DE60121642D1 - Montage eines Rotors - Google Patents
Montage eines RotorsInfo
- Publication number
- DE60121642D1 DE60121642D1 DE60121642T DE60121642T DE60121642D1 DE 60121642 D1 DE60121642 D1 DE 60121642D1 DE 60121642 T DE60121642 T DE 60121642T DE 60121642 T DE60121642 T DE 60121642T DE 60121642 D1 DE60121642 D1 DE 60121642D1
- Authority
- DE
- Germany
- Prior art keywords
- rotor
- assembly
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/64—Mounting; Assembling; Disassembling of axial pumps
- F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
-
- 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
- F01D5/005—Repairing methods or devices
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/025—Fixing blade carrying members on shafts
-
- 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
- F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/70—Disassembly methods
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/80—Repairing, retrofitting or upgrading methods
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US710656 | 1991-06-05 | ||
US17921200P | 2000-01-31 | 2000-01-31 | |
US179212P | 2000-01-31 | ||
US09/710,656 US6375421B1 (en) | 2000-01-31 | 2000-11-09 | Piggyback rotor blisk |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60121642D1 true DE60121642D1 (de) | 2006-09-07 |
DE60121642T2 DE60121642T2 (de) | 2007-07-26 |
Family
ID=26875112
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60121642T Expired - Lifetime DE60121642T2 (de) | 2000-01-31 | 2001-01-31 | Montage eines Rotors |
Country Status (4)
Country | Link |
---|---|
US (1) | US6375421B1 (de) |
EP (1) | EP1122443B1 (de) |
JP (1) | JP4785256B2 (de) |
DE (1) | DE60121642T2 (de) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6354780B1 (en) * | 2000-09-15 | 2002-03-12 | General Electric Company | Eccentric balanced blisk |
DE10159669A1 (de) * | 2001-12-05 | 2003-07-03 | Rolls Royce Deutschland | Bajonettverbindung für ein Ringgehäuse eines Hochdruckkompressors einer Gasturbine |
GB2398882B (en) * | 2003-02-27 | 2007-09-05 | Rolls Royce Plc | Rotor balancing |
FR2857419B1 (fr) | 2003-07-11 | 2005-09-23 | Snecma Moteurs | Liaison amelioree entre disques aubages sur la ligne rotor d'un compresseur |
US7458774B2 (en) * | 2005-12-20 | 2008-12-02 | General Electric Company | High pressure turbine disk hub with curved hub surface and method |
DE102006033299A1 (de) * | 2006-07-17 | 2008-01-24 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zur Reparatur eines in BLISK-Bauweise ausgeführten Verdichterrotors |
DE102007031712A1 (de) * | 2007-07-06 | 2009-01-08 | Rolls-Royce Deutschland Ltd & Co Kg | Vorrichtung und Verfahren zum Einspannen von beschaufelten Rotorscheiben eines Strahltriebwerkes |
US8215919B2 (en) * | 2008-02-22 | 2012-07-10 | Hamilton Sundstrand Corporation | Curved tooth coupling for a miniature gas turbine engine |
GB0814314D0 (en) * | 2008-08-06 | 2008-09-10 | Rolls Royce Plc | A Method of assembling a multi-stage turbine or compressor |
DE102008060571A1 (de) * | 2008-12-04 | 2010-06-10 | Mtu Aero Engines Gmbh | Montagevorrichtung für ein Rotorsystem einer Axial-Strömungsmaschine |
US8998588B2 (en) * | 2011-08-18 | 2015-04-07 | General Electric Company | Segmented fan assembly |
US8932011B2 (en) * | 2011-10-06 | 2015-01-13 | United Technologies Corporation | Shaft assembly for a gas turbine engine |
US8935923B2 (en) * | 2011-10-25 | 2015-01-20 | United Technologies Corporation | Gas turbine engine with intercooling turbine section and intercooling turbine section bypass |
US9410446B2 (en) | 2012-07-10 | 2016-08-09 | United Technologies Corporation | Dynamic stability and mid axial preload control for a tie shaft coupled axial high pressure rotor |
US20140064976A1 (en) * | 2012-08-14 | 2014-03-06 | Kevin L. Corcoran | Rotor keyhole fillet for a gas turbine engine |
US10036316B2 (en) * | 2012-10-02 | 2018-07-31 | United Technologies Corporation | Geared turbofan engine with high compressor exit temperature |
EP2904254B8 (de) * | 2012-10-02 | 2020-11-04 | Raytheon Technologies Corporation | Getriebefan mit hoher verdichterausgangstemperatur |
US10060282B2 (en) * | 2014-06-10 | 2018-08-28 | United Technologies Corporation | Geared turbofan with integrally bladed rotor |
FR3066552B1 (fr) * | 2017-05-22 | 2021-11-19 | Safran Aircraft Engines | Assemblage sur un arbre de turbomachine d'un disque aubage monobloc et d'un rotor de compresseur basse pression a au moins deux etages d'aubes mobiles |
US11231043B2 (en) | 2018-02-21 | 2022-01-25 | General Electric Company | Gas turbine engine with ultra high pressure compressor |
US10823191B2 (en) | 2018-03-15 | 2020-11-03 | General Electric Company | Gas turbine engine arrangement with ultra high pressure compressor |
US11828190B2 (en) | 2021-11-18 | 2023-11-28 | General Electric Company | Airfoil joining apparatus and methods |
DE102022213569A1 (de) | 2022-12-13 | 2024-06-13 | Rolls-Royce Deutschland Ltd & Co Kg | Rotoranordnung, flugzeugtriebwerk und flugzeug |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1047281A (de) | 1964-01-23 | |||
GB1286235A (en) | 1970-01-20 | 1972-08-23 | Rolls Royce | A rotary bladed structure for a fluid flow machine |
US3742706A (en) | 1971-12-20 | 1973-07-03 | Gen Electric | Dual flow cooled turbine arrangement for gas turbine engines |
US4016636A (en) | 1974-07-23 | 1977-04-12 | United Technologies Corporation | Compressor construction |
JPS5115209A (en) * | 1974-07-29 | 1976-02-06 | Hitachi Ltd | Doyokunoshabanheno toritsukehohooyobi toritsukekozo |
US4664599A (en) * | 1985-05-01 | 1987-05-12 | United Technologies Corporation | Two stage turbine rotor assembly |
FR2607866B1 (fr) | 1986-12-03 | 1991-04-12 | Snecma | Axes de fixation de rotors de turbomachine, procede de montage et rotors ainsi montes |
GB8630754D0 (en) | 1986-12-23 | 1987-02-04 | Rolls Royce Plc | Turbofan gas turbine engine |
JPH057903U (ja) * | 1991-07-09 | 1993-02-02 | 石川島播磨重工業株式会社 | 部品の組付シート面補修構造 |
FR2712037B1 (fr) * | 1993-11-03 | 1995-12-08 | Snecma | Turbomachine à compresseur dont le rotor a un étage amont amovible. |
US5537814A (en) * | 1994-09-28 | 1996-07-23 | General Electric Company | High pressure gas generator rotor tie rod system for gas turbine engine |
US5628621A (en) * | 1996-07-26 | 1997-05-13 | General Electric Company | Reinforced compressor rotor coupling |
-
2000
- 2000-11-09 US US09/710,656 patent/US6375421B1/en not_active Expired - Lifetime
-
2001
- 2001-01-30 JP JP2001020890A patent/JP4785256B2/ja not_active Expired - Fee Related
- 2001-01-31 EP EP01300862A patent/EP1122443B1/de not_active Expired - Lifetime
- 2001-01-31 DE DE60121642T patent/DE60121642T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP4785256B2 (ja) | 2011-10-05 |
US6375421B1 (en) | 2002-04-23 |
EP1122443A3 (de) | 2003-04-02 |
EP1122443B1 (de) | 2006-07-26 |
JP2001254696A (ja) | 2001-09-21 |
EP1122443A2 (de) | 2001-08-08 |
DE60121642T2 (de) | 2007-07-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |