FR2710103B1 - Turbomachine rotor flange and assembly of this flange with a rotor. - Google Patents
Turbomachine rotor flange and assembly of this flange with a rotor.Info
- Publication number
- FR2710103B1 FR2710103B1 FR9311025A FR9311025A FR2710103B1 FR 2710103 B1 FR2710103 B1 FR 2710103B1 FR 9311025 A FR9311025 A FR 9311025A FR 9311025 A FR9311025 A FR 9311025A FR 2710103 B1 FR2710103 B1 FR 2710103B1
- Authority
- FR
- France
- Prior art keywords
- flange
- rotor
- assembly
- turbomachine
- turbomachine rotor
- 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 - Lifetime
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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
- F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
-
- 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
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9311025A FR2710103B1 (en) | 1993-09-16 | 1993-09-16 | Turbomachine rotor flange and assembly of this flange with a rotor. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9311025A FR2710103B1 (en) | 1993-09-16 | 1993-09-16 | Turbomachine rotor flange and assembly of this flange with a rotor. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2710103A1 FR2710103A1 (en) | 1995-03-24 |
FR2710103B1 true FR2710103B1 (en) | 1995-10-20 |
Family
ID=9450923
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9311025A Expired - Lifetime FR2710103B1 (en) | 1993-09-16 | 1993-09-16 | Turbomachine rotor flange and assembly of this flange with a rotor. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2710103B1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19960896A1 (en) * | 1999-12-17 | 2001-06-28 | Rolls Royce Deutschland | Retaining device for rotor blades of axial turbine engine, with recesses in outer circumference of retainer corresponding to sections of blade receivers |
FR2814495B1 (en) * | 2000-09-28 | 2003-01-17 | Snecma Moteurs | UPSTREAM RETENTION SYSTEM FOR BLADES AND BLOWER PLATFORMS |
EP2679770A1 (en) * | 2012-06-26 | 2014-01-01 | Siemens Aktiengesellschaft | Platform seal strip for a gas turbine |
GB201604473D0 (en) | 2016-03-16 | 2016-04-27 | Rolls Royce Plc | A bladed rotor arrangement and a lock plate for a bladed rotor arrangement |
FR3049645B1 (en) * | 2016-03-30 | 2019-06-28 | Safran Aircraft Engines | ROTARY ASSEMBLY FOR TURBOMACHINE WITH ROUND JUNCTION IN U |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE792286A (en) * | 1971-12-06 | 1973-03-30 | Gen Electric | BOLTLESS AUBA RETAINER FOR TURBOMACHIN ROTOR |
FR2393931A1 (en) * | 1977-06-08 | 1979-01-05 | Snecma | DEVICE FOR HOLDING THE BLADES OF A ROTOR |
GB2006883B (en) * | 1977-10-27 | 1982-02-24 | Rolls Royce | Fan or compressor stage for a gas turbine engine |
FR2419389A1 (en) * | 1978-03-08 | 1979-10-05 | Snecma | IMPROVEMENTS TO TURBOMACHINE ROTOR FLANGES |
US4344740A (en) * | 1979-09-28 | 1982-08-17 | United Technologies Corporation | Rotor assembly |
US4304523A (en) * | 1980-06-23 | 1981-12-08 | General Electric Company | Means and method for securing a member to a structure |
FR2523208A1 (en) * | 1982-03-12 | 1983-09-16 | Snecma | DEVICE FOR DAMPING MOBILE TURBINE BLADE VIBRATIONS |
US4558988A (en) * | 1983-12-22 | 1985-12-17 | United Technologies Corporation | Rotor disk cover plate attachment |
US4890981A (en) * | 1988-12-30 | 1990-01-02 | General Electric Company | Boltless rotor blade retainer |
-
1993
- 1993-09-16 FR FR9311025A patent/FR2710103B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2710103A1 (en) | 1995-03-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CL | Concession to grant licenses | ||
CD | Change of name or company name | ||
TP | Transmission of property | ||
CD | Change of name or company name |