GB793930A - Rotor for rotary power conversion machines - Google Patents
Rotor for rotary power conversion machinesInfo
- Publication number
- GB793930A GB793930A GB23223/54A GB2322354A GB793930A GB 793930 A GB793930 A GB 793930A GB 23223/54 A GB23223/54 A GB 23223/54A GB 2322354 A GB2322354 A GB 2322354A GB 793930 A GB793930 A GB 793930A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pin
- tabs
- rotor
- blade
- locking
- 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
- F01D5/323—Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
793,930. Turbine and compressor-bladed rotors. PURVIS, J. T., and SACHS, R. M. Aug. 10, 1954, No. 23223/54. Class 110 (3). A turbine or compressor rotor is formed at its periphery with a plurality of axially-extending slots which are undercut and receive the correspondingly-shaped blade roots, locking devices being provided to prevent endwise movement of the blades. Each blade-mounting slot 15 is formed at its base with an axially-extending groove 16 of rectangular cross-section so that when the blade root 17 is inserted, a rectangular passage is formed beneath the blade root. A locking pin 20 in the form of a strip of rectangular cross-section is disposed in the passage, one end of the pin having a pair of stops 23, 24 disposed on opposite sides of the pin and engaging the blade root and the rotor respectively, at least one of the stops being bent to the locking position after assembly of the blade in the rotor. The stops 23, 24 are formed by a longitudinal slit 22 in the end portion of the pin, thus providing a pair of tabs lying side-by-side. The locking pin shown has a pair of tabs 23, 24 provided at each end of the pin and both tabs 23, 24 at the left-hand end of the pin (see Fig. 2) and one of the tabs at the other end of the pin may be bent to the locking positions before assembly. Reference has been directed by the Comptroller to Specification 672,401.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB12293/57A GB793931A (en) | 1954-08-10 | 1954-08-10 | Rotor for rotary power conversion machines |
GB23223/54A GB793930A (en) | 1954-08-10 | 1954-08-10 | Rotor for rotary power conversion machines |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB12293/57A GB793931A (en) | 1954-08-10 | 1954-08-10 | Rotor for rotary power conversion machines |
GB23223/54A GB793930A (en) | 1954-08-10 | 1954-08-10 | Rotor for rotary power conversion machines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB793930A true GB793930A (en) | 1958-04-23 |
Family
ID=62529417
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB23223/54A Expired GB793930A (en) | 1954-08-10 | 1954-08-10 | Rotor for rotary power conversion machines |
GB12293/57A Expired GB793931A (en) | 1954-08-10 | 1954-08-10 | Rotor for rotary power conversion machines |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB12293/57A Expired GB793931A (en) | 1954-08-10 | 1954-08-10 | Rotor for rotary power conversion machines |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB793930A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4711007A (en) * | 1986-09-29 | 1987-12-08 | Westinghouse Electric Corp. | Method and apparatus for installing free standing turbine blades |
US5425621A (en) * | 1993-01-14 | 1995-06-20 | Mtu Motoren- Und Turbinen-Union Muenchen Gmbh | Device for axially securing moving blades and for eliminating rotor unbalances for axial-flow compressors or turbines |
FR2841933A1 (en) * | 2002-07-04 | 2004-01-09 | Snecma Moteurs | Self-locking wedge for turbojet blower disc blades comprises heel supported on blade root upstream face and wedge shaped runner located with play behind locking ring |
CN110296105A (en) * | 2019-08-15 | 2019-10-01 | 上海电气燃气轮机有限公司 | Blade locking mechanism |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3076634A (en) * | 1959-06-12 | 1963-02-05 | Ass Elect Ind | Locking means for compressor and turbine blades |
GB2287993A (en) * | 1994-03-24 | 1995-10-04 | Rolls Royce Plc | Gas turbine engine fan blade retention |
EP1306522A1 (en) * | 2001-10-29 | 2003-05-02 | ABB Turbo Systems AG | Locking device for axial turbomachine blades |
KR101919228B1 (en) * | 2017-03-16 | 2018-11-15 | 두산중공업 주식회사 | Apparatus for axial locking of bucket and bucket assembly and gas turbine having the same |
-
1954
- 1954-08-10 GB GB23223/54A patent/GB793930A/en not_active Expired
- 1954-08-10 GB GB12293/57A patent/GB793931A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4711007A (en) * | 1986-09-29 | 1987-12-08 | Westinghouse Electric Corp. | Method and apparatus for installing free standing turbine blades |
US5425621A (en) * | 1993-01-14 | 1995-06-20 | Mtu Motoren- Und Turbinen-Union Muenchen Gmbh | Device for axially securing moving blades and for eliminating rotor unbalances for axial-flow compressors or turbines |
FR2841933A1 (en) * | 2002-07-04 | 2004-01-09 | Snecma Moteurs | Self-locking wedge for turbojet blower disc blades comprises heel supported on blade root upstream face and wedge shaped runner located with play behind locking ring |
CN110296105A (en) * | 2019-08-15 | 2019-10-01 | 上海电气燃气轮机有限公司 | Blade locking mechanism |
Also Published As
Publication number | Publication date |
---|---|
GB793931A (en) | 1958-04-23 |
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