GB448295A - Improvements in means for controlling internal-combustion engines of the liquid-fuel injection type - Google Patents
Improvements in means for controlling internal-combustion engines of the liquid-fuel injection typeInfo
- Publication number
- GB448295A GB448295A GB1217335A GB1217335A GB448295A GB 448295 A GB448295 A GB 448295A GB 1217335 A GB1217335 A GB 1217335A GB 1217335 A GB1217335 A GB 1217335A GB 448295 A GB448295 A GB 448295A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- control
- throttle
- fuel
- mixture
- 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
- F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2700/00—Mechanical control of speed or power of a single cylinder piston engine
- F02D2700/02—Controlling by changing the air or fuel supply
- F02D2700/0269—Controlling by changing the air or fuel supply for air compressing engines with compression ignition
- F02D2700/0271—Controlling the air supply as well as the fuel supply
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- High-Pressure Fuel Injection Pump Control (AREA)
Abstract
448,295. Fluid-pressure servomotorcontrol systems. DODSON, E., 66, Lewin Road, Streatham, London. April 23, 1935, No. 12173. [Class 135] [See also Group XXVII] In engines of the liquid-fuel injection type, means for controlling the amount of fuel injected by the pump are actuated by a device sensitive to induction-pipe pressure, and independently by means connected to the throttle control lever, further means being provided for operating the fuel control independently of both the throttle control and the pressure sensitive device. In Fig. 1, the fuel-control lever 6 is actuated by a servomotor piston 5, the valve 4 of which is controlled by a capsule 3 subjected to the delivery pressure of the air supercharger communicated by a pipe 1. The capsule 3 is further under the control of an altitude capsule 12, the position of which may be adjusted from the throttle control lever 31 by means of a link 9, cam 10, and lever 11. The throttle lever 31 is connected, in the manner described in Specification 419,472, to a mixture-control lever 8, so that when the former is in its idling position I or full-open position III, the latter is moved from its weak-mixture position A to its rich position B, and the lever 8 is connected to the link 9 by an arm 8x. The lever 8 adjusts the fuel to give the weak or rich mixture by a cam 7, lever 6<xx>, and sleeve valve 6<x> around the valve 4. For taking-off of aircraft, the lever 8 is moved to position C, in which linkage 17, 17<x> actuates a cam 18 and lever 17<xx> so as to adjust the boost control 19<x>, as described in Specification 419,113, to allow extra supercharging pressure, while still permitting the boost control to act through links 20, 21, 22 on the air throttle 23 in the induction pipe. In this position C of the lever 8, the cam 10 also comes into action to give an extra-rich mixture ; the lever 8 is also moved into this position when the throttle lever 31 is moved past a sealing-device into an emergency position IV. Further, in the position C, an anti-detonating agent, such as alcohol with or without water, is added to the mixture by the opening of a valve 26 admitting the second fuel from a supply tank through a pipe 28 connected to the eye of the supercharging-blower. The throttle lever 31 also actuates a cam 29 to vary the datum of the boost control in the manner described in the above-mentioned Specification 419,113 to prevent the usual supercharging pressure from being obtained with a weak mixture. The throttle and mixture control levers are further connected to an arm 40 controlling the ignition advance of the magneto 41<xx>. Also, when the throttle lever 31 is in position I or III, it raises the fuel-control lever 6 by means of cams 51, 52. The capsules 3 and 12 are each located in a container which limits the expansion in case of puncture, and comprises two cup-shaped parts 55, 56, Fig. 6, having interfitting tongues 58 and gaps 57, expansion of the container being resisted by a spring 61 bearing on flanges 59 formed at the ends of the tongues 58.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1217335A GB448295A (en) | 1935-04-23 | 1935-04-23 | Improvements in means for controlling internal-combustion engines of the liquid-fuel injection type |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1217335A GB448295A (en) | 1935-04-23 | 1935-04-23 | Improvements in means for controlling internal-combustion engines of the liquid-fuel injection type |
Publications (1)
Publication Number | Publication Date |
---|---|
GB448295A true GB448295A (en) | 1936-06-05 |
Family
ID=9999676
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1217335A Expired GB448295A (en) | 1935-04-23 | 1935-04-23 | Improvements in means for controlling internal-combustion engines of the liquid-fuel injection type |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB448295A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE744123C (en) * | 1937-10-09 | 1944-01-15 | Argus Motoren Ges M B H | Control device for internal combustion engines, especially aircraft engines |
DE886977C (en) * | 1939-10-07 | 1953-08-24 | Daimler Benz Ag | Automatic control device, which is dependent on the pressure in the inlet line, for the amount of fuel in internal combustion engines with large valve timing overlaps |
DE900634C (en) * | 1936-09-15 | 1953-12-28 | Daimler Benz Ag | Control device for supercharged internal combustion engines |
-
1935
- 1935-04-23 GB GB1217335A patent/GB448295A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE900634C (en) * | 1936-09-15 | 1953-12-28 | Daimler Benz Ag | Control device for supercharged internal combustion engines |
DE744123C (en) * | 1937-10-09 | 1944-01-15 | Argus Motoren Ges M B H | Control device for internal combustion engines, especially aircraft engines |
DE886977C (en) * | 1939-10-07 | 1953-08-24 | Daimler Benz Ag | Automatic control device, which is dependent on the pressure in the inlet line, for the amount of fuel in internal combustion engines with large valve timing overlaps |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2031527A (en) | Controlling means for fuel injection engines | |
GB577007A (en) | Improvements in or relating to fuel injection systems for internal combustion engines | |
US2379288A (en) | Internal-combustion engine | |
GB448295A (en) | Improvements in means for controlling internal-combustion engines of the liquid-fuel injection type | |
GB534124A (en) | Improvements in and relating to internal combustion engines of the injected fuel type | |
GB499741A (en) | Improvements in and connected with fuel feed control for internal combustion engines | |
US2877002A (en) | Fuel injection system | |
US1749721A (en) | Carburetor | |
GB272863A (en) | Improvements in or relating to means for regulating internal combustion engines for aircraft | |
GB346503A (en) | Improvements in means for regulating internal combustion engines for aircraft | |
GB454154A (en) | Improvements in or relating to supercharged internal-combustion engines for aircraft | |
GB476141A (en) | Improvements relating to regulating devices for internal combustion engines | |
GB450587A (en) | Improvements in or relating to supercharged internal-combustion engines for aircraft | |
GB499395A (en) | Improvements in or relating to boost controls for internal combustion engines | |
GB419113A (en) | Improvements in or connected with throttle controls for aircraft | |
GB532072A (en) | Improvements in or relating to fuel injection apparatus for internal combustion engines | |
GB395494A (en) | Improved means for controlling supercharged internal combustion engines for aircraft | |
GB191405150A (en) | Improvements in or relating to the Regulation of Injection Air for Internal Combustion Engines. | |
GB354926A (en) | Improvements in oil engines associated with vacuum-operated apparatus | |
GB507690A (en) | Improvements in or relating to two-stroke cycle internal combustion engines | |
GB537024A (en) | Improvements relating to internal combustion engines adapted to operate selectively with either oil or gaseous fuel | |
GB521411A (en) | Improvements in or relating to the fuel supply of internal combustion engines | |
GB412262A (en) | Improvements in throttle control for internal combustion engines | |
GB530000A (en) | Improvements in or relating to the control of internal combustion engines operating on the two-stroke cycle and with compression ignition | |
GB310012A (en) | Improvements in or relating to the regulation of fuel pumps for internal combustion engines |