GB485053A - Improvements in mechanical transmission systems for aircraft - Google Patents
Improvements in mechanical transmission systems for aircraftInfo
- Publication number
- GB485053A GB485053A GB14656/37A GB1465637A GB485053A GB 485053 A GB485053 A GB 485053A GB 14656/37 A GB14656/37 A GB 14656/37A GB 1465637 A GB1465637 A GB 1465637A GB 485053 A GB485053 A GB 485053A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cables
- driving
- aircraft
- driven shafts
- propellers
- 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
- 230000009347 mechanical transmission Effects 0.000 title 1
- 239000002184 metal Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWERÂ PLANTSÂ OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/04—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
485,053. Propelling aircraft. ALMONACID, V. A. May 26, 1937, No. 14656. Convention date, May 4. [Class 4] [Also in Groups XXIV and XXVI] Mechanism in which driving and driven shafts a<1>, a<2>, Fig. 1, have at least two opposed crank arms b<1>, c<1>, b<2>, c<2>, the corresponding crank-pins of which are connected by wires d, e, or other tension members, so that the crank arms always remain parallel, is applied to the driving of a number of aeroplane propellers. A central driving shaft a<1>, Fig. 3, is connected through cables d, e with driven shafts a<2>.. a<7> carrying propellers g<2>, g<7>, respectively, arranged in spaced and parallel relationship at the front of an aeroplane wing h. Guide cranks i may be provided to prevent vibration and deformation. The ends of the cables d, Fig. 4, are connected through eyes d<1>, d2 to a common metal piece j mounted by means of a ball or roller bearing k on the crankpin b<1>. Stretchers or other devices may be provided for adjusting the tension of the cables.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR485053X | 1937-05-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB485053A true GB485053A (en) | 1938-05-13 |
Family
ID=8903890
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB14656/37A Expired GB485053A (en) | 1937-05-04 | 1937-05-26 | Improvements in mechanical transmission systems for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB485053A (en) |
-
1937
- 1937-05-26 GB GB14656/37A patent/GB485053A/en not_active Expired
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