CH385033A - Avion - Google Patents
AvionInfo
- Publication number
- CH385033A CH385033A CH240963A CH240963A CH385033A CH 385033 A CH385033 A CH 385033A CH 240963 A CH240963 A CH 240963A CH 240963 A CH240963 A CH 240963A CH 385033 A CH385033 A CH 385033A
- Authority
- CH
- Switzerland
- Prior art keywords
- plane
- Prior art date
Links
Classifications
-
- 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)
- Toys (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH240963A CH385033A (fr) | 1963-02-25 | 1963-02-25 | Avion |
US347272A US3201071A (en) | 1963-02-25 | 1964-02-25 | Tilting engine aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH240963A CH385033A (fr) | 1963-02-25 | 1963-02-25 | Avion |
Publications (1)
Publication Number | Publication Date |
---|---|
CH385033A true CH385033A (fr) | 1965-02-26 |
Family
ID=4233113
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH240963A CH385033A (fr) | 1963-02-25 | 1963-02-25 | Avion |
Country Status (2)
Country | Link |
---|---|
US (1) | US3201071A (fr) |
CH (1) | CH385033A (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5765783A (en) * | 1994-03-04 | 1998-06-16 | The Boeing Company | Vertically launchable and recoverable winged aircraft |
FR2920408B1 (fr) * | 2007-08-30 | 2010-02-19 | Snecma | Pylone de suspension d'un moteur sous une aile d'avion |
US20090114771A1 (en) * | 2007-11-05 | 2009-05-07 | Qian Mu | Split Return Wing |
US8721383B2 (en) * | 2009-09-09 | 2014-05-13 | Aurora Flight Sciences Corporation | Modular miniature unmanned aircraft with vectored thrust control |
DE102013216787A1 (de) | 2013-08-23 | 2015-02-26 | Evonik Degussa Gmbh | Guanidingruppen aufweisende semi-organische Siliciumgruppen enthaltende Verbindungen |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1872845A (en) * | 1930-05-29 | 1932-08-23 | George C Sullivan | Aeroplane |
US3029043A (en) * | 1958-01-27 | 1962-04-10 | Robert D Lindeman | Free floating wing structure and control system for convertible aircraft |
-
1963
- 1963-02-25 CH CH240963A patent/CH385033A/fr unknown
-
1964
- 1964-02-25 US US347272A patent/US3201071A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US3201071A (en) | 1965-08-17 |
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