GB277663A - Improvements in or relating to turbines - Google Patents
Improvements in or relating to turbinesInfo
- Publication number
- GB277663A GB277663A GB24035/27A GB2403527A GB277663A GB 277663 A GB277663 A GB 277663A GB 24035/27 A GB24035/27 A GB 24035/27A GB 2403527 A GB2403527 A GB 2403527A GB 277663 A GB277663 A GB 277663A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- lorenzen
- ges
- rotor
- flanges
- 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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- F01D5/3069—Fixing blades to rotors; Blade roots ; Blade spacers between two discs or rings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
277,663. Lorenzen-Turbinen Akt.- Ges., (Assignees of Lorenzen Ges., C.). Sept. 20, 1926, [Convention date]. Blades.-Turbine blades whih may be hollow are formed with head portions and a number of blades are joined together by welding the beads to form a unit which may be set into or removed from the rotor in which it is secured by root portions on the blades. The form shown consists of a number of blades 1 having outer head portions 2, welded together to form a continuous ring with grooved side rings 8 connected thereto, and root portions 3 which are secured beneath flanges 5 when the two parts 6<1> forming the rotor are bolted together. The flanges 5 may have teeth 12 fitting between the blades. The grooved side rings 8 form a packing device with a corresponding flange on the stator.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE277663X | 1926-09-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB277663A true GB277663A (en) | 1928-01-26 |
Family
ID=6028362
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24035/27A Expired GB277663A (en) | 1926-09-20 | 1927-09-13 | Improvements in or relating to turbines |
Country Status (3)
Country | Link |
---|---|
US (1) | US1876067A (en) |
FR (1) | FR641068A (en) |
GB (1) | GB277663A (en) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3083446A (en) * | 1950-06-14 | 1963-04-02 | Stalker Corp | Rotor construction |
BE570267A (en) * | 1957-08-16 | |||
US3070350A (en) * | 1958-06-02 | 1962-12-25 | Gen Motors Corp | Rotor shroud |
US3014691A (en) * | 1958-06-04 | 1961-12-26 | Edward A Stalker | Turbine rotor |
US3065955A (en) * | 1958-12-29 | 1962-11-27 | Gen Electric | Rotor blade and shroud assembly |
US3357082A (en) * | 1963-02-13 | 1967-12-12 | Whiton Machine Company | Method of making a turbine wheel |
FR2051912A5 (en) * | 1969-07-01 | 1971-04-09 | Rabouyt Denis | |
FR2514409B1 (en) * | 1981-10-09 | 1986-03-21 | Snecma | DEVICE FOR LAYING BLADES IN SECTORS ON A TURBOMACHINE ROTOR DISC |
US5486095A (en) * | 1994-12-08 | 1996-01-23 | General Electric Company | Split disk blade support |
US6508624B2 (en) * | 2001-05-02 | 2003-01-21 | Siemens Automotive, Inc. | Turbomachine with double-faced rotor-shroud seal structure |
DE102008008887A1 (en) * | 2008-02-13 | 2009-08-27 | Man Turbo Ag | Multi-piece bladed rotor for a turbomachine |
FR2940350B1 (en) | 2008-12-23 | 2011-03-18 | Snecma | MOBILE WHEEL OF TURBOMACHINE A AUBES COMPOSITE MATERIAL HAVING A SPRING RING. |
FR2940353B1 (en) * | 2008-12-23 | 2011-02-11 | Snecma | MOBILE WHEEL OF TURBOMACHINE A AUBES IN COMPOSITE MATERIAL. |
US8162615B2 (en) * | 2009-03-17 | 2012-04-24 | United Technologies Corporation | Split disk assembly for a gas turbine engine |
FR2967453B1 (en) * | 2010-11-17 | 2012-12-21 | Snecma | AUBES RETENTION DISC |
US10787917B2 (en) * | 2018-05-04 | 2020-09-29 | Rolls-Royce North American Technologies Inc. | Multi-piece turbine disk for ceramic matrix composite components |
-
1927
- 1927-09-13 GB GB24035/27A patent/GB277663A/en not_active Expired
- 1927-09-15 US US219600A patent/US1876067A/en not_active Expired - Lifetime
- 1927-09-17 FR FR641068D patent/FR641068A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR641068A (en) | 1928-07-27 |
US1876067A (en) | 1932-09-06 |
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