GB431687A - Improvements in and relating to motor driven propeller units - Google Patents
Improvements in and relating to motor driven propeller unitsInfo
- Publication number
- GB431687A GB431687A GB689/34A GB68934A GB431687A GB 431687 A GB431687 A GB 431687A GB 689/34 A GB689/34 A GB 689/34A GB 68934 A GB68934 A GB 68934A GB 431687 A GB431687 A GB 431687A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shafts
- crank
- cylinders
- stroke
- wheels
- 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
- 238000001816 cooling Methods 0.000 abstract 2
- 239000000446 fuel Substances 0.000 abstract 2
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 239000000203 mixture 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B73/00—Combinations of two or more engines, not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
431,687. Two - stroke and four - stroke engines. SCOTT, B. D., Camp, Miserden, near Stroud, Gloucestershire. Jan. 8, 1934, No. 689. [Classes 7 (ii) and 7 (vi)] [See also Group XXXIII] An aircraft engine has one or more pairs of cylinders 41, 42, provided with a common combustion chamber 43, and pistons connected to drive parallel crankshafts 48, 49, in opposite directions. The crank - shafts are geared together by wheels 50, 51, Fig. 1, and to coaxial propeller shafts 16, 17, by wheels 50 ... 53. The exhaust 21, 22 from the engines act on turbines 24, 25 before passing to atmosphere, the centre of the turbines 26, 27 injecting air at 29, 30 to cool the cylinders or supply air for supercharging. The cooling fins 82, Fig. 2, of the cylinders are enclosed in a casing 28 and alternate fins are gapped to produce a labyrinth course for the cooling air which is discharged to atmosphere at the bottom of the fins. Each pair of cylinders 41, 42, are inclined and the axes of the crank-shafts 48, 49 are offset from the centre lines of the cylinders toward one another. The inlet and exhaust valves 56, 57 are operated by balanced cams 58, 59, driven at four to one ratio. The cam-shafts 60, 61 are connected by crank-pins 70, 71, Fig. 3, to a cross-frame 63 pivoted eccentrically at 67 to a gear 661 connected by idle wheels 65, 66 to pinions 481, 491 on the crank-shafts. The lower part of the cross-frame 63 is connected at 72, 73 to oil pumps. Auxiliary frames 74, 75 connected to the crank-shafts at 76, 77 drive, by means of connections 78 ... 81, a dynamo, revolution counter or other auxiliary gear. The engine may operate on the two stroke, four stroke as shown, or a modified four stroke cycle. The latter may be effected by providing an additional admission valve having different timing and open for a shorter period. This valve may supply air or mixture for supercharging, an additional fuel valve or an extra fuel jet being provided in the carburetter. Two or more exhaust valves may be used. The engine may operate by compression-ignition.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB689/34A GB431687A (en) | 1934-01-08 | 1934-01-08 | Improvements in and relating to motor driven propeller units |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB689/34A GB431687A (en) | 1934-01-08 | 1934-01-08 | Improvements in and relating to motor driven propeller units |
Publications (1)
Publication Number | Publication Date |
---|---|
GB431687A true GB431687A (en) | 1935-07-08 |
Family
ID=9708792
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB689/34A Expired GB431687A (en) | 1934-01-08 | 1934-01-08 | Improvements in and relating to motor driven propeller units |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB431687A (en) |
-
1934
- 1934-01-08 GB GB689/34A patent/GB431687A/en not_active Expired
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