GB352428A - Improvements in the arrangement and grouping of multiple internal combustion engineson aircraft - Google Patents
Improvements in the arrangement and grouping of multiple internal combustion engineson aircraftInfo
- Publication number
- GB352428A GB352428A GB39862/29A GB3986229A GB352428A GB 352428 A GB352428 A GB 352428A GB 39862/29 A GB39862/29 A GB 39862/29A GB 3986229 A GB3986229 A GB 3986229A GB 352428 A GB352428 A GB 352428A
- Authority
- GB
- United Kingdom
- Prior art keywords
- propeller
- wing
- driven
- aircraft
- 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
- 238000002485 combustion reaction Methods 0.000 title 1
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 238000001816 cooling Methods 0.000 abstract 1
- 239000011800 void material 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/04—Aircraft characterised by the type or position of power plants of piston type
- B64D27/06—Aircraft characterised by the type or position of power plants of piston type within, or attached to, wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Details Of Gearings (AREA)
- Gear Transmission (AREA)
- Retarders (AREA)
Abstract
352,428. Aircraft propelling means. CATTANEO, G., 89, Via Monte Rosa, Milan, Italy. Dec. 31, 1929, No. 39862. Convention date, Jan. 2. Void [Published under Sect. 91 of the Acts]. [Class 4.] An aeroplane propeller is driven through helical or bevel gear d, e, f from one or two engines a, a<1> having their cylinders in line, V or W formation, and arranged transversely of the wing within the thickness of its leading edge. A third or a third and a fourth engine arranged with their axes vertically may drive the same propeller shaft. Where two, three or four engines are used an additional propeller at the trailing edge of the wing may have its shaft driven by a bevel wheel opposite to the wheel f and gearing with the pinions d, e. The propeller shafts may be driven at the same speed as the engine shafts or at a reduced speed. The cylinders may project beyond the wing contour or they may be enclosed by a cowling c provided with slits for the entrance and exit of cooling air.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT352428X | 1929-01-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB352428A true GB352428A (en) | 1931-07-07 |
Family
ID=11241180
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB39862/29A Expired GB352428A (en) | 1929-01-02 | 1929-12-31 | Improvements in the arrangement and grouping of multiple internal combustion engineson aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB352428A (en) |
-
1929
- 1929-12-31 GB GB39862/29A patent/GB352428A/en not_active Expired
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