FR1536732A - Perfectionnements aux aéronefs combinés - Google Patents
Perfectionnements aux aéronefs combinésInfo
- Publication number
- FR1536732A FR1536732A FR120814A FR120814A FR1536732A FR 1536732 A FR1536732 A FR 1536732A FR 120814 A FR120814 A FR 120814A FR 120814 A FR120814 A FR 120814A FR 1536732 A FR1536732 A FR 1536732A
- Authority
- FR
- France
- Prior art keywords
- combined aircraft
- aircraft
- combined
- aircraft improvements
- 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
- B64C11/003—Variable-diameter propellers; Mechanisms therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
-
- 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
- B64C29/0033—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 tiltable relative to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR120814A FR1536732A (fr) | 1967-09-13 | 1967-09-13 | Perfectionnements aux aéronefs combinés |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR120814A FR1536732A (fr) | 1967-09-13 | 1967-09-13 | Perfectionnements aux aéronefs combinés |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1536732A true FR1536732A (fr) | 1968-08-16 |
Family
ID=8638221
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR120814A Expired FR1536732A (fr) | 1967-09-13 | 1967-09-13 | Perfectionnements aux aéronefs combinés |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1536732A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1993024365A1 (fr) * | 1992-06-01 | 1993-12-09 | United Technologies Corp. | Rotor a diametre variable a torsion decalee |
-
1967
- 1967-09-13 FR FR120814A patent/FR1536732A/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1993024365A1 (fr) * | 1992-06-01 | 1993-12-09 | United Technologies Corp. | Rotor a diametre variable a torsion decalee |
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