FR3003893B1 - Aube de turbomachine - Google Patents
Aube de turbomachineInfo
- Publication number
- FR3003893B1 FR3003893B1 FR1352967A FR1352967A FR3003893B1 FR 3003893 B1 FR3003893 B1 FR 3003893B1 FR 1352967 A FR1352967 A FR 1352967A FR 1352967 A FR1352967 A FR 1352967A FR 3003893 B1 FR3003893 B1 FR 3003893B1
- Authority
- FR
- France
- Prior art keywords
- dawn
- turbine
- turbine dawn
- 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.)
- Active
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 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
-
- 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
- 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
- F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
-
- 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
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1352967A FR3003893B1 (fr) | 2013-04-02 | 2013-04-02 | Aube de turbomachine |
US14/228,409 US9638049B2 (en) | 2013-04-02 | 2014-03-28 | Turbine engine blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1352967A FR3003893B1 (fr) | 2013-04-02 | 2013-04-02 | Aube de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3003893A1 FR3003893A1 (fr) | 2014-10-03 |
FR3003893B1 true FR3003893B1 (fr) | 2017-12-29 |
Family
ID=48771646
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1352967A Active FR3003893B1 (fr) | 2013-04-02 | 2013-04-02 | Aube de turbomachine |
Country Status (2)
Country | Link |
---|---|
US (1) | US9638049B2 (fr) |
FR (1) | FR3003893B1 (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2486488A (en) | 2010-12-17 | 2012-06-20 | Ge Aviat Systems Ltd | Testing a transient voltage protection device |
US9039382B2 (en) * | 2011-11-29 | 2015-05-26 | General Electric Company | Blade skirt |
FR3030613B1 (fr) * | 2014-12-18 | 2021-05-21 | Snecma | Aube mobile pour organe de turbomachine comprenant une nervure de rigidification |
RU174793U1 (ru) * | 2016-09-13 | 2017-11-02 | Общество с ограниченной ответственностью "Инжиниринговый центр "Газотурбинные технологии" | Рабочая лопатка турбомашины |
US10683765B2 (en) * | 2017-02-14 | 2020-06-16 | General Electric Company | Turbine blades having shank features and methods of fabricating the same |
FR3072122B1 (fr) * | 2017-10-11 | 2019-09-27 | Safran Aircraft Engines | Roue de turbomachine |
KR20190046118A (ko) * | 2017-10-25 | 2019-05-07 | 두산중공업 주식회사 | 터빈 블레이드 |
FR3075869B1 (fr) * | 2017-12-21 | 2020-01-10 | Safran Aircraft Engines | Roue mobile de turbine pour turbomachine d'aeronef, comprenant un anneau d'etancheite retenu radialement par des excroissances sur l'echasse des aubes |
FR3090032B1 (fr) * | 2018-12-12 | 2021-01-29 | Safran Aircraft Engines | Aube pour roue de turbomachine |
US11795826B2 (en) * | 2022-02-15 | 2023-10-24 | Rtx Corporation | Turbine blade neck pocket |
US12228052B2 (en) * | 2023-07-19 | 2025-02-18 | Pratt & Whitney Canada Corp. | Integrally bladed rotor with increased rim bending stiffness |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7097429B2 (en) * | 2004-07-13 | 2006-08-29 | General Electric Company | Skirted turbine blade |
US7121802B2 (en) * | 2004-07-13 | 2006-10-17 | General Electric Company | Selectively thinned turbine blade |
US8047797B2 (en) * | 2007-07-16 | 2011-11-01 | Nuovo Pignone Holdings, S.P.A. | Steam turbine and rotating blade |
FR2963383B1 (fr) * | 2010-07-27 | 2016-09-09 | Snecma | Aube de turbomachine, rotor, turbine basse pression et turbomachine equipes d'une telle aube |
EP2520768A1 (fr) * | 2011-05-02 | 2012-11-07 | MTU Aero Engines AG | Dispositif étanche pour un corps de base de rotor à aubage intégral d'une turbomachine |
US9546556B2 (en) * | 2012-09-26 | 2017-01-17 | United Technologies Corporation | Turbine blade root profile |
FR3006364B1 (fr) * | 2013-05-30 | 2018-07-13 | Safran Aircraft Engines | Roue de turbomachine, notamment pour turbine basse pression |
-
2013
- 2013-04-02 FR FR1352967A patent/FR3003893B1/fr active Active
-
2014
- 2014-03-28 US US14/228,409 patent/US9638049B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US9638049B2 (en) | 2017-05-02 |
FR3003893A1 (fr) | 2014-10-03 |
US20140294587A1 (en) | 2014-10-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR3001758B1 (fr) | Aube de rotor de turbomachine | |
FR3003893B1 (fr) | Aube de turbomachine | |
DK3060385T3 (da) | Vindmøllevinger | |
EP3086924C0 (fr) | Pales d'éoliennes | |
FR2989107B1 (fr) | Aube de rotor de turbomachine | |
DK3027385T3 (da) | Erosionsresistent aerodynamisk beklædning | |
DE102013107115B8 (de) | Schalldämpfer | |
GB201317924D0 (en) | Gas turbine engine | |
FR3015434B1 (fr) | Suspension de turbomachine | |
BR112014027901A2 (pt) | aerofólio de turbina | |
BR112014026785A2 (pt) | aerofólio de turbina. | |
DK3004635T3 (da) | Vindturbinestyring | |
BR112014026871A2 (pt) | aerofólio de turbina. | |
FR3012515B1 (fr) | Aube composite de turbomachine | |
FR3011888B1 (fr) | Piece de turbomachine a surface non-axisymetrique | |
GB2525117B (en) | Turbine Engine Impeller | |
FR2977908B1 (fr) | Aube de turbomachine | |
EP2960442A4 (fr) | Turbine à vapeur | |
DK3077661T3 (da) | Forbøjet vindmøllevinge | |
EP2703600A4 (fr) | Aube de turbine | |
BR112016011438A2 (pt) | ventilador de turbina | |
EP2719863A4 (fr) | Aube de turbine | |
FR3012539B1 (fr) | Compresseur radial | |
EP2975225A4 (fr) | Procédé de fabrication d'aube de turbine à vapeur | |
FR3012417B1 (fr) | Nacelle de turboreacteur |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 4 |
|
PLFP | Fee payment |
Year of fee payment: 5 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170707 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |