DE59200459D1 - Turbomaschinenschaufel für subsonische Verhältnisse. - Google Patents
Turbomaschinenschaufel für subsonische Verhältnisse.Info
- Publication number
- DE59200459D1 DE59200459D1 DE59200459T DE59200459T DE59200459D1 DE 59200459 D1 DE59200459 D1 DE 59200459D1 DE 59200459 T DE59200459 T DE 59200459T DE 59200459 T DE59200459 T DE 59200459T DE 59200459 D1 DE59200459 D1 DE 59200459D1
- Authority
- DE
- Germany
- Prior art keywords
- turbomachine blade
- subsonic conditions
- subsonic
- conditions
- turbomachine
- 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 - Fee Related
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
- F01D5/12—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
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/145—Means for influencing boundary layers or secondary circulations
-
- 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
- Y10S415/00—Rotary kinetic fluid motors or pumps
- Y10S415/914—Device to control boundary layer
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH192491 | 1991-06-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE59200459D1 true DE59200459D1 (de) | 1994-10-13 |
Family
ID=4221779
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE59200459T Expired - Fee Related DE59200459D1 (de) | 1991-06-28 | 1992-06-16 | Turbomaschinenschaufel für subsonische Verhältnisse. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5228833A (de) |
EP (1) | EP0520288B1 (de) |
JP (1) | JPH05187202A (de) |
DE (1) | DE59200459D1 (de) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998019048A1 (en) * | 1996-10-28 | 1998-05-07 | Siemens Westinghouse Power Corporation | Airfoil for a turbomachine |
DE19650656C1 (de) * | 1996-12-06 | 1998-06-10 | Mtu Muenchen Gmbh | Turbomaschine mit transsonischer Verdichterstufe |
JP4484396B2 (ja) | 2001-05-18 | 2010-06-16 | 株式会社日立製作所 | タービン動翼 |
US6682301B2 (en) | 2001-10-05 | 2004-01-27 | General Electric Company | Reduced shock transonic airfoil |
KR100713252B1 (ko) * | 2005-07-08 | 2007-05-02 | 부산대학교 산학협력단 | 축류 터빈용 로터 블레이드 |
US9790797B2 (en) | 2011-07-05 | 2017-10-17 | United Technologies Corporation | Subsonic swept fan blade |
US9957801B2 (en) | 2012-08-03 | 2018-05-01 | United Technologies Corporation | Airfoil design having localized suction side curvatures |
US10641113B2 (en) * | 2015-04-08 | 2020-05-05 | United Technologies Corporation | Airfoils |
JP6730245B2 (ja) * | 2017-11-17 | 2020-07-29 | 三菱日立パワーシステムズ株式会社 | タービンノズル及びこのタービンノズルを備える軸流タービン |
CN109356666B (zh) * | 2018-12-14 | 2021-05-25 | 中国航发沈阳发动机研究所 | 一种轴流式涡轮大小叶片组合叶栅的叶型设计方法 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE249844C (de) * | ||||
US1748892A (en) * | 1917-10-20 | 1930-02-25 | Allis Chalmers Mfg Co | Hydraulic process and apparatus |
GB490501A (en) * | 1937-03-04 | 1938-08-16 | Escher Wyss Maschf Ag | Improvements in or relating to the blading of steam or gas turbines |
US2935246A (en) * | 1949-06-02 | 1960-05-03 | Onera (Off Nat Aerospatiale) | Shock wave compressors, especially for use in connection with continuous flow engines for aircraft |
US2830753A (en) * | 1951-11-10 | 1958-04-15 | Edward A Stalker | Axial flow compressors with circular arc blades |
US2949224A (en) * | 1955-08-19 | 1960-08-16 | American Mach & Foundry | Supersonic centripetal compressor |
US3156407A (en) * | 1958-07-07 | 1964-11-10 | Commissariat Energie Atomique | Supersonic compressors |
US3333817A (en) * | 1965-04-01 | 1967-08-01 | Bbc Brown Boveri & Cie | Blading structure for axial flow turbo-machines |
DE3202855C1 (de) * | 1982-01-29 | 1983-03-31 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur Verminderung von Sekundaerstroemungsverlusten in einem beschaufelten Stroemungskanal |
-
1992
- 1992-06-16 EP EP92110107A patent/EP0520288B1/de not_active Expired - Lifetime
- 1992-06-16 DE DE59200459T patent/DE59200459D1/de not_active Expired - Fee Related
- 1992-06-23 US US07/902,738 patent/US5228833A/en not_active Expired - Fee Related
- 1992-06-26 JP JP4169421A patent/JPH05187202A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
US5228833A (en) | 1993-07-20 |
EP0520288B1 (de) | 1994-09-07 |
EP0520288A1 (de) | 1992-12-30 |
JPH05187202A (ja) | 1993-07-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |