DE69400079D1 - Turbomaschinenrotor mit Schaufelnbefestigung durch Stifte - Google Patents
Turbomaschinenrotor mit Schaufelnbefestigung durch StifteInfo
- Publication number
- DE69400079D1 DE69400079D1 DE69400079T DE69400079T DE69400079D1 DE 69400079 D1 DE69400079 D1 DE 69400079D1 DE 69400079 T DE69400079 T DE 69400079T DE 69400079 T DE69400079 T DE 69400079T DE 69400079 D1 DE69400079 D1 DE 69400079D1
- Authority
- DE
- Germany
- Prior art keywords
- pins
- turbo machine
- machine rotor
- blade attachment
- blade
- 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 - Fee Related
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
- F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
-
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9300276A FR2700362B1 (fr) | 1993-01-14 | 1993-01-14 | Rotor de turbomachine à attaches d'aubes par broches. |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69400079D1 true DE69400079D1 (de) | 1996-04-11 |
DE69400079T2 DE69400079T2 (de) | 1996-09-12 |
Family
ID=9443009
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69400079T Expired - Fee Related DE69400079T2 (de) | 1993-01-14 | 1994-01-12 | Turbomaschinenrotor mit Schaufelnbefestigung durch Stifte |
Country Status (5)
Country | Link |
---|---|
US (1) | US5409353A (de) |
EP (1) | EP0607082B1 (de) |
JP (1) | JP2807624B2 (de) |
DE (1) | DE69400079T2 (de) |
FR (1) | FR2700362B1 (de) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5725353A (en) * | 1996-12-04 | 1998-03-10 | United Technologies Corporation | Turbine engine rotor disk |
US5735673A (en) * | 1996-12-04 | 1998-04-07 | United Technologies Corporation | Turbine engine rotor blade pair |
DE10310994B4 (de) * | 2003-03-06 | 2006-09-07 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Rotor für ein Turbinentriebwerk |
US20050068646A1 (en) * | 2003-09-25 | 2005-03-31 | Homedics, Inc. | Mirror with adjustable magnification and with a plurality of displays and devices |
US8556531B1 (en) * | 2006-11-17 | 2013-10-15 | United Technologies Corporation | Simple CMC fastening system |
FR2925015B1 (fr) * | 2007-12-14 | 2010-06-04 | Eurocopter France | Pale de giravion, rotor de giravion muni de ladite pale, et procede de fabrication de cette pale |
EP2322763A1 (de) * | 2009-11-17 | 2011-05-18 | Siemens Aktiengesellschaft | Turbinen- oder Verdichterschaufel |
FR2963055B1 (fr) * | 2010-07-21 | 2014-01-31 | Snecma | Aube de rotor d'un turbomoteur a gaz en materiau composite comprenant une chape de liaison, procede de fabrication de l'aube |
FR2990462B1 (fr) * | 2012-05-14 | 2014-05-30 | Snecma | Dispositif d'attache d'aubes sur un disque de rotor de turbomachine |
FR2995004B1 (fr) * | 2012-09-03 | 2015-03-20 | Snecma | Aube de turbomachine en materiau composite et son attache sur un disque de rotor |
US9470092B2 (en) * | 2013-01-02 | 2016-10-18 | General Electric Company | System and method for attaching a rotating blade in a turbine |
EP3034783B1 (de) * | 2014-12-17 | 2019-11-20 | Rolls-Royce Deutschland Ltd & Co KG | Schaufelanordnung eines Strahltriebwerks oder eines Flugzeugpropellers und zugehöriges Triebwerk |
US10677075B2 (en) * | 2018-05-04 | 2020-06-09 | General Electric Company | Composite airfoil assembly for an interdigitated rotor |
US11306601B2 (en) | 2018-10-18 | 2022-04-19 | Raytheon Technologies Corporation | Pinned airfoil for gas turbine engines |
US11092020B2 (en) * | 2018-10-18 | 2021-08-17 | Raytheon Technologies Corporation | Rotor assembly for gas turbine engines |
US11208892B2 (en) * | 2020-01-17 | 2021-12-28 | Raytheon Technologies Corporation | Rotor assembly with multiple rotor disks |
US11371351B2 (en) | 2020-01-17 | 2022-06-28 | Raytheon Technologies Corporation | Multi-disk bladed rotor assembly for rotational equipment |
US11156110B1 (en) | 2020-08-04 | 2021-10-26 | General Electric Company | Rotor assembly for a turbine section of a gas turbine engine |
US11655719B2 (en) | 2021-04-16 | 2023-05-23 | General Electric Company | Airfoil assembly |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE872416C (de) * | 1943-07-23 | 1953-04-27 | Versuchsanstalt Fuer Luftfahrt | Hohlschaufelturbine mit aus Blech gefalteten Schaufeln |
NL248261A (de) * | 1959-02-12 | |||
US3014695A (en) * | 1960-02-03 | 1961-12-26 | Gen Electric | Turbine bucket retaining means |
US3694104A (en) * | 1970-10-07 | 1972-09-26 | Garrett Corp | Turbomachinery blade |
DE2441249C3 (de) * | 1974-08-28 | 1979-01-04 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Axiallaufrad für hochtourige Turbomaschinen |
US4098559A (en) * | 1976-07-26 | 1978-07-04 | United Technologies Corporation | Paired blade assembly |
DE3826378A1 (de) * | 1988-08-03 | 1990-02-08 | Mtu Muenchen Gmbh | Fasertechnische propellerschaufeln |
FR2654773B1 (fr) * | 1989-11-22 | 1992-02-14 | Snecma | Rotor de turbomachine a flux axial. |
-
1993
- 1993-01-14 FR FR9300276A patent/FR2700362B1/fr not_active Expired - Fee Related
-
1994
- 1994-01-12 DE DE69400079T patent/DE69400079T2/de not_active Expired - Fee Related
- 1994-01-12 EP EP94400066A patent/EP0607082B1/de not_active Expired - Lifetime
- 1994-01-13 US US08/181,086 patent/US5409353A/en not_active Expired - Fee Related
- 1994-01-14 JP JP6002747A patent/JP2807624B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2700362B1 (fr) | 1995-02-10 |
US5409353A (en) | 1995-04-25 |
DE69400079T2 (de) | 1996-09-12 |
JP2807624B2 (ja) | 1998-10-08 |
JPH06241002A (ja) | 1994-08-30 |
EP0607082A1 (de) | 1994-07-20 |
FR2700362A1 (fr) | 1994-07-13 |
EP0607082B1 (de) | 1996-03-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: SNECMA MOTEURS, PARIS, FR |
|
8339 | Ceased/non-payment of the annual fee |