FR823441A - Device for reducing noise in fans and rotary fluid compressors - Google Patents
Device for reducing noise in fans and rotary fluid compressorsInfo
- Publication number
- FR823441A FR823441A FR823441DA FR823441A FR 823441 A FR823441 A FR 823441A FR 823441D A FR823441D A FR 823441DA FR 823441 A FR823441 A FR 823441A
- Authority
- FR
- France
- Prior art keywords
- fans
- reducing noise
- rotary fluid
- fluid compressors
- compressors
- 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
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/028—Layout of fluid flow through the stages
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR823441T | 1936-10-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR823441A true FR823441A (en) | 1938-01-20 |
Family
ID=9281372
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR823441D Expired FR823441A (en) | 1936-10-02 | 1936-10-02 | Device for reducing noise in fans and rotary fluid compressors |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR823441A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2671634A (en) * | 1949-07-01 | 1954-03-09 | Rolls Royce | Adjustable stator blade and shroud ring arrangement for axial flow turbines and compressors |
US2795373A (en) * | 1950-03-03 | 1957-06-11 | Rolls Royce | Guide vane assemblies in annular fluid ducts |
US2846137A (en) * | 1955-06-03 | 1958-08-05 | Gen Electric | Construction for axial-flow turbomachinery |
US2962260A (en) * | 1954-12-13 | 1960-11-29 | United Aircraft Corp | Sweep back in blading |
US3536414A (en) * | 1968-03-06 | 1970-10-27 | Gen Electric | Vanes for turning fluid flow in an annular duct |
FR2365692A1 (en) * | 1976-09-24 | 1978-04-21 | Kronogard Sven | GAS TURBINE STATOR |
-
1936
- 1936-10-02 FR FR823441D patent/FR823441A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2671634A (en) * | 1949-07-01 | 1954-03-09 | Rolls Royce | Adjustable stator blade and shroud ring arrangement for axial flow turbines and compressors |
US2795373A (en) * | 1950-03-03 | 1957-06-11 | Rolls Royce | Guide vane assemblies in annular fluid ducts |
US2962260A (en) * | 1954-12-13 | 1960-11-29 | United Aircraft Corp | Sweep back in blading |
US2846137A (en) * | 1955-06-03 | 1958-08-05 | Gen Electric | Construction for axial-flow turbomachinery |
US3536414A (en) * | 1968-03-06 | 1970-10-27 | Gen Electric | Vanes for turning fluid flow in an annular duct |
FR2365692A1 (en) * | 1976-09-24 | 1978-04-21 | Kronogard Sven | GAS TURBINE STATOR |
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