GB1147782A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB1147782A GB1147782A GB18490/66A GB1849066A GB1147782A GB 1147782 A GB1147782 A GB 1147782A GB 18490/66 A GB18490/66 A GB 18490/66A GB 1849066 A GB1849066 A GB 1849066A GB 1147782 A GB1147782 A GB 1147782A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- wing
- april
- longitudinal structure
- relating
- 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
- B64C39/00—Aircraft not otherwise provided for
- B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
- B64C39/005—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
Abstract
1,147,782. Rotary wing aircraft. P. ORAZI. 27 April, 1966 [27 April, 1965], No. 18490/66. Headings B7G and B7W. An aircraft, which may be a towed glider, comprises a primary longitudinal structure c, formed with a pylon b for a wing a which rotates about its own spanwise axis. When constructed as a towed glider the wing is mounted at the aft end of the longitudinal structure and a front undercarriage wheel e is steered by a forwardly projecting arm f to which a towcable h is attached.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT1055465 | 1965-04-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1147782A true GB1147782A (en) | 1969-04-10 |
Family
ID=11134218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18490/66A Expired GB1147782A (en) | 1965-04-27 | 1966-04-27 | Improvements in or relating to aircraft |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE1481625A1 (en) |
GB (1) | GB1147782A (en) |
-
1966
- 1966-04-26 DE DE19661481625 patent/DE1481625A1/en active Pending
- 1966-04-27 GB GB18490/66A patent/GB1147782A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE1481625A1 (en) | 1970-05-06 |
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