GB482596A - Improvements in or relating to control systems for supercharged aero and like engines - Google Patents
Improvements in or relating to control systems for supercharged aero and like enginesInfo
- Publication number
- GB482596A GB482596A GB26993/36A GB2699336A GB482596A GB 482596 A GB482596 A GB 482596A GB 26993/36 A GB26993/36 A GB 26993/36A GB 2699336 A GB2699336 A GB 2699336A GB 482596 A GB482596 A GB 482596A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- control
- engines
- aero
- supercharged
- 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
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D29/00—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
- F02D29/02—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto peculiar to engines driving vehicles; peculiar to engines driving variable pitch propellers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D19/00—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
- F02D19/12—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with non-fuel substances or with anti-knock agents, e.g. with anti-knock fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D23/00—Controlling engines characterised by their being supercharged
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
482,596. Regulating ; spray carburetters. AERO ENGINES, Ltd., and HALLIDAY, G. F. Oct. 5, 1936, No. 26993. [Classes 7 (iii) and 7 (vi)] In supercharged aircraft and like engines, the anti-detonating properties of the fuel are controlled in accordance with the supercharger pressure, or with indirect effects thereof, such as the temperature or composition of the exhaust or the cylinder temperature, and this control of the fuel is interconnected with the pitch control of the airscrew, and with means for varying the datum of the altitude boost control. Fig. 1 shows the invention applied to an engine 1 having a carburetter 6 and supercharger 5, the fuel being supplied by a pump 16 connected to reservoirs 22A and 23A containing the main fuel and the anti-detonating liquid or fuel respectively. The proportions of liquid supplied from these reservoirs to the pump are varied by a valve device 17, the rod 21 of which is connected mechanically or hydraulically as at 25, 26 to the airscrew control 4, and also to the lever 13 for varying the datum of the boost control 7, which adjusts the throttle control by means of the usual connection 8 to a toggle linkage 9.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB26993/36A GB482596A (en) | 1936-10-05 | 1936-10-05 | Improvements in or relating to control systems for supercharged aero and like engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB26993/36A GB482596A (en) | 1936-10-05 | 1936-10-05 | Improvements in or relating to control systems for supercharged aero and like engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB482596A true GB482596A (en) | 1938-04-01 |
Family
ID=10252440
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB26993/36A Expired GB482596A (en) | 1936-10-05 | 1936-10-05 | Improvements in or relating to control systems for supercharged aero and like engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB482596A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2451204A (en) * | 1943-08-17 | 1948-10-12 | Gen Motors Corp | Engine controller |
US2560262A (en) * | 1943-11-06 | 1951-07-10 | Wright Aeronautical Corp | Automatic antidetonation system |
EP0042163A2 (en) * | 1980-06-14 | 1981-12-23 | Robert Bosch Gmbh | Method of controlling fuel supply and ignition timing in combustion engines |
FR2754310A1 (en) * | 1996-10-04 | 1998-04-10 | Renault Sport | Motor-propeller unit with controller for light aircraft |
-
1936
- 1936-10-05 GB GB26993/36A patent/GB482596A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2451204A (en) * | 1943-08-17 | 1948-10-12 | Gen Motors Corp | Engine controller |
US2560262A (en) * | 1943-11-06 | 1951-07-10 | Wright Aeronautical Corp | Automatic antidetonation system |
EP0042163A2 (en) * | 1980-06-14 | 1981-12-23 | Robert Bosch Gmbh | Method of controlling fuel supply and ignition timing in combustion engines |
EP0042163A3 (en) * | 1980-06-14 | 1982-09-22 | Robert Bosch Gmbh | Control apparatus for the fuel-air mixing in combustion engines |
FR2754310A1 (en) * | 1996-10-04 | 1998-04-10 | Renault Sport | Motor-propeller unit with controller for light aircraft |
US6004098A (en) * | 1996-10-04 | 1999-12-21 | Renault Sport | Propulsion unit for an aircraft and its control procedure |
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