BE762044A - LOCKING DEVICE FOR THE FINS OF A TURBO-MACHINE - Google Patents
LOCKING DEVICE FOR THE FINS OF A TURBO-MACHINEInfo
- Publication number
- BE762044A BE762044A BE762044A BE762044A BE762044A BE 762044 A BE762044 A BE 762044A BE 762044 A BE762044 A BE 762044A BE 762044 A BE762044 A BE 762044A BE 762044 A BE762044 A BE 762044A
- Authority
- BE
- Belgium
- Prior art keywords
- turbo
- fins
- machine
- locking device
- locking
- Prior art date
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
-
- 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
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
- F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US757970A | 1970-02-02 | 1970-02-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE762044A true BE762044A (en) | 1971-07-01 |
Family
ID=21726999
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE762044A BE762044A (en) | 1970-02-02 | 1971-01-26 | LOCKING DEVICE FOR THE FINS OF A TURBO-MACHINE |
Country Status (5)
Country | Link |
---|---|
US (1) | US3597112A (en) |
BE (1) | BE762044A (en) |
DE (1) | DE2104511A1 (en) |
FR (1) | FR2078097A5 (en) |
GB (1) | GB1331711A (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3902824A (en) * | 1974-07-29 | 1975-09-02 | Gen Motors Corp | Blade lock |
CA1114301A (en) * | 1979-06-27 | 1981-12-15 | Ivor J. Roberts | Locking device for blade mounting |
GB2112465B (en) * | 1981-12-30 | 1985-04-11 | Rolls Royce | Turbomachine rotor |
FR2616480B1 (en) * | 1987-06-10 | 1989-09-29 | Snecma | DEVICE FOR LOCKING BLADES WITH A HAMMER FOOT ON A TURBOMACHINE DISC AND ASSEMBLY AND DISASSEMBLY METHODS |
GB2258273B (en) * | 1991-08-02 | 1994-08-10 | Ruston Gas Turbines Ltd | Rotor blade locking arrangement |
FR2758364B1 (en) * | 1997-01-16 | 1999-02-12 | Snecma | TRIPOD BLADE BLADE DISC |
DE19963346A1 (en) * | 1999-12-27 | 2001-07-05 | Abb Alstom Power Ch Ag | Blade assembly in a turbo-engine and method for fitting blades on a rotor fits blades on a rotor crosswise to their operating orientation with a butt end in a perimeter recess for twisting them into their operating orientation. |
US6739837B2 (en) | 2002-04-16 | 2004-05-25 | United Technologies Corporation | Bladed rotor with a tiered blade to hub interface |
GB0216951D0 (en) * | 2002-07-20 | 2002-08-28 | Rolls Royce Plc | A fan blade assembly |
US6837686B2 (en) * | 2002-09-27 | 2005-01-04 | Pratt & Whitney Canada Corp. | Blade retention scheme using a retention tab |
DE10351092B4 (en) * | 2003-10-31 | 2013-11-21 | MTU Aero Engines AG | Turbomachine and bladed rotor for a compressor stage of a turbomachine |
FR2997722B1 (en) * | 2012-11-06 | 2015-01-23 | Snecma | CIRCUMFERENTIAL BLOCKING DEVICE OF BLADE HAMMER FOR TURBOMACHINE, COMPRISING A WIRED SHAPE ACTUATION PART |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1085643B (en) * | 1959-04-13 | 1960-07-21 | Ehrhardt & Sehmer Ag Maschf | Blade attachment in axial flow machines |
GB903176A (en) * | 1960-01-18 | 1962-08-15 | Rolls Royce | Method of mounting a multi-blade set on a support member, for example to form a gas turbine compressor rotor |
US3252687A (en) * | 1965-02-01 | 1966-05-24 | Gen Motors Corp | Rotor blade locking |
US3383094A (en) * | 1967-01-19 | 1968-05-14 | Gen Electric | Rotor blade locking means |
-
1970
- 1970-02-02 US US7579A patent/US3597112A/en not_active Expired - Lifetime
-
1971
- 1971-01-26 BE BE762044A patent/BE762044A/en unknown
- 1971-02-01 DE DE19712104511 patent/DE2104511A1/en active Pending
- 1971-02-02 FR FR7103478A patent/FR2078097A5/fr not_active Expired
- 1971-04-19 GB GB2075271A patent/GB1331711A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2104511A1 (en) | 1971-08-12 |
FR2078097A5 (en) | 1971-11-05 |
US3597112A (en) | 1971-08-03 |
GB1331711A (en) | 1973-09-26 |
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