GB361246A - - Google Patents
Info
- Publication number
- GB361246A GB361246A GB9768/31A GB976831A GB361246A GB 361246 A GB361246 A GB 361246A GB 9768/31 A GB9768/31 A GB 9768/31A GB 976831 A GB976831 A GB 976831A GB 361246 A GB361246 A GB 361246A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- engines
- airscrews
- gangway
- shafts
- 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
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 239000000446 fuel 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 POWER PLANTS 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)
- Tires In General (AREA)
Abstract
361,246. Mounting aeroplane engines and propellers. GRULICH, K., 152, Kurf³rstendamm, Halensee, Berlin. March 31, 1931, No. 9768. Convention date, Oct. 27, 1930. [Class 4.] Aeroplanes with pusher airscrews f have engines b, with underhung cylinders or other means for obtaining the highest possible position of the driving shaft, mounted in the upper surface of the wing and connected by shafts e to the airscrews which are located as high above the trailing edge of the wing as possible. As shown the engines b are mounted in chambers b in front of a gangway c through the wing. Alternatively the engines may be mounted in chambers behind the gangway but in this case certain engines may be mounted as shown in order to prevent the machine from being tail heavy. Couplings g, h both radially and axially flexible are inserted at the ends of the shafts e and one of these is made releasable to enable the propeller to rotate freely should the engine stop. The projecting parts are covered with streamlined casings i which increase the speed of the airflow over the rear upper surface of the wing. Other compartments in the wing accommodate passengers, fuel, and freight.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE361246T | 1930-10-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB361246A true GB361246A (en) | 1931-11-19 |
Family
ID=31895432
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9768/31A Expired GB361246A (en) | 1930-10-27 | 1931-03-31 |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB361246A (en) |
-
1931
- 1931-03-31 GB GB9768/31A patent/GB361246A/en not_active Expired
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