GB435707A - Starting apparatus for road vehicle and aeroplane engines - Google Patents
Starting apparatus for road vehicle and aeroplane enginesInfo
- Publication number
- GB435707A GB435707A GB940234A GB940234A GB435707A GB 435707 A GB435707 A GB 435707A GB 940234 A GB940234 A GB 940234A GB 940234 A GB940234 A GB 940234A GB 435707 A GB435707 A GB 435707A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- switch
- atmosphere
- control device
- piston
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M1/00—Carburettors with means for facilitating engine's starting or its idling below operational temperatures
- F02M1/04—Carburettors with means for facilitating engine's starting or its idling below operational temperatures the means to facilitate starting or idling being auxiliary carburetting apparatus able to be put into, and out of, operation, e.g. having automatically-operated disc valves
- F02M1/046—Auxiliary carburetting apparatus controlled by piston valves
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
Abstract
435,707. Spray carburetters. JACOBY, H. E., 9, Hofstrasse, Wetzikon, and NUSSLI, H., 9, Bahnhofstrasse, Hinwil, both in Switzerland. March 26, 1934, No. 9402. [Class 7 (iii)] [See also Group XXXV] For starting up internal-combustion engines a control device 8, 9, 10 is provided which automatically brings in an auxiliary carburetter jet 14 when the engine is started. Closure of the engine switch 17 and starting motor switch 18 energizes the electromagnet 13 to attract the armature 12 and force the pistons 9 and 10 down against the spring 7 thus allowing pipes a and b to communicate and opening pipe c to the atmosphere. Turning off switch 18 de-energizes 13 unless the engine is cold when circuit is still completed through thermostat 19 until a satisfactory temperature is reached when switch 20 opens. When pipe c is open to atmosphere the vacuum in the float chamber 1 is reduced so as to allow free flow through the jets. To render the engine capable of work at maximum permissible load when cold, the control device may be provided with a third piston attached to the shaft 8 so that when 13 is energized this piston permits connection to atmosphere of a pipe line led from cylinder 11 to a second pipe line which on one side leads to a low pressure cylinder containing a piston linked to the throttle and on the other side leads to a regulator operatively connected to the accelerator pedal as described in Specification 435,471. When various fuels are used, the control device may effect the switching over from one fuel to another or the cutting off of an undesired fuel.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB940234A GB435707A (en) | 1934-03-26 | 1934-03-26 | Starting apparatus for road vehicle and aeroplane engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB940234A GB435707A (en) | 1934-03-26 | 1934-03-26 | Starting apparatus for road vehicle and aeroplane engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB435707A true GB435707A (en) | 1935-09-26 |
Family
ID=9871279
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB940234A Expired GB435707A (en) | 1934-03-26 | 1934-03-26 | Starting apparatus for road vehicle and aeroplane engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB435707A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2664872A (en) * | 1946-01-15 | 1954-01-05 | Carter Carburetor Corp | Fuel control system |
DE1077483B (en) * | 1955-12-22 | 1960-03-10 | S U Carburetter Co | Starting device for gasoline injection internal combustion engines |
DE1210249B (en) * | 1964-01-16 | 1966-02-03 | Bosch Gmbh Robert | Fuel injection system for mixture-compressing internal combustion engines |
-
1934
- 1934-03-26 GB GB940234A patent/GB435707A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2664872A (en) * | 1946-01-15 | 1954-01-05 | Carter Carburetor Corp | Fuel control system |
DE1077483B (en) * | 1955-12-22 | 1960-03-10 | S U Carburetter Co | Starting device for gasoline injection internal combustion engines |
DE1210249B (en) * | 1964-01-16 | 1966-02-03 | Bosch Gmbh Robert | Fuel injection system for mixture-compressing internal combustion engines |
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