FR1096708A - Perfectionnements apportés aux appareils à aubage supersonique, notamment aux compresseurs supersoniques - Google Patents
Perfectionnements apportés aux appareils à aubage supersonique, notamment aux compresseurs supersoniquesInfo
- Publication number
- FR1096708A FR1096708A FR1096708DA FR1096708A FR 1096708 A FR1096708 A FR 1096708A FR 1096708D A FR1096708D A FR 1096708DA FR 1096708 A FR1096708 A FR 1096708A
- Authority
- FR
- France
- Prior art keywords
- supersonic
- blading
- devices
- improvements made
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
-
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D21/00—Pump involving supersonic speed of pumped fluids
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1096708T | 1953-12-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1096708A true FR1096708A (fr) | 1955-06-23 |
Family
ID=9618308
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1096708D Expired FR1096708A (fr) | 1953-12-30 | 1953-12-30 | Perfectionnements apportés aux appareils à aubage supersonique, notamment aux compresseurs supersoniques |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1096708A (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3376018A (en) * | 1966-01-10 | 1968-04-02 | Rolls Royce | Vane operating mechanism |
US3484039A (en) * | 1967-07-14 | 1969-12-16 | Georg S Mittelstaedt | Fans and compressors |
US4012165A (en) * | 1975-12-08 | 1977-03-15 | United Technologies Corporation | Fan structure |
FR2698405A1 (fr) * | 1992-11-25 | 1994-05-27 | Snecma | Turbomachine à plusieurs étages d'aubes de stator à orientation variable. |
-
1953
- 1953-12-30 FR FR1096708D patent/FR1096708A/fr not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3376018A (en) * | 1966-01-10 | 1968-04-02 | Rolls Royce | Vane operating mechanism |
US3484039A (en) * | 1967-07-14 | 1969-12-16 | Georg S Mittelstaedt | Fans and compressors |
US4012165A (en) * | 1975-12-08 | 1977-03-15 | United Technologies Corporation | Fan structure |
FR2698405A1 (fr) * | 1992-11-25 | 1994-05-27 | Snecma | Turbomachine à plusieurs étages d'aubes de stator à orientation variable. |
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