GB146375A - Improvements in and connected with the construction and propulsion of aeroplanes - Google Patents
Improvements in and connected with the construction and propulsion of aeroplanesInfo
- Publication number
- GB146375A GB146375A GB18349/20A GB1834920A GB146375A GB 146375 A GB146375 A GB 146375A GB 18349/20 A GB18349/20 A GB 18349/20A GB 1834920 A GB1834920 A GB 1834920A GB 146375 A GB146375 A GB 146375A
- Authority
- GB
- United Kingdom
- Prior art keywords
- screws
- central fuselage
- guns
- fitted
- pusher
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/04—Aircraft characterised by the type or position of power plant of piston type
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automatic Assembly (AREA)
Abstract
146,375. Daimler-Motoren-Ges. Oct. 11, 1915, [Convention date]. Aeroplanes; cars, propelling; guns, disposition of.-An aeroplane is constructed with a central fuselage 12 connecting the supporting-planes 18 to the tail planes 19 and carrying one or more tractor screws 15, and with one or more shorter bodies 13, 14 arranged on each side of the central fuselage and fitted with pusher screws. Guns 20, 21 may be mounted at the front of the two short bodies approximately in the plane of the tractor screw on the central fuselage, and a, third gun 22 may be mounted on the central fuselage in the plane of the two pusher screws on the short bodies. The screws may be driven by separate engines in each body, or all the engines may be in the central fuselage. The Specification as open to inspection under Sect. 91 (3) (a) describes also an aeroplane having two long fuselages 2, 3, Fig. 1 (Cancelled), fitted with t-ractor screws 5, 6 and a central body 1 fitted with a pusher screw 4. Guns are mounted at 9, 10 and 11. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE146375X | 1915-10-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB146375A true GB146375A (en) | 1921-06-09 |
Family
ID=5671333
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18349/20A Expired GB146375A (en) | 1915-10-11 | 1920-07-02 | Improvements in and connected with the construction and propulsion of aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB146375A (en) |
-
1920
- 1920-07-02 GB GB18349/20A patent/GB146375A/en not_active Expired
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