FR1130131A - Improvement in the control of stator-reactor or annular wing aerodynes - Google Patents
Improvement in the control of stator-reactor or annular wing aerodynesInfo
- Publication number
- FR1130131A FR1130131A FR1130131DA FR1130131A FR 1130131 A FR1130131 A FR 1130131A FR 1130131D A FR1130131D A FR 1130131DA FR 1130131 A FR1130131 A FR 1130131A
- Authority
- FR
- France
- Prior art keywords
- stator
- reactor
- improvement
- control
- annular wing
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/16—Composite ram-jet/turbo-jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1130131T | 1955-07-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1130131A true FR1130131A (en) | 1957-01-31 |
Family
ID=9637256
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1130131D Expired FR1130131A (en) | 1955-07-12 | 1955-07-12 | Improvement in the control of stator-reactor or annular wing aerodynes |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1130131A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3000177A (en) * | 1956-07-11 | 1961-09-19 | Snecma | Multiple-flow jet-propulsion engines |
US3103102A (en) * | 1958-07-18 | 1963-09-10 | Bristol Siddeley Engines Ltd | Propulsion power plants for aircraft |
US3402894A (en) * | 1966-06-01 | 1968-09-24 | United Aircraft Corp | Base-thrust nozzles |
-
1955
- 1955-07-12 FR FR1130131D patent/FR1130131A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3000177A (en) * | 1956-07-11 | 1961-09-19 | Snecma | Multiple-flow jet-propulsion engines |
US3103102A (en) * | 1958-07-18 | 1963-09-10 | Bristol Siddeley Engines Ltd | Propulsion power plants for aircraft |
US3402894A (en) * | 1966-06-01 | 1968-09-24 | United Aircraft Corp | Base-thrust nozzles |
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