbine or compressor rotors - Google Patents
Bladed turbine or compressor rotorsInfo
- 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
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/32—Locking, e.g. by final locking blades or keys
- F01D5/326—Locking 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.
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)
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)
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)
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 |
-
1963
- 1963-09-26 US US311865A patent/US3198485A/en not_active Expired - Lifetime
-
1964
- 1964-09-21 GB GB38511/64A patent/GB1011713A/en not_active Expired
Cited By (2)
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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