GB728710A - Improvements in and relating to axial-flow turbines and the like - Google Patents
Improvements in and relating to axial-flow turbines and the likeInfo
- Publication number
- GB728710A GB728710A GB2462/53A GB246253A GB728710A GB 728710 A GB728710 A GB 728710A GB 2462/53 A GB2462/53 A GB 2462/53A GB 246253 A GB246253 A GB 246253A GB 728710 A GB728710 A GB 728710A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- root
- blades
- pieces
- piece
- 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
- F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
Abstract
728,710. Turbines and compressors. ESCHER WYSS AKT.-GES. Jan. 28, 1953 [Feb. 13, 1952], No. 2462/53. Class 110 (3). In an axial-flow turbine or compressor, blades are mounted in slots in a blade carrier, the slots extending substantially parallel to the chords of the blades and having parallel lateral faces. The blades have a constant cross-sectional profile throughout their length and one or more root pieces are fitted to each blade where the blades are mounted in the blade carrier so as to form a prismatic-shaped root having parallel lateral faces which lie against the faces of the associated slot. The blades and root pieces are secured by pins, at least one for each blade, which extend through the blade carrier, blade and root piece. The root piece may be welded to the blade. In Fig. 2, the blade 3 is mounted in a slot 2 in the rotor disc 1 and the root portion is formed by two root pieces 4, 5 at either side of the root end of the blade, the blade being secured in position by two pins 6. In a second embodiment in which one face of the blade is plane, only one root piece is provided. In an embodiment in which the blade is hollow and is formed of sheet metal, two root pieces are used and they bear against each other beyond the leading and trailing edges of the blade. Alternatively, an additional piece 17, Fig. 5, may be inserted into the hollow blade in the region of the root pieces.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH728710X | 1952-02-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB728710A true GB728710A (en) | 1955-04-27 |
Family
ID=4532169
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2462/53A Expired GB728710A (en) | 1952-02-13 | 1953-01-28 | Improvements in and relating to axial-flow turbines and the like |
Country Status (6)
Country | Link |
---|---|
BE (1) | BE517285A (en) |
CH (1) | CH298592A (en) |
DE (1) | DE942236C (en) |
FR (1) | FR1070291A (en) |
GB (1) | GB728710A (en) |
NL (1) | NL81262C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4767275A (en) * | 1986-07-11 | 1988-08-30 | Westinghouse Electric Corp. | Locking pin system for turbine curved root side entry closing blades |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3073568A (en) * | 1958-06-27 | 1963-01-15 | Edward A Stalker | Composite blades for turbines, compressors and the like |
US4605355A (en) * | 1983-03-31 | 1986-08-12 | Competition Aircraft, Inc. | Propeller |
DE3710321C1 (en) * | 1987-03-28 | 1988-06-01 | Mtu Muenchen Gmbh | Fan blade, especially for prop fan engines |
FR2990462B1 (en) | 2012-05-14 | 2014-05-30 | Snecma | DEVICE FOR ATTACHING AUBES TO A TURBOMACHINE ROTOR DISC |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE391880C (en) * | 1921-05-14 | 1924-07-29 | Christian Lorenzen | Blade attachment for gas turbines with combustion air passed through the turbine blades |
US2402418A (en) * | 1943-01-20 | 1946-06-18 | Westinghouse Electric Corp | Turbine apparatus |
DE829685C (en) * | 1945-03-17 | 1952-01-28 | Bayerische Motoren Werke Ag | Attachment of the blades in the wheel disc, especially of exhaust gas turbines |
FR955013A (en) * | 1946-11-20 | 1950-01-07 | ||
FR970578A (en) * | 1948-08-19 | 1951-01-05 | Bohler & Cie Ag Geb | Hollow blades for turbines, in particular for gas turbines, and method for their manufacture |
FR981133A (en) * | 1949-02-21 | 1951-05-22 | Parsons C A & Co Ltd | Process for the manufacture of hollow blades for internal combustion turbines |
FR989043A (en) * | 1949-04-19 | 1951-09-04 | Rateau Soc | Blades for turbine engine wheels and in particular gas blades |
BE498667A (en) * | 1949-08-27 |
-
0
- NL NL81262D patent/NL81262C/xx active
- BE BE517285D patent/BE517285A/xx unknown
-
1952
- 1952-02-13 CH CH298592D patent/CH298592A/en unknown
-
1953
- 1953-01-28 GB GB2462/53A patent/GB728710A/en not_active Expired
- 1953-02-01 DE DEE6703A patent/DE942236C/en not_active Expired
- 1953-02-03 FR FR1070291D patent/FR1070291A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4767275A (en) * | 1986-07-11 | 1988-08-30 | Westinghouse Electric Corp. | Locking pin system for turbine curved root side entry closing blades |
Also Published As
Publication number | Publication date |
---|---|
CH298592A (en) | 1954-05-15 |
NL81262C (en) | |
DE942236C (en) | 1956-04-26 |
BE517285A (en) | |
FR1070291A (en) | 1954-07-21 |
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