FR983334A - Airplane with blown annular wing and body wing - Google Patents
Airplane with blown annular wing and body wingInfo
- Publication number
- FR983334A FR983334A FR983334DA FR983334A FR 983334 A FR983334 A FR 983334A FR 983334D A FR983334D A FR 983334DA FR 983334 A FR983334 A FR 983334A
- Authority
- FR
- France
- Prior art keywords
- wing
- airplane
- blown annular
- blown
- annular
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR983334T | 1949-03-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR983334A true FR983334A (en) | 1951-06-21 |
Family
ID=9535965
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR983334D Expired FR983334A (en) | 1949-03-17 | 1949-03-17 | Airplane with blown annular wing and body wing |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR983334A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2991026A (en) * | 1956-06-28 | 1961-07-04 | Doak Aircraft Co Inc | Aircraft flight control system |
US3054579A (en) * | 1957-03-14 | 1962-09-18 | Woldemar A Bary | Aircraft with slow speed landing and take-off |
US9259984B2 (en) | 2008-07-28 | 2016-02-16 | Fleck Future Concepts Gmbh | Combined air, water and road vehicle |
-
1949
- 1949-03-17 FR FR983334D patent/FR983334A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2991026A (en) * | 1956-06-28 | 1961-07-04 | Doak Aircraft Co Inc | Aircraft flight control system |
US3054579A (en) * | 1957-03-14 | 1962-09-18 | Woldemar A Bary | Aircraft with slow speed landing and take-off |
US9259984B2 (en) | 2008-07-28 | 2016-02-16 | Fleck Future Concepts Gmbh | Combined air, water and road vehicle |
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