CH617493A5 - - Google Patents
Download PDFInfo
- Publication number
- CH617493A5 CH617493A5 CH1381776A CH1381776A CH617493A5 CH 617493 A5 CH617493 A5 CH 617493A5 CH 1381776 A CH1381776 A CH 1381776A CH 1381776 A CH1381776 A CH 1381776A CH 617493 A5 CH617493 A5 CH 617493A5
- Authority
- CH
- Switzerland
- Prior art keywords
- blade
- section
- cross
- radius
- sections
- Prior art date
Links
- 230000006870 function Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000001154 acute effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL1975184450A PL111037B1 (en) | 1975-11-03 | 1975-11-03 | Working blade,especially long one,for steam and gas turbines and axial compressors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH617493A5 true CH617493A5 (cs) | 1980-05-30 |
Family
ID=19974108
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH1381776A CH617493A5 (cs) | 1975-11-03 | 1976-11-02 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US4284388A (cs) |
| CH (1) | CH617493A5 (cs) |
| DE (1) | DE2650433C3 (cs) |
| PL (1) | PL111037B1 (cs) |
Families Citing this family (33)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5783696A (en) * | 1980-11-14 | 1982-05-25 | Nippon Denso Co Ltd | Fan |
| US4585395A (en) * | 1983-12-12 | 1986-04-29 | General Electric Company | Gas turbine engine blade |
| US4682935A (en) * | 1983-12-12 | 1987-07-28 | General Electric Company | Bowed turbine blade |
| GB2164098B (en) * | 1984-09-07 | 1988-12-07 | Rolls Royce | Improvements in or relating to aerofoil section members for turbine engines |
| JP2590514B2 (ja) * | 1987-03-13 | 1997-03-12 | 日本電装株式会社 | 送風ファン |
| US4930990A (en) * | 1989-09-15 | 1990-06-05 | Siemens-Bendix Automotive Electronics Limited | Quiet clutch fan blade |
| US5480285A (en) * | 1993-08-23 | 1996-01-02 | Westinghouse Electric Corporation | Steam turbine blade |
| JP2002213206A (ja) * | 2001-01-12 | 2002-07-31 | Mitsubishi Heavy Ind Ltd | ガスタービンにおける翼構造 |
| JP3912989B2 (ja) * | 2001-01-25 | 2007-05-09 | 三菱重工業株式会社 | ガスタービン |
| WO2012098277A2 (es) * | 2012-03-30 | 2012-07-26 | Hurtado Baeza Juan Andres | Turbinas de simetría dinámica |
| US20140072433A1 (en) * | 2012-09-10 | 2014-03-13 | General Electric Company | Method of clocking a turbine by reshaping the turbine's downstream airfoils |
| US9435221B2 (en) | 2013-08-09 | 2016-09-06 | General Electric Company | Turbomachine airfoil positioning |
| US10570916B2 (en) | 2014-02-19 | 2020-02-25 | United Technologies Corporation | Gas turbine engine airfoil |
| US9347323B2 (en) | 2014-02-19 | 2016-05-24 | United Technologies Corporation | Gas turbine engine airfoil total chord relative to span |
| EP3108113A4 (en) | 2014-02-19 | 2017-03-15 | United Technologies Corporation | Gas turbine engine airfoil |
| US10393139B2 (en) | 2014-02-19 | 2019-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108103B1 (en) | 2014-02-19 | 2023-09-27 | Raytheon Technologies Corporation | Fan blade for a gas turbine engine |
| US10605259B2 (en) | 2014-02-19 | 2020-03-31 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015126450A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108110B1 (en) | 2014-02-19 | 2020-04-22 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108121B1 (en) | 2014-02-19 | 2023-09-06 | Raytheon Technologies Corporation | Turbofan engine with geared architecture and lpc airfoils |
| WO2015175073A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015175043A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015126454A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108101B1 (en) | 2014-02-19 | 2022-04-20 | 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 |
| WO2015175056A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108116B1 (en) * | 2014-02-19 | 2024-01-17 | RTX Corporation | Gas turbine engine |
| EP3114321B1 (en) | 2014-02-19 | 2019-04-17 | United Technologies Corporation | Gas turbine engine airfoil |
| US10557477B2 (en) | 2014-02-19 | 2020-02-11 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015126449A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015126715A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| US9163517B2 (en) | 2014-02-19 | 2015-10-20 | United Technologies Corporation | Gas turbine engine airfoil |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2660401A (en) * | 1951-08-07 | 1953-11-24 | Gen Electric | Turbine bucket |
| US3065933A (en) * | 1960-05-20 | 1962-11-27 | Frank Krause Jr A | Helicopter |
| US3169694A (en) * | 1963-04-08 | 1965-02-16 | Borchers Ariel George | Propeller fans and the like |
| DE2144600A1 (de) * | 1971-09-07 | 1973-03-15 | Maschf Augsburg Nuernberg Ag | Verwundene und verjuengte laufschaufel fuer axiale turbomaschinen |
| CH541065A (de) * | 1972-01-20 | 1973-08-31 | Bbc Brown Boveri & Cie | Verdrillte Laufschaufel einer axial durchströmten Turbomaschine |
| PL100097B1 (pl) * | 1973-09-07 | 1978-08-31 | Typ konstrukcyjny ekstremalnie dlugiej lopatki roboczej turbin parowych i innych maszyn cieplnych wirnikowych typu osiowego |
-
1975
- 1975-11-03 PL PL1975184450A patent/PL111037B1/pl unknown
-
1976
- 1976-11-02 CH CH1381776A patent/CH617493A5/de not_active IP Right Cessation
- 1976-11-03 DE DE2650433A patent/DE2650433C3/de not_active Expired
-
1979
- 1979-02-01 US US06/008,397 patent/US4284388A/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| DE2650433B2 (de) | 1980-07-03 |
| DE2650433A1 (de) | 1977-05-12 |
| PL111037B1 (en) | 1980-08-30 |
| DE2650433C3 (de) | 1981-04-09 |
| US4284388A (en) | 1981-08-18 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PL | Patent ceased | ||
| PL | Patent ceased |