GB1331711A - Turbomachine rotor blade retaining means - Google Patents
Turbomachine rotor blade retaining meansInfo
- Publication number
- GB1331711A GB1331711A GB2075271A GB2075271A GB1331711A GB 1331711 A GB1331711 A GB 1331711A GB 2075271 A GB2075271 A GB 2075271A GB 2075271 A GB2075271 A GB 2075271A GB 1331711 A GB1331711 A GB 1331711A
- Authority
- GB
- United Kingdom
- Prior art keywords
- groove
- recess
- roots
- projection
- base
- 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
- 230000002093 peripheral effect Effects 0.000 abstract 1
- 230000000717 retained effect Effects 0.000 abstract 1
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 |
|---|---|
| GB1331711A true GB1331711A (en) | 1973-09-26 |
Family
ID=21726999
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2075271A Expired GB1331711A (en) | 1970-02-02 | 1971-04-19 | Turbomachine rotor blade retaining means |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3597112A (enExample) |
| BE (1) | BE762044A (enExample) |
| DE (1) | DE2104511A1 (enExample) |
| FR (1) | FR2078097A5 (enExample) |
| GB (1) | GB1331711A (enExample) |
Families Citing this family (13)
| 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 (fr) * | 1987-06-10 | 1989-09-29 | Snecma | Dispositif de verrouillage d'aubes a pied marteau sur un disque de turbomachine et procedes de montage et de demontage |
| GB2258273B (en) * | 1991-08-02 | 1994-08-10 | Ruston Gas Turbines Ltd | Rotor blade locking arrangement |
| FR2758364B1 (fr) * | 1997-01-16 | 1999-02-12 | Snecma | Disque aubage a aubes tripodes |
| DE19963346A1 (de) * | 1999-12-27 | 2001-07-05 | Abb Alstom Power Ch Ag | Schaufelanordnung einer Strömungsmaschine und Verfahren zur Montage |
| 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 (de) * | 2003-10-31 | 2013-11-21 | MTU Aero Engines AG | Turbomaschine und beschaufelter Rotor für eine Verdichterstufe einer Turbomaschine |
| FR2997722B1 (fr) * | 2012-11-06 | 2015-01-23 | Snecma | Dispositif de blocage circonferentiel d'aubes marteau pour turbomachine, comprenant une piece d'actionnement de forme filaire |
| FR3159192A1 (fr) * | 2024-02-08 | 2025-08-15 | Safran Aircraft Engines | Cale pour aube mobile de turbomachine |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1085643B (de) * | 1959-04-13 | 1960-07-21 | Ehrhardt & Sehmer Ag Maschf | Laufschaufelbefestigung bei Axialstroemungsmaschinen |
| 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/xx unknown
- 1971-02-01 DE DE19712104511 patent/DE2104511A1/de 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 (de) | 1971-08-12 |
| FR2078097A5 (enExample) | 1971-11-05 |
| US3597112A (en) | 1971-08-03 |
| BE762044A (fr) | 1971-07-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1331711A (en) | Turbomachine rotor blade retaining means | |
| SE8107451L (sv) | Lasning av rotorblad | |
| GB1040825A (en) | Improvements in rotor blades and/or stator blades for gas turbine engines | |
| GB1512882A (en) | Bladed rotor assembly for a gas turbine engine | |
| GB1533564A (en) | Device for locking turbomachinery blades | |
| GB1410607A (en) | Turbomachinery rotors | |
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| GB802476A (en) | Improvements in or relating to rotors of axial-flow fluid machines for example compressors and turbines | |
| GB996729A (en) | Improvements relating to turbines and compressors | |
| GB905582A (en) | Improvements relating to the sealing of blades in a bladed rotor | |
| GB1270203A (en) | Improvements in turbo machines | |
| GB1219994A (en) | Turbine for a compressible medium | |
| GB1326122A (en) | Blade securing arrangement for compressors and or turbines | |
| GB1187227A (en) | Improvements in Bladed Rotors for Axial Flow Compressors, Turbines and the like | |
| US3508844A (en) | Blade lock | |
| GB933047A (en) | Improvements in rotor assembly for gas turbine engines | |
| US3632228A (en) | Device for locking turbomachinery blades | |
| GB1492286A (en) | Means of locking parts mounted on the rotor of a turbomachine | |
| GB345359A (en) | Improvements in the mounting of blades in steam or gas turbines | |
| GB1353114A (en) | Turbo-machinery | |
| GB1276100A (en) | Bladed member for a fluid flow machine | |
| GB1141280A (en) | Bladed rotor for a fluid flow machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |