DE602004003840D1 - Vorrichtung zur Halterung eines ringförmigen Lagerschildes an einer radialen Seite eines Rotors - Google Patents
Vorrichtung zur Halterung eines ringförmigen Lagerschildes an einer radialen Seite eines RotorsInfo
- Publication number
- DE602004003840D1 DE602004003840D1 DE602004003840T DE602004003840T DE602004003840D1 DE 602004003840 D1 DE602004003840 D1 DE 602004003840D1 DE 602004003840 T DE602004003840 T DE 602004003840T DE 602004003840 T DE602004003840 T DE 602004003840T DE 602004003840 D1 DE602004003840 D1 DE 602004003840D1
- Authority
- DE
- Germany
- Prior art keywords
- rotor
- holding
- bearing plate
- annular bearing
- radial side
- 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
- F01D5/3007—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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
- Braking Arrangements (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0300436A FR2850130B1 (fr) | 2003-01-16 | 2003-01-16 | Dispositif pour retenir un flasque annulaire contre une face radiale d'un disque |
FR0300436 | 2003-01-16 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE602004003840D1 true DE602004003840D1 (de) | 2007-02-08 |
DE602004003840T2 DE602004003840T2 (de) | 2007-10-11 |
Family
ID=32524953
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602004003840T Expired - Lifetime DE602004003840T2 (de) | 2003-01-16 | 2004-01-13 | Vorrichtung zur Halterung eines ringförmigen Lagerschildes an einer radialen Seite eines Rotors |
Country Status (8)
Country | Link |
---|---|
US (1) | US7040866B2 (de) |
EP (1) | EP1439282B1 (de) |
JP (1) | JP4066264B2 (de) |
CA (1) | CA2456014C (de) |
DE (1) | DE602004003840T2 (de) |
ES (1) | ES2277660T3 (de) |
FR (1) | FR2850130B1 (de) |
RU (1) | RU2327062C2 (de) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2405183A (en) * | 2003-08-21 | 2005-02-23 | Rolls Royce Plc | Ring and channel arrangement for joining components |
FR2868808B1 (fr) * | 2004-04-09 | 2008-08-29 | Snecma Moteurs Sa | Dispositif de retenue axiale d'aubes sur un disque de rotor d'une turbomachine |
US7238008B2 (en) | 2004-05-28 | 2007-07-03 | General Electric Company | Turbine blade retainer seal |
FR2903154B1 (fr) * | 2006-06-29 | 2011-10-28 | Snecma | Rotor de turbomachine et turbomachine comportant un tel rotor |
FR2922587B1 (fr) * | 2007-10-22 | 2010-02-26 | Snecma | Roue de turbomachine |
US8313289B2 (en) | 2007-12-07 | 2012-11-20 | United Technologies Corp. | Gas turbine engine systems involving rotor bayonet coverplates and tools for installing such coverplates |
CN101676536B (zh) * | 2008-09-18 | 2013-04-24 | 中国航空工业第一集团公司沈阳发动机设计研究所 | 一种用于燃气涡轮发动机的弹性安装法兰 |
US8162615B2 (en) * | 2009-03-17 | 2012-04-24 | United Technologies Corporation | Split disk assembly for a gas turbine engine |
FR2955889B1 (fr) | 2010-01-29 | 2012-11-16 | Snecma | Moyen de blocage d'un flasque d'etancheite sur un disque de turbine |
DE102010015404B4 (de) * | 2010-04-19 | 2012-02-16 | Mtu Aero Engines Gmbh | Verfahren zur Reparatur einer Rotoranordnung einer Turbomaschine, Ringelement für eine Rotoranordnung einer Turbomaschine sowie Rotoranordnung für eine Turbomaschine |
US8870544B2 (en) * | 2010-07-29 | 2014-10-28 | United Technologies Corporation | Rotor cover plate retention method |
US8662845B2 (en) | 2011-01-11 | 2014-03-04 | United Technologies Corporation | Multi-function heat shield for a gas turbine engine |
US8740554B2 (en) | 2011-01-11 | 2014-06-03 | United Technologies Corporation | Cover plate with interstage seal for a gas turbine engine |
US8840375B2 (en) | 2011-03-21 | 2014-09-23 | United Technologies Corporation | Component lock for a gas turbine engine |
FR2973829B1 (fr) * | 2011-04-05 | 2013-05-24 | Snecma | Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant |
EP2514923A1 (de) * | 2011-04-18 | 2012-10-24 | MTU Aero Engines GmbH | Blendeneinrichtung, integral beschaufelter Rotorgrundkörper, Verfahren und Strömungsmaschine |
US8979502B2 (en) | 2011-12-15 | 2015-03-17 | Pratt & Whitney Canada Corp. | Turbine rotor retaining system |
US9212562B2 (en) * | 2012-07-18 | 2015-12-15 | United Technologies Corporation | Bayoneted anti-rotation turbine seals |
US9376926B2 (en) * | 2012-11-15 | 2016-06-28 | United Technologies Corporation | Gas turbine engine fan blade lock assembly |
US9567857B2 (en) | 2013-03-08 | 2017-02-14 | Rolls-Royce North American Technologies, Inc. | Turbine split ring retention and anti-rotation method |
EP2984303A4 (de) * | 2013-04-12 | 2016-12-21 | United Technologies Corp | Abdeckplatte für eine rotoranordnung eines gasturbinenmotors |
EP2933436A1 (de) * | 2014-04-15 | 2015-10-21 | Siemens Aktiengesellschaft | Radscheibe mit wenigstens einem Dichtblech |
FR3026430B1 (fr) * | 2014-09-29 | 2020-07-10 | Safran Aircraft Engines | Roue de turbine dans une turbomachine |
KR102182102B1 (ko) | 2014-11-27 | 2020-11-23 | 한화에어로스페이스 주식회사 | 터빈 장치 |
US10329929B2 (en) * | 2016-03-15 | 2019-06-25 | United Technologies Corporation | Retaining ring axially loaded against segmented disc surface |
US10323519B2 (en) * | 2016-06-23 | 2019-06-18 | United Technologies Corporation | Gas turbine engine having a turbine rotor with torque transfer and balance features |
US10968744B2 (en) | 2017-05-04 | 2021-04-06 | Rolls-Royce Corporation | Turbine rotor assembly having a retaining collar for a bayonet mount |
US10774678B2 (en) | 2017-05-04 | 2020-09-15 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
US10865646B2 (en) | 2017-05-04 | 2020-12-15 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
US20180320522A1 (en) * | 2017-05-04 | 2018-11-08 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
CN107196467B (zh) * | 2017-06-30 | 2023-09-29 | 广东美的环境电器制造有限公司 | 吊扇电机安装结构、吊扇及吊扇电机安装方法 |
FR3073001B1 (fr) * | 2017-10-26 | 2021-07-23 | Safran Aircraft Engines | Ensemble pour disque de turbine |
EP3564489A1 (de) * | 2018-05-03 | 2019-11-06 | Siemens Aktiengesellschaft | Rotor mit fliehkraft-optimierten kontaktflächen |
US10787921B2 (en) * | 2018-09-13 | 2020-09-29 | Raytheon Technologies Corporation | High pressure turbine rear side plate |
US20200095874A1 (en) * | 2018-09-26 | 2020-03-26 | Rolls-Royce North American Technologies Inc. | Turbine wheel assembly with platform retention features |
US11021974B2 (en) | 2018-10-10 | 2021-06-01 | Rolls-Royce North American Technologies Inc. | Turbine wheel assembly with retainer rings for ceramic matrix composite material blades |
FR3093131B1 (fr) * | 2019-02-22 | 2021-10-01 | Safran Aircraft Engines | Ensemble pour turbomachine |
CN111828107B (zh) * | 2020-07-24 | 2023-02-24 | 中国科学院工程热物理研究所 | 一种发动机涡轮转子叶片挡气盖板轴向限位结构 |
CN114762968B (zh) * | 2021-01-14 | 2024-07-16 | 中国航发商用航空发动机有限责任公司 | 叶片挡环安装工具和叶片挡环安装方法 |
CN113153445B (zh) * | 2021-04-15 | 2023-04-28 | 中国航发湖南动力机械研究所 | 涡轮发动机涡轮工作叶片的榫接结构和涡轮发动机 |
US11686202B1 (en) * | 2021-12-20 | 2023-06-27 | Rolls-Royce North American Technologies Inc. | Rotor damper with contact biasing feature for turbine engines |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4304523A (en) * | 1980-06-23 | 1981-12-08 | General Electric Company | Means and method for securing a member to a structure |
US4803893A (en) * | 1987-09-24 | 1989-02-14 | United Technologies Corporation | High speed rotor balance system |
US5018943A (en) * | 1989-04-17 | 1991-05-28 | General Electric Company | Boltless balance weight for turbine rotors |
US5472313A (en) * | 1991-10-30 | 1995-12-05 | General Electric Company | Turbine disk cooling system |
FR2695433B1 (fr) * | 1992-09-09 | 1994-10-21 | Snecma | Joint annulaire d'étanchéité disposé à une extrémité axiale d'un rotor et recouvrant des brochages d'aubes. |
GB2332024B (en) * | 1997-12-03 | 2000-12-13 | Rolls Royce Plc | Rotary assembly |
FR2812906B1 (fr) * | 2000-08-10 | 2002-09-20 | Snecma Moteurs | Bague de retention axiale d'un flasque sur un disque |
-
2003
- 2003-01-16 FR FR0300436A patent/FR2850130B1/fr not_active Expired - Fee Related
-
2004
- 2004-01-13 ES ES04290081T patent/ES2277660T3/es not_active Expired - Lifetime
- 2004-01-13 EP EP04290081A patent/EP1439282B1/de not_active Expired - Lifetime
- 2004-01-13 DE DE602004003840T patent/DE602004003840T2/de not_active Expired - Lifetime
- 2004-01-14 US US10/756,456 patent/US7040866B2/en active Active
- 2004-01-15 JP JP2004007609A patent/JP4066264B2/ja not_active Expired - Fee Related
- 2004-01-15 RU RU2004102064/11A patent/RU2327062C2/ru active
- 2004-01-15 CA CA2456014A patent/CA2456014C/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
ES2277660T3 (es) | 2007-07-16 |
RU2327062C2 (ru) | 2008-06-20 |
JP2004218642A (ja) | 2004-08-05 |
CA2456014A1 (fr) | 2004-07-16 |
CA2456014C (fr) | 2011-09-20 |
FR2850130A1 (fr) | 2004-07-23 |
US7040866B2 (en) | 2006-05-09 |
JP4066264B2 (ja) | 2008-03-26 |
RU2004102064A (ru) | 2005-06-20 |
US20050175459A1 (en) | 2005-08-11 |
DE602004003840T2 (de) | 2007-10-11 |
EP1439282B1 (de) | 2006-12-27 |
EP1439282A1 (de) | 2004-07-21 |
FR2850130B1 (fr) | 2006-01-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |