NO20071071L - Rotorblad for et andre trinn i en kompressor. - Google Patents
Rotorblad for et andre trinn i en kompressor.Info
- Publication number
- NO20071071L NO20071071L NO20071071A NO20071071A NO20071071L NO 20071071 L NO20071071 L NO 20071071L NO 20071071 A NO20071071 A NO 20071071A NO 20071071 A NO20071071 A NO 20071071A NO 20071071 L NO20071071 L NO 20071071L
- Authority
- NO
- Norway
- Prior art keywords
- blade
- rotor
- compressor
- itself
- axis
- Prior art date
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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
-
- 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
- F04D29/324—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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- 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
- F01D5/288—Protective coatings for blades
-
- 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
- F04D29/38—Blades
-
- 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
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/668—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/74—Shape given by a set or table of xyz-coordinates
-
- 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
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Operation Control Of Excavators (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
Oppfinnelsen gjelder et blad (10) tilhørende en rotor i et andre trinn i en kompressor. Rotoren kan fastlegges ut fra koordinatene for en diskret kombinasjon av punkter i et kartesisk koordinatsystem (x, y, z), hvor z-aksen er en radial akse som skjærer kompressorens sentrale akse. Bladet (10) har en profil som kan fastlegges ved hjelp av en rekke lukkede skjæringskurver mellom selve profilen og et plan (x, y) i en avstand (z) fra den sentrale akse. Bladet (10) omfatter videre en fortykning (30) som i alt vesentlig strekker seg parallelt med en base (12) av selve bladet (10). Basen er egnet til å feste bladet til rotoren, og fortykningen (30) er i alt vesentlig anordnet midtveis opp på dette og er egnet for å forskyve selve bladets (10) naturlige resonansfrekvenser til et område utenfor rotorens funksj onshastighetsområde.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT000340A ITMI20060340A1 (it) | 2006-02-27 | 2006-02-27 | Pala di un rotore di un secondo stadio di un compressore |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NO20071071L true NO20071071L (no) | 2007-08-28 |
Family
ID=38037459
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO20071071A NO20071071L (no) | 2006-02-27 | 2007-02-26 | Rotorblad for et andre trinn i en kompressor. |
Country Status (8)
| Country | Link |
|---|---|
| US (2) | US7766624B2 (no) |
| EP (1) | EP1826414B1 (no) |
| JP (1) | JP5314851B2 (no) |
| KR (1) | KR101433374B1 (no) |
| CN (1) | CN101029648B (no) |
| CA (1) | CA2579383C (no) |
| IT (1) | ITMI20060340A1 (no) |
| NO (1) | NO20071071L (no) |
Families Citing this family (59)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7329093B2 (en) * | 2006-01-27 | 2008-02-12 | General Electric Company | Nozzle blade airfoil profile for a turbine |
| US7329092B2 (en) * | 2006-01-27 | 2008-02-12 | General Electric Company | Stator blade airfoil profile for a compressor |
| US7306436B2 (en) * | 2006-03-02 | 2007-12-11 | Pratt & Whitney Canada Corp. | HP turbine blade airfoil profile |
| US7581930B2 (en) * | 2006-08-16 | 2009-09-01 | United Technologies Corporation | High lift transonic turbine blade |
| US7611326B2 (en) * | 2006-09-06 | 2009-11-03 | Pratt & Whitney Canada Corp. | HP turbine vane airfoil profile |
| US7513748B2 (en) * | 2006-10-25 | 2009-04-07 | General Electric Company | Airfoil shape for a compressor |
| US7517197B2 (en) * | 2006-10-25 | 2009-04-14 | General Electric Company | Airfoil shape for a compressor |
| US7510378B2 (en) * | 2006-10-25 | 2009-03-31 | General Electric Company | Airfoil shape for a compressor |
| US7530793B2 (en) * | 2006-10-25 | 2009-05-12 | General Electric Company | Airfoil shape for a compressor |
| US7566202B2 (en) * | 2006-10-25 | 2009-07-28 | General Electric Company | Airfoil shape for a compressor |
| US7520729B2 (en) * | 2006-10-25 | 2009-04-21 | General Electric Company | Airfoil shape for a compressor |
| US7572104B2 (en) * | 2006-10-25 | 2009-08-11 | General Electric Company | Airfoil shape for a compressor |
| US7572105B2 (en) * | 2006-10-25 | 2009-08-11 | General Electric Company | Airfoil shape for a compressor |
| US7537434B2 (en) * | 2006-11-02 | 2009-05-26 | General Electric Company | Airfoil shape for a compressor |
| US7497665B2 (en) * | 2006-11-02 | 2009-03-03 | General Electric Company | Airfoil shape for a compressor |
| US7568892B2 (en) * | 2006-11-02 | 2009-08-04 | General Electric Company | Airfoil shape for a compressor |
| US7559748B2 (en) * | 2006-11-28 | 2009-07-14 | Pratt & Whitney Canada Corp. | LP turbine blade airfoil profile |
| US8057188B2 (en) * | 2008-05-21 | 2011-11-15 | Alstom Technologies Ltd. Llc | Compressor airfoil |
| EP2241761A1 (en) * | 2009-04-09 | 2010-10-20 | Alstom Technology Ltd | Blade for an Axial Compressor and Manufacturing Method Thereof |
| US8573945B2 (en) * | 2009-11-13 | 2013-11-05 | Alstom Technology Ltd. | Compressor stator vane |
| IT1401661B1 (it) | 2010-08-25 | 2013-08-02 | Nuova Pignone S R L | Forma di profilo areodinamico per compressore. |
| US8215917B2 (en) * | 2010-08-31 | 2012-07-10 | General Electric Company | Airfoil shape for a compressor |
| CA146333S (en) * | 2012-02-02 | 2013-02-07 | Novenco As | Ventilator blade |
| US9133713B2 (en) * | 2012-07-02 | 2015-09-15 | United Technologies Corporation | Gas turbine engine turbine blade airfoil profile |
| US8979499B2 (en) * | 2012-08-17 | 2015-03-17 | United Technologies Corporation | Gas turbine engine airfoil profile |
| US9506347B2 (en) * | 2012-12-19 | 2016-11-29 | Solar Turbines Incorporated | Compressor blade for gas turbine engine |
| US9523284B2 (en) * | 2013-11-22 | 2016-12-20 | General Electric Technology Gmbh | Adjusted stationary airfoil |
| EP3108103B1 (en) | 2014-02-19 | 2023-09-27 | Raytheon Technologies Corporation | Fan blade for a gas turbine engine |
| US10495106B2 (en) | 2014-02-19 | 2019-12-03 | United Technologies Corporation | Gas turbine engine airfoil |
| US10570915B2 (en) | 2014-02-19 | 2020-02-25 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015175073A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| US10570916B2 (en) | 2014-02-19 | 2020-02-25 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015175043A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015126941A1 (en) * | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108120B1 (en) | 2014-02-19 | 2021-03-31 | Raytheon Technologies Corporation | Gas turbine engine having a geared architecture and a specific fixed airfoil structure |
| WO2015175044A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3575551B1 (en) | 2014-02-19 | 2021-10-27 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
| EP3108123B1 (en) | 2014-02-19 | 2023-10-04 | Raytheon Technologies Corporation | Turbofan engine with geared architecture and lpc airfoils |
| WO2015175052A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| US10584715B2 (en) | 2014-02-19 | 2020-03-10 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108106B1 (en) | 2014-02-19 | 2022-05-04 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
| US10465702B2 (en) | 2014-02-19 | 2019-11-05 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108101B1 (en) | 2014-02-19 | 2022-04-20 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
| EP3985226B1 (en) | 2014-02-19 | 2024-12-25 | RTX Corporation | Gas turbine engine airfoil |
| US9567858B2 (en) | 2014-02-19 | 2017-02-14 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015126454A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| US9140127B2 (en) | 2014-02-19 | 2015-09-22 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108100B1 (en) | 2014-02-19 | 2021-04-14 | Raytheon Technologies Corporation | Gas turbine engine fan blade |
| EP3108105B1 (en) | 2014-02-19 | 2021-05-12 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
| CN104265681B (zh) * | 2014-08-01 | 2016-08-31 | 中国人民解放军第五七一九工厂 | 改变叶片自身固有频率的方法 |
| FR3032494B1 (fr) * | 2015-02-06 | 2018-05-25 | Safran Aircraft Engines | Aube de soufflante |
| US10443393B2 (en) * | 2016-07-13 | 2019-10-15 | Safran Aircraft Engines | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the seventh stage of a turbine |
| US10443392B2 (en) * | 2016-07-13 | 2019-10-15 | Safran Aircraft Engines | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine |
| GB201813666D0 (en) * | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Fan blade |
| US10677065B2 (en) * | 2018-09-27 | 2020-06-09 | General Electric Company | Airfoil shape for second stage compressor rotor blade |
| KR102411655B1 (ko) | 2019-08-23 | 2022-06-21 | 두산에너빌리티 주식회사 | 베인과 이를 포함하는 압축기 및 가스 터빈 |
| US20210381385A1 (en) * | 2020-06-03 | 2021-12-09 | Honeywell International Inc. | Characteristic distribution for rotor blade of booster rotor |
| CN112648235B (zh) * | 2021-01-19 | 2024-05-07 | 大连海事大学 | 一种带有鼓包和凹缝结构的跨声速压气机转子叶片 |
| CN113217458B (zh) * | 2021-05-28 | 2022-09-02 | 宁波方太厨具有限公司 | 一种叶轮、应用有该叶轮的风机系统和吸油烟机 |
Family Cites Families (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3012709A (en) * | 1955-05-18 | 1961-12-12 | Daimler Benz Ag | Blade for axial compressors |
| BE638547A (no) * | 1962-10-29 | 1900-01-01 | ||
| US3692425A (en) * | 1969-01-02 | 1972-09-19 | Gen Electric | Compressor for handling gases at velocities exceeding a sonic value |
| US3653110A (en) * | 1970-01-05 | 1972-04-04 | North American Rockwell | Method of fabricating hollow blades |
| US3706512A (en) * | 1970-11-16 | 1972-12-19 | United Aircraft Canada | Compressor blades |
| US4116584A (en) * | 1973-10-12 | 1978-09-26 | Gutehoffnungshutte Sterkrade Ag | Device for extending the working range of axial flow compressors |
| US4128363A (en) * | 1975-04-30 | 1978-12-05 | Kabushiki Kaisha Toyota Chuo Kenkyusho | Axial flow fan |
| US4108573A (en) * | 1977-01-26 | 1978-08-22 | Westinghouse Electric Corp. | Vibratory tuning of rotatable blades for elastic fluid machines |
| US4318672A (en) * | 1978-11-06 | 1982-03-09 | Nordisk Ventilator Co. A/S | Particle erosion resistant covering for fan blade leading edge |
| FR2626841B1 (fr) * | 1988-02-05 | 1995-07-28 | Onera (Off Nat Aerospatiale) | Profils pour pale d'helice aerienne carenee |
| FR2628062B1 (fr) * | 1988-03-07 | 1990-08-10 | Aerospatiale | Pale pour helice carenee a hautes performances, helice carenee multipale pourvue de telles pales et agencement de rotor de queue a helice carenee pour aeronef a voilure tournante |
| JPH03206400A (ja) * | 1990-01-08 | 1991-09-09 | Hitachi Ltd | ターボ機械の翼面上付着物除去装置 |
| US5181678A (en) * | 1991-02-04 | 1993-01-26 | Flex Foil Technology, Inc. | Flexible tailored elastic airfoil section |
| US5312696A (en) * | 1991-09-16 | 1994-05-17 | United Technologies Corporation | Method for reducing fretting wear between contacting surfaces |
| JPH08254156A (ja) | 1995-03-17 | 1996-10-01 | Senshin Zairyo Riyou Gas Jienereeta Kenkyusho:Kk | 軸流圧縮機の動翼 |
| US6129528A (en) * | 1998-07-20 | 2000-10-10 | Nmb Usa Inc. | Axial flow fan having a compact circuit board and impeller blade arrangement |
| DE19913269A1 (de) * | 1999-03-24 | 2000-09-28 | Asea Brown Boveri | Turbinenschaufel |
| DE19957718C1 (de) * | 1999-11-30 | 2001-06-13 | Mtu Muenchen Gmbh | Schaufel mit optimiertem Schwingungsverhalten |
| US6471482B2 (en) * | 2000-11-30 | 2002-10-29 | United Technologies Corporation | Frequency-mistuned light-weight turbomachinery blade rows for increased flutter stability |
| US6450770B1 (en) | 2001-06-28 | 2002-09-17 | General Electric Company | Second-stage turbine bucket airfoil |
| US6558122B1 (en) | 2001-11-14 | 2003-05-06 | General Electric Company | Second-stage turbine bucket airfoil |
| US6685434B1 (en) | 2002-09-17 | 2004-02-03 | General Electric Company | Second stage turbine bucket airfoil |
| US6779977B2 (en) | 2002-12-17 | 2004-08-24 | General Electric Company | Airfoil shape for a turbine bucket |
| US6832897B2 (en) | 2003-05-07 | 2004-12-21 | General Electric Company | Second stage turbine bucket airfoil |
| US6808368B1 (en) | 2003-06-13 | 2004-10-26 | General Electric Company | Airfoil shape for a turbine bucket |
| US6857853B1 (en) * | 2003-08-13 | 2005-02-22 | General Electric Company | Conical tip shroud fillet for a turbine bucket |
| US7112043B2 (en) * | 2003-08-29 | 2006-09-26 | General Motors Corporation | Compressor impeller thickness profile with localized thick spot |
| US6881038B1 (en) | 2003-10-09 | 2005-04-19 | General Electric Company | Airfoil shape for a turbine bucket |
| GB0325215D0 (en) * | 2003-10-29 | 2003-12-03 | Rolls Royce Plc | Design of vanes for exposure to vibratory loading |
| US7186090B2 (en) * | 2004-08-05 | 2007-03-06 | General Electric Company | Air foil shape for a compressor blade |
| US20060073022A1 (en) * | 2004-10-05 | 2006-04-06 | Gentile David P | Frequency tailored thickness blade for a turbomachine wheel |
-
2006
- 2006-02-27 IT IT000340A patent/ITMI20060340A1/it unknown
-
2007
- 2007-02-13 US US11/674,319 patent/US7766624B2/en active Active
- 2007-02-16 US US11/675,969 patent/US7785074B2/en active Active
- 2007-02-22 CA CA2579383A patent/CA2579383C/en not_active Expired - Fee Related
- 2007-02-26 NO NO20071071A patent/NO20071071L/no not_active Application Discontinuation
- 2007-02-26 KR KR1020070019167A patent/KR101433374B1/ko not_active Expired - Fee Related
- 2007-02-26 JP JP2007045135A patent/JP5314851B2/ja not_active Expired - Fee Related
- 2007-02-27 EP EP07103116A patent/EP1826414B1/en active Active
- 2007-02-27 CN CN200710084367.6A patent/CN101029648B/zh not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP1826414B1 (en) | 2012-04-11 |
| JP5314851B2 (ja) | 2013-10-16 |
| KR20070089081A (ko) | 2007-08-30 |
| CA2579383C (en) | 2016-05-03 |
| EP1826414A2 (en) | 2007-08-29 |
| CN101029648A (zh) | 2007-09-05 |
| US7785074B2 (en) | 2010-08-31 |
| ITMI20060340A1 (it) | 2007-08-28 |
| JP2007231944A (ja) | 2007-09-13 |
| CA2579383A1 (en) | 2007-08-27 |
| EP1826414A3 (en) | 2010-09-15 |
| US7766624B2 (en) | 2010-08-03 |
| US20070201983A1 (en) | 2007-08-30 |
| US20080044288A1 (en) | 2008-02-21 |
| KR101433374B1 (ko) | 2014-08-26 |
| CN101029648B (zh) | 2014-11-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| NO20071071L (no) | Rotorblad for et andre trinn i en kompressor. | |
| GB201113083D0 (en) | A method for in-situ cleaning of compressor blades in a gas turbine engine on aircraft and compositions | |
| EP2372102A3 (en) | Rotor blade platform of a gas turbine engine | |
| EP2551592A3 (en) | Microcircuit cooling for gas turbine engine combustor | |
| PL2099582T3 (pl) | Urządzenie i sposób naprawy lub wytwarzania końców łopatek turbiny gazowej, w szczególności silnika lotniczego | |
| WO2012134833A3 (en) | High camber compressor rotor blade | |
| EP2587028A3 (en) | Active clearance control system and method for a gas turbine engine | |
| DE502005003215D1 (de) | Verfahren zum betrieb eines verdichters einer gasturbine bei verdunstungskühlung der verdichteransaugluft | |
| WO2010149139A3 (de) | Deckbandsegment zur anordnung an einer schaufel | |
| DE502004011310D1 (de) | Vorrichtung zum Ausbauen von Schaufeln einer Turbine oder eines Verdichters | |
| EP2423436A3 (en) | Airfoil shape for compressor | |
| EP2535548A3 (en) | Turbine section of high bypass turbofan | |
| WO2013050569A3 (de) | Verfahren und vorrichtung zum montieren eines rotors einer windenergieanlage | |
| ATE468299T1 (de) | Zweiteiliger hauptausleger für einen gittermastkran und verfahren zum aufrichten davon | |
| DE602006014773D1 (de) | Buchse für die Drehschaft einer verstellbaren Statorschaufel einer Turbomaschine, und entsprechende Statorbeschaufelung, Verdichter, und Turbomaschine | |
| FR2983234B1 (fr) | Aube pour disque aubage monobloc de turbomachine | |
| NO20051740L (no) | Stator med hoy virkningsgrad for den andre fase i en gassturbin | |
| WO2012087420A3 (en) | Method for balancing rotating assembly of gas turbine engine | |
| WO2013102135A3 (en) | Gas turbine engine and turbine blade | |
| EP2706241A3 (en) | Fan blade | |
| DE602007007462D1 (de) | Gekoppelter resonator für ein regulierungssystem | |
| EP2955243A3 (en) | Methods of manufacturing a shroud abradable coating | |
| EP2402563A3 (en) | System and method for monitoring health of airfoils | |
| EP2412926A3 (en) | Hollow blade for a gas turbine | |
| ATE497094T1 (de) | Verfahren zum betreiben einer gasturbine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FC2A | Withdrawal, rejection or dismissal of laid open patent application |