DE1069475B - - Google Patents
Info
- Publication number
- DE1069475B DE1069475B DENDAT1069475D DE1069475DA DE1069475B DE 1069475 B DE1069475 B DE 1069475B DE NDAT1069475 D DENDAT1069475 D DE NDAT1069475D DE 1069475D A DE1069475D A DE 1069475DA DE 1069475 B DE1069475 B DE 1069475B
- Authority
- DE
- Germany
- Prior art keywords
- umlauie
- tellhar
- schaufchi
- rilierl
- prchilloillc
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/40—Transmitting means with power amplification using fluid pressure
- B64C13/42—Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Description
Hilfskraftanlage für Flugzeuge mit Antrieb durch eine axial beaufschlagte
Stauluftturbine
Claims (1)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE1069475B true DE1069475B (en) | 1900-01-01 |
Family
ID=594582
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DENDAT1069475D Pending DE1069475B (en) |
Country Status (1)
| Country | Link |
|---|---|
| DE (1) | DE1069475B (en) |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE618257C (en) * | 1930-07-10 | 1935-09-04 | Pioneer Instr Company Inc | Bucket wheel with two circumferential, coaxially mounted blading rims, in which the blades of one rim are adjustable in relation to the other |
-
0
- DE DENDAT1069475D patent/DE1069475B/de active Pending
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE618257C (en) * | 1930-07-10 | 1935-09-04 | Pioneer Instr Company Inc | Bucket wheel with two circumferential, coaxially mounted blading rims, in which the blades of one rim are adjustable in relation to the other |
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