GB526460A - Improvements in or relating to the power plants of aircraft - Google Patents
Improvements in or relating to the power plants of aircraftInfo
- Publication number
- GB526460A GB526460A GB8494/39A GB849439A GB526460A GB 526460 A GB526460 A GB 526460A GB 8494/39 A GB8494/39 A GB 8494/39A GB 849439 A GB849439 A GB 849439A GB 526460 A GB526460 A GB 526460A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- relating
- power plants
- engines
- march
- 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
- B64D35/00—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
- B64D35/08—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
-
- 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
- B64D35/00—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
- B64D35/04—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
- B64D35/06—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors the propellers or rotors being counter-rotating
Abstract
526,460. Propelling aircraft. BUGATTI, E. March 16, 1939, No. 8494. Convention date March 19, 1938. [Class 4] An aircraft has two co-axial airs crews 4, 5, rotated in opposite directions each by its own engine 12, 13. The engines being arranged one behind the other in the fuselage and driving the propellers through intermediate shafting including at least one bend provided with a suitable coupling. As shown, the engines may be arranged behind the cockpit and the transmission shafts 14, 15 may pass on either side of the pilot's seat, e.g. beneath his elbows.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
LU526460X | 1938-03-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB526460A true GB526460A (en) | 1940-09-18 |
Family
ID=19732863
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8494/39A Expired GB526460A (en) | 1938-03-19 | 1939-03-16 | Improvements in or relating to the power plants of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB526460A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1993013983A1 (en) * | 1992-01-17 | 1993-07-22 | Wisting Sven | Engine arrangement |
-
1939
- 1939-03-16 GB GB8494/39A patent/GB526460A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1993013983A1 (en) * | 1992-01-17 | 1993-07-22 | Wisting Sven | Engine arrangement |
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