FR2075804A5 - - Google Patents
Info
- Publication number
- FR2075804A5 FR2075804A5 FR7101948A FR7101948A FR2075804A5 FR 2075804 A5 FR2075804 A5 FR 2075804A5 FR 7101948 A FR7101948 A FR 7101948A FR 7101948 A FR7101948 A FR 7101948A FR 2075804 A5 FR2075804 A5 FR 2075804A5
- Authority
- FR
- France
- 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
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2002469A DE2002469C3 (en) | 1970-01-21 | 1970-01-21 | Blade fastening in a dovetail-shaped circumferential groove of a rotor of flow machines with axial flow, in particular gas turbine jet engines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2075804A5 true FR2075804A5 (en) | 1971-10-08 |
Family
ID=5760103
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7101948A Expired FR2075804A5 (en) | 1970-01-21 | 1971-01-21 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3778191A (en) |
DE (1) | DE2002469C3 (en) |
FR (1) | FR2075804A5 (en) |
GB (1) | GB1326122A (en) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3902824A (en) * | 1974-07-29 | 1975-09-02 | Gen Motors Corp | Blade lock |
GB2119026B (en) * | 1981-03-25 | 1984-06-20 | Rolls Royce | Aerofoil blade mounting |
JPS57168005A (en) * | 1981-04-10 | 1982-10-16 | Hitachi Ltd | Rotor structue for axial machines |
US4684326A (en) * | 1982-08-16 | 1987-08-04 | Terry Corporation | Bladed rotor assembly, and method of forming same |
GB2156908A (en) * | 1984-03-30 | 1985-10-16 | Rolls Royce | Bladed rotor assembly for gas turbine engine |
US4907944A (en) * | 1984-10-01 | 1990-03-13 | General Electric Company | Turbomachinery blade mounting arrangement |
JPH0658168A (en) * | 1992-08-06 | 1994-03-01 | Hitachi Ltd | Compressor for gas turbine and gas turbine |
DE10351092B4 (en) * | 2003-10-31 | 2013-11-21 | MTU Aero Engines AG | Turbomachine and bladed rotor for a compressor stage of a turbomachine |
DE102004011508A1 (en) | 2004-03-08 | 2005-09-29 | Alstom Technology Ltd | Rotor end |
DE102004051116A1 (en) * | 2004-10-20 | 2006-04-27 | Mtu Aero Engines Gmbh | Rotor of a turbomachine, in particular gas turbine rotor |
EP1698759B1 (en) * | 2005-02-23 | 2015-06-03 | Alstom Technology Ltd | Rotor end piece |
FR2900989B1 (en) * | 2006-05-12 | 2008-07-11 | Snecma Sa | AIRCRAFT ENGINE COMPRESSOR ASSEMBLY COMPRISING AUBES WITH FOOT HAMMER ATTACHMENT |
US8899933B2 (en) * | 2012-01-03 | 2014-12-02 | General Electric Company | Rotor blade mounting |
US9828865B2 (en) | 2012-09-26 | 2017-11-28 | United Technologies Corporation | Turbomachine rotor groove |
US9404367B2 (en) * | 2012-11-21 | 2016-08-02 | Solar Turbines Incorporated | Gas turbine engine compressor rotor assembly and balancing system |
US11242761B2 (en) * | 2020-02-18 | 2022-02-08 | Raytheon Technologies Corporation | Tangential rotor blade slot spacer for a gas turbine engine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US995367A (en) * | 1909-03-01 | 1911-06-13 | Allis Chalmers | Steam-turbine. |
US1539574A (en) * | 1922-04-18 | 1925-05-26 | Westinghouse Electric & Mfg Co | Turbine-blade fastening |
US2857134A (en) * | 1954-03-17 | 1958-10-21 | Parsons C A & Co Ltd | Assembly of blades for turbines and the like |
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 |
GB916001A (en) * | 1961-02-09 | 1963-01-16 | Prvni Brnenska Strojirna | Improvements in or relating to rotors for turbines and compressors |
US3216700A (en) * | 1963-10-24 | 1965-11-09 | Gen Electric | Rotor blade locking means |
-
1970
- 1970-01-21 DE DE2002469A patent/DE2002469C3/en not_active Expired
-
1971
- 1971-01-21 FR FR7101948A patent/FR2075804A5/fr not_active Expired
- 1971-01-21 US US00108350A patent/US3778191A/en not_active Expired - Lifetime
- 1971-04-19 GB GB2003971A patent/GB1326122A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB1326122A (en) | 1973-08-08 |
DE2002469A1 (en) | 1971-07-29 |
DE2002469C3 (en) | 1978-03-30 |
US3778191A (en) | 1973-12-11 |
DE2002469B2 (en) | 1977-08-11 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |