GB302511A - Improvements in flying machines - Google Patents
Improvements in flying machinesInfo
- Publication number
- GB302511A GB302511A GB1714/28A GB171428A GB302511A GB 302511 A GB302511 A GB 302511A GB 1714/28 A GB1714/28 A GB 1714/28A GB 171428 A GB171428 A GB 171428A GB 302511 A GB302511 A GB 302511A
- Authority
- GB
- United Kingdom
- Prior art keywords
- secured
- structures
- casings
- planes
- engines
- 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
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
302,511. Marks, E. C. R., (Soc. L. Lombardi et Cie). Jan. 18, 1928. Aeroplanes; helicopters; steering; floats, arrangement of.-An aircraft has its supporting planes 11, propellers in casings 10 and engines formed as a unit adapted to pivot about a transverse axis on the machine so as to assume a horizontal, vertical, or any intermediate position. Preferably biplane supporting surfaces 11 are employed carried by two wheel-like structures 4 adapted to be rotated in supports 3 carried by V-shaped members 2 from the body 1. Two engines are secured to the outsides of the structures 4 for driving two screws in the non-rotary casings 10. In the case of a seaplane two sets of lateral floats 12, 121, for use respectively during gliding and vertical descents are secured to the planes 11. Two rudders 13 are mounted near the ends of the wings and an elevator 16 is provided on the body. A modification is described in which the unit is pivoted on a transverse shaft supported by brackets from the body.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1714/28A GB302511A (en) | 1928-01-18 | 1928-01-18 | Improvements in flying machines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1714/28A GB302511A (en) | 1928-01-18 | 1928-01-18 | Improvements in flying machines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB302511A true GB302511A (en) | 1928-12-20 |
Family
ID=9726735
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1714/28A Expired GB302511A (en) | 1928-01-18 | 1928-01-18 | Improvements in flying machines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB302511A (en) |
-
1928
- 1928-01-18 GB GB1714/28A patent/GB302511A/en not_active Expired
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