DE60321623D1 - Gebläseschaufelanordnung - Google Patents
GebläseschaufelanordnungInfo
- Publication number
- DE60321623D1 DE60321623D1 DE60321623T DE60321623T DE60321623D1 DE 60321623 D1 DE60321623 D1 DE 60321623D1 DE 60321623 T DE60321623 T DE 60321623T DE 60321623 T DE60321623 T DE 60321623T DE 60321623 D1 DE60321623 D1 DE 60321623D1
- Authority
- DE
- Germany
- Prior art keywords
- fan blade
- blade assembly
- assembly
- fan
- 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 - 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
- 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
- F01D5/323—Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/50—Vibration damping features
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0216951.4A GB0216951D0 (en) | 2002-07-20 | 2002-07-20 | A fan blade assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
DE60321623D1 true DE60321623D1 (de) | 2008-07-31 |
Family
ID=9940878
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60321623T Expired - Lifetime DE60321623D1 (de) | 2002-07-20 | 2003-06-25 | Gebläseschaufelanordnung |
Country Status (4)
Country | Link |
---|---|
US (1) | US6905311B2 (de) |
EP (1) | EP1382800B1 (de) |
DE (1) | DE60321623D1 (de) |
GB (1) | GB0216951D0 (de) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8616849B2 (en) * | 2009-02-18 | 2013-12-31 | Pratt & Whitney Canada Corp. | Fan blade platform |
US8568102B2 (en) * | 2009-02-18 | 2013-10-29 | Pratt & Whitney Canada Corp. | Fan blade anti-fretting insert |
US8834123B2 (en) * | 2009-12-29 | 2014-09-16 | Rolls-Royce Corporation | Turbomachinery component |
US8708656B2 (en) | 2010-05-25 | 2014-04-29 | Pratt & Whitney Canada Corp. | Blade fixing design for protecting against low speed rotation induced wear |
US9739160B2 (en) | 2013-10-18 | 2017-08-22 | Siemens Aktiengesellschaft | Adjustable blade root spring for turbine blade fixation in turbomachinery |
US9909431B2 (en) | 2013-10-18 | 2018-03-06 | Siemens Energy, Inc. | Variable dual spring blade root support for gas turbines |
US9896946B2 (en) | 2013-10-31 | 2018-02-20 | General Electric Company | Gas turbine engine rotor assembly and method of assembling the same |
US9970297B2 (en) * | 2014-08-29 | 2018-05-15 | Rolls-Royce Corporation | Composite fan slider with nano-coating |
US10215035B2 (en) * | 2014-12-29 | 2019-02-26 | Rolls-Royce North American Technologies Inc. | Turbine wheels with preloaded blade attachment |
GB201503303D0 (en) | 2015-02-27 | 2015-04-15 | Rolls Royce Plc | Retention device |
GB201504186D0 (en) * | 2015-03-12 | 2015-04-29 | Rolls Royce Plc | Chocking and retaining device |
FR3034130B1 (fr) * | 2015-03-25 | 2018-04-06 | Safran Aircraft Engines | Demontage d'aubes de soufflante |
FR3038653B1 (fr) * | 2015-07-08 | 2017-08-04 | Snecma | Assemblage d'une plateforme rapportee d'aube de soufflante sur un disque de soufflante |
US10208709B2 (en) * | 2016-04-05 | 2019-02-19 | United Technologies Corporation | Fan blade removal feature for a gas turbine engine |
IT201600130088A1 (it) * | 2016-12-22 | 2018-06-22 | Nuovo Pignone Tecnologie Srl | Pala di turbina e set di fissaggio |
FR3102206B1 (fr) * | 2019-10-18 | 2023-02-17 | Safran Aircraft Engines | Ensemble pour une aube de turbomachine comprenant une attache définissant une alvéole et une cale adaptée pour être reçue dans l’alvéole en même temps qu’un pied de l’aube |
CN114109512A (zh) | 2020-08-25 | 2022-03-01 | 通用电气公司 | 叶片燕尾榫和保持设备 |
KR102478172B1 (ko) * | 2021-02-02 | 2022-12-14 | 두산에너빌리티 주식회사 | 회전 기계, 이를 포함하는 가스 터빈, 회전 기계의 조립 방법 |
FR3132078B1 (fr) * | 2022-01-24 | 2023-12-08 | Safran Aircraft Engines | Ensemble de fixation pour une aube pour turbomachine |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3383095A (en) * | 1967-09-12 | 1968-05-14 | Gen Electric | Lock for turbomachinery blades |
US3597112A (en) * | 1970-02-02 | 1971-08-03 | Gen Electric | Compressor-blade-retaining means |
US3936234A (en) | 1975-02-10 | 1976-02-03 | General Electric Company | Device for locking turbomachinery blades |
US4208170A (en) | 1978-05-18 | 1980-06-17 | General Electric Company | Blade retainer |
US4265595A (en) | 1979-01-02 | 1981-05-05 | General Electric Company | Turbomachinery blade retaining assembly |
FR2519072B1 (fr) * | 1981-12-29 | 1986-05-30 | Snecma | Dispositif de retenue axiale et radiale d'aube de rotor de turboreacteur |
FR2535794A1 (fr) * | 1982-11-08 | 1984-05-11 | Snecma | Dispositif de retenue axiale et radiale d'aubes de soufflante |
US5236309A (en) * | 1991-04-29 | 1993-08-17 | Westinghouse Electric Corp. | Turbine blade assembly |
GB9223593D0 (en) * | 1992-11-11 | 1992-12-23 | Rolls Royce Plc | Gas turbine engine fan blade assembly |
GB9412963D0 (en) | 1994-06-28 | 1994-09-28 | Rolls Royce Plc | Gas turbine engine fan blade assembly |
FR2807096B1 (fr) * | 2000-03-30 | 2002-05-31 | Abb Alstom Power Nv | Disque rotorique de turbine equipe d'ailettes a pied de sapin et procede de montage d'une ailette sur un disque |
-
2002
- 2002-07-20 GB GBGB0216951.4A patent/GB0216951D0/en not_active Ceased
-
2003
- 2003-06-25 EP EP03254003A patent/EP1382800B1/de not_active Expired - Fee Related
- 2003-06-25 DE DE60321623T patent/DE60321623D1/de not_active Expired - Lifetime
- 2003-06-27 US US10/607,187 patent/US6905311B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1382800A3 (de) | 2006-08-23 |
GB0216951D0 (en) | 2002-08-28 |
US20040013528A1 (en) | 2004-01-22 |
EP1382800A2 (de) | 2004-01-21 |
EP1382800B1 (de) | 2008-06-18 |
US6905311B2 (en) | 2005-06-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |