FR2017885A1 - - Google Patents
Info
- Publication number
- FR2017885A1 FR2017885A1 FR6930565A FR6930565A FR2017885A1 FR 2017885 A1 FR2017885 A1 FR 2017885A1 FR 6930565 A FR6930565 A FR 6930565A FR 6930565 A FR6930565 A FR 6930565A FR 2017885 A1 FR2017885 A1 FR 2017885A1
- Authority
- FR
- France
- 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.)
- Withdrawn
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
-
- 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
- F01D5/148—Blades with variable camber, e.g. by ejection of fluid
-
- 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
- F01D7/00—Rotors with blades adjustable in operation; Control thereof
-
- 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
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
-
- 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
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/76—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
-
- 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
-
- 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
- Y10S416/05—Variable camber or chord length
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)
- Sealing Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB43367/68A GB1235545A (en) | 1968-09-12 | 1968-09-12 | Improvements in or relating to blades or vanes for fluid flow machines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2017885A1 true FR2017885A1 (de) | 1970-05-22 |
Family
ID=10428464
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR6930565A Withdrawn FR2017885A1 (de) | 1968-09-12 | 1969-09-09 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3614260A (de) |
DE (1) | DE1946086C3 (de) |
FR (1) | FR2017885A1 (de) |
GB (1) | GB1235545A (de) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3844677A (en) * | 1971-11-01 | 1974-10-29 | Gen Electric | Blunted leading edge fan blade for noise reduction |
US4571157A (en) * | 1981-10-02 | 1986-02-18 | Karl Eickmann | Propeller with an interior arrangement to variate the pitch |
US4619585A (en) * | 1983-07-28 | 1986-10-28 | Joe Storm | Wind turbine apparatus |
DE3540401A1 (de) * | 1985-11-14 | 1987-05-21 | Mtu Muenchen Gmbh | Leitschaufelkranz fuer turbomaschinen, insbesondere fuer gasturbinen |
DE3710321C1 (de) * | 1987-03-28 | 1988-06-01 | Mtu Muenchen Gmbh | Geblaeseschaufel,insbesondere fuer Prop-Fan-Triebwerke |
US4802823A (en) * | 1988-05-09 | 1989-02-07 | Avco Corporation | Stress relief support structures and assemblies |
US5207558A (en) * | 1991-10-30 | 1993-05-04 | The United States Of America As Represented By The Secretary Of The Air Force | Thermally actuated vane flow control |
NZ511661A (en) * | 2001-05-11 | 2003-09-26 | Graham Bond Grove | An improved aerofoil |
DE10256008B3 (de) * | 2002-11-30 | 2004-08-12 | Universität Kassel | Turbomaschine |
US6763899B1 (en) * | 2003-02-21 | 2004-07-20 | Schlumberger Technology Corporation | Deformable blades for downhole applications in a wellbore |
GB0519502D0 (en) | 2005-09-24 | 2005-11-02 | Rolls Royce Plc | Vane assembly |
GB0601220D0 (en) | 2006-01-21 | 2006-03-01 | Rolls Royce Plc | Aerofoils for gas turbine engines |
US8162603B2 (en) * | 2009-01-30 | 2012-04-24 | General Electric Company | Vane frame for a turbomachine and method of minimizing weight thereof |
US9650903B2 (en) * | 2009-08-28 | 2017-05-16 | United Technologies Corporation | Combustor turbine interface for a gas turbine engine |
US20110232291A1 (en) * | 2010-03-26 | 2011-09-29 | General Electric Company | System and method for an exhaust diffuser |
GB201108001D0 (en) | 2011-05-13 | 2011-06-29 | Rolls Royce Plc | A method of reducing asymmetric fluid flow effect in a passage |
US9789636B2 (en) | 2013-06-03 | 2017-10-17 | United Technologies Corporation | Rigid and rotatable vanes molded within variably shaped flexible airfoils |
US9267427B2 (en) * | 2013-06-11 | 2016-02-23 | Ford Global Technologies, Llc | Variable geometry turbine vane |
DE102014216266A1 (de) | 2014-07-23 | 2016-01-28 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Schaufel für ein Laufrad |
US10502086B2 (en) * | 2016-03-16 | 2019-12-10 | General Electric Company | System and method for actuating gas turbine engine components using integrated jamming devices |
EP3517773B1 (de) * | 2018-01-29 | 2020-08-12 | Siemens Gamesa Renewable Energy A/S | Hinterkantenanordnung |
US11465735B2 (en) | 2019-06-11 | 2022-10-11 | David Thomas BIRKENSTOCK | Aircraft wing with bellows assembly for optimizing a boundary layer control system |
US11971004B2 (en) * | 2021-10-21 | 2024-04-30 | Schlumberger Technology Corporation | Adjustable fins on a turbine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT100913B (de) * | 1924-09-25 | 1925-09-10 | Istvan Eder | Schaufel für Schleuderpumpen. |
US2616509A (en) * | 1946-11-29 | 1952-11-04 | Thomas Wilfred | Pneumatic airfoil |
DE961742C (de) * | 1952-05-25 | 1957-04-11 | Kloeckner Humboldt Deutz Ag | Einrichtung zur Verstellung der Beschaufelung von Stroemungsmaschinen |
US2967573A (en) * | 1954-10-14 | 1961-01-10 | Goodyear Aircraft Corp | Pneumatic airfoil |
US3042371A (en) * | 1958-09-04 | 1962-07-03 | United Aircraft Corp | Variable camber balding |
US3158338A (en) * | 1963-02-18 | 1964-11-24 | Walton W Cushman | Sustaining airfoils having variable configurations to vary lift characteristics |
-
1968
- 1968-09-12 GB GB43367/68A patent/GB1235545A/en not_active Expired
-
1969
- 1969-09-05 US US855668A patent/US3614260A/en not_active Expired - Lifetime
- 1969-09-09 FR FR6930565A patent/FR2017885A1/fr not_active Withdrawn
- 1969-09-11 DE DE1946086A patent/DE1946086C3/de not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE1946086A1 (de) | 1970-07-30 |
DE1946086B2 (de) | 1973-09-20 |
US3614260A (en) | 1971-10-19 |
DE1946086C3 (de) | 1974-04-25 |
GB1235545A (en) | 1971-06-16 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
TP | Transmission of property | ||
ST | Notification of lapse |