FR1086314A - Improvements to turbines to reduce the power absorbed by a rotor rotating in the opposite direction to its normal direction of rotation - Google Patents
Improvements to turbines to reduce the power absorbed by a rotor rotating in the opposite direction to its normal direction of rotationInfo
- Publication number
- FR1086314A FR1086314A FR1086314DA FR1086314A FR 1086314 A FR1086314 A FR 1086314A FR 1086314D A FR1086314D A FR 1086314DA FR 1086314 A FR1086314 A FR 1086314A
- Authority
- FR
- France
- Prior art keywords
- turbines
- rotation
- reduce
- rotor rotating
- power absorbed
- 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
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
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/02—Adaptations for driving vehicles, e.g. locomotives
- F01D15/04—Adaptations for driving vehicles, e.g. locomotives the vehicles being waterborne vessels
-
- 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
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
-
- 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
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1086314T | 1953-07-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1086314A true FR1086314A (en) | 1955-02-11 |
Family
ID=9612738
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1086314D Expired FR1086314A (en) | 1953-07-06 | 1953-07-06 | Improvements to turbines to reduce the power absorbed by a rotor rotating in the opposite direction to its normal direction of rotation |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1086314A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3283995A (en) * | 1965-04-28 | 1966-11-08 | United Aircraft Corp | Splitter vane construction for turbofan engine |
EP2716864A1 (en) * | 2012-10-02 | 2014-04-09 | General Electric Company | Turbine tip leakage reduction system |
-
1953
- 1953-07-06 FR FR1086314D patent/FR1086314A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3283995A (en) * | 1965-04-28 | 1966-11-08 | United Aircraft Corp | Splitter vane construction for turbofan engine |
EP2716864A1 (en) * | 2012-10-02 | 2014-04-09 | General Electric Company | Turbine tip leakage reduction system |
US9453417B2 (en) | 2012-10-02 | 2016-09-27 | General Electric Company | Turbine intrusion loss reduction system |
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