GB582116A - Improvements relating to liquid fuel injection means for internal combustion engines - Google Patents
Improvements relating to liquid fuel injection means for internal combustion enginesInfo
- Publication number
- GB582116A GB582116A GB1594044A GB1594044A GB582116A GB 582116 A GB582116 A GB 582116A GB 1594044 A GB1594044 A GB 1594044A GB 1594044 A GB1594044 A GB 1594044A GB 582116 A GB582116 A GB 582116A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- supplied
- chamber
- fuel injection
- internal combustion
- 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
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
- F02M69/04—Injectors peculiar thereto
- F02M69/047—Injectors peculiar thereto injectors with air chambers, e.g. communicating with atmosphere for aerating the nozzles
-
- 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
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
- F02M69/08—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by the fuel being carried by compressed air into main stream of combustion-air
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
582,116. Fuel nozzles. ROVER CO., Ltd., and WILKS, M. C. Aug. 21, 1944, No. 15940. [Class 7 (iii)] A chamber d is provided around the end of a fuel injection nozzle of the type through which measured quantities of fuel are supplied by a pump to the cylinder or induction pipe and this chamber has a constantly open discharge orifice or orifices e spaced from and in advance of the nozzle outlet b and is supplied with air or gas under pressure independent of the combustion air to prevent fuel being drawn out of the nozzle due to high suction at idling. The chamber may be supplied with exhaust gas or with air from a separate pump A non-return valve c is provided in the fuel passage.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1594044A GB582116A (en) | 1944-08-21 | 1944-08-21 | Improvements relating to liquid fuel injection means for internal combustion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1594044A GB582116A (en) | 1944-08-21 | 1944-08-21 | Improvements relating to liquid fuel injection means for internal combustion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB582116A true GB582116A (en) | 1946-11-05 |
Family
ID=10068285
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1594044A Expired GB582116A (en) | 1944-08-21 | 1944-08-21 | Improvements relating to liquid fuel injection means for internal combustion engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB582116A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3105352A (en) * | 1959-01-02 | 1963-10-01 | Thompson Ramo Wooldridge Inc | Thrust control for rocket engines |
GB2216182A (en) * | 1988-02-22 | 1989-10-04 | Outboard Marine Corp | Fuel injector with continuous air flow |
-
1944
- 1944-08-21 GB GB1594044A patent/GB582116A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3105352A (en) * | 1959-01-02 | 1963-10-01 | Thompson Ramo Wooldridge Inc | Thrust control for rocket engines |
GB2216182A (en) * | 1988-02-22 | 1989-10-04 | Outboard Marine Corp | Fuel injector with continuous air flow |
GB2216182B (en) * | 1988-02-22 | 1991-12-18 | Outboard Marine Corp | Fuel injector with continuous air flow |
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