| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 二冲程内燃发动机 | CN200980158439.4 | 2009-03-31 | CN102378859A | 2012-03-14 | 乔尔·贝尔纳克列夫; 米卡埃尔·伯格曼 |
| 一种二冲程曲轴箱扫气式二冲程内燃发动机，该发动机包括：汽缸(2)，其被构造成在其中往复运动地容纳活塞(6)，且限定燃烧室(8)，所述燃烧室包括用于点燃空气/燃料混合物的点火装置(5)以及用于排出废气的排气口(40)；曲轴箱(3)，包括曲柄轴(18)；间接燃料供应系统(4)，例如汽化器(12)或低压燃料喷射系统，用于向所述曲轴箱(3)提供燃料，从而扫气至所述燃烧室(8)；至少一根输送管(20，20’)，均从所述曲轴箱(3)延伸至至少一个相应的输送口(21、21’)，以连接至所述燃烧室(8)；附加空气填充装置(25、24、27、23、23’、22、22’、26、26’)，用于利用附加空气至少部分地填充所述输送管(20，20’)，附加空气填充装置从所述输送口(21，21’)至所述曲轴箱(3)；以及直接喷射装置(7)，用于将燃料直接喷射到所述燃烧室(8)。 | ||||||
| 2 | 二冲程内燃发动机 | CN200980158439.4 | 2009-03-31 | CN102378859B | 2014-12-03 | 乔尔·贝尔纳克列夫; 米卡埃尔·伯格曼 |
| 一种二冲程曲轴箱扫气式二冲程内燃发动机，该发动机包括：汽缸(2)，其被构造成在其中往复运动地容纳活塞(6)，且限定燃烧室(8)，所述燃烧室包括用于点燃空气/燃料混合物的点火装置(5)以及用于排出废气的排气口(40)；曲轴箱(3)，包括曲柄轴(18)；间接燃料供应系统(4)，例如汽化器(12)或低压燃料喷射系统，用于向所述曲轴箱(3)提供燃料，从而扫气至所述燃烧室(8)；至少一根输送管(20，20’)，均从所述曲轴箱(3)延伸至至少一个相应的输送口(21、21’)，以连接至所述燃烧室(8)；附加空气填充装置(25、24、27、23、23’、22、22’、26、26’)，用于利用附加空气至少部分地填充所述输送管(20，20’)，附加空气填充装置从所述输送口(21，21’)至所述曲轴箱(3)；以及直接喷射装置(7)，用于将燃料直接喷射到所述燃烧室(8)。 | ||||||
| 3 | 内燃机的燃料-空气混合体的形成方法及燃料供给装置 | CN96110348.5 | 1996-06-14 | CN1069381C | 2001-08-08 | E·-W·郎; K·约斯 |
| 本发明涉及一种用于内燃机的形成燃料-空气混合体的方法特别是在内燃机起动后在加热过程中形成燃料-空气混合体的方法，其中，供给内燃机的燃料被蒸发，并且所产生的蒸发燃料与由内燃机吸入的空气相混合，其特征在于，所说的燃料蒸发在相对较低的温度下进行。本发明还涉及一种执行上述方法的装置该装置包括一个总吸管，一个安装在与总吸管相连的空气吸管内的空气计量装置，多个吸嘴及一个燃料蒸发器。 | ||||||
| 4 | 内燃机的燃料--空气混合体的形成方法及燃料供给装置 | CN96110348.5 | 1996-06-14 | CN1138663A | 1996-12-25 | E·W·郎; K·约斯 |
| 本发明涉及一种用于内燃机的形成燃料——空气混合体的方法特别是在内燃机起动后在加热过程中形成燃料—空气混合体的方法，其中，供给内燃机的燃料被蒸发，并且所产生的蒸发燃料与由内燃机吸入的空气相混合，其特征在于，所说的燃料蒸发在相对较低的温度下进行。本发明还涉及一种执行上述方法的装置，该装置包括一个总吸管，一个安装在与总吸管相连的空气吸管内的空气计量装置，多个吸嘴及一个燃料蒸发器。 | ||||||
| 5 | Two-stroke internal combustion engine | US13260668 | 2009-03-31 | US08677954B2 | 2014-03-25 | Joel Berneklev; Mikael Bergman |
| A two stroke crank case scavenged two-stroke internal combustion engine, the engine including: —a cylinder (2) configured to reciprocatingly receive a piston (6) therein defining a combustion chamber (8), the combustion chamber comprising an ignition means (5) for igniting an air/fuel mixture and an exhaust port (40) for evacuating the exhaust fumes, —a crank case (3) including a crank shaft (18), —an indirect fuel supply system (4), such as a carburettor (12) or a low pressure fuel-injection system, for supplying fuel to the crank case (3) to be scavenged to the combustion chamber (8), —at least one transfer duct (20, 20′) each extending from the crank case (3) to at least one corresponding transfer port (21, 21′) for connecting to the combustion chamber (8), —additional air filling means (25, 24, 27, 23, 23′, 22, 22′,26, 26′) for at least partly filling the transfer duct/s (20, 20′) with additional air from the transfer port (21, 21′) towards the crank case (3), —and a direct injection means (7) for injecting fuel directly into the combustion chamber (8). | ||||||
| 6 | Fuel controlling apparartus for internal combustion engine | US09796482 | 2001-03-02 | US20010018900A1 | 2001-09-06 | Yoshimoto Matsuda; Yoji Fukami; Satoru Watabe |
| A fuel controlling apparatus of an internal combustion engine for controlling a quantity of a fuel that is supplied to the engine includes: a fuel injector that injects the fuel to the engine, the fuel injector being controlled on a basis of a throttle opening degree and an engine speed without measuring a quantity of an intake air that is taken through an intake system of the engine; and a carburetor that supplies the fuel to the engine using a negative pressure produced by the intake system of the engine. The fuel is supplied to the engine solely by the fuel injector while the engine speed is lower than a lower limit of a high engine speed range including an upper limit engine speed. The fuel is supplied to the engine by both the fuel injector and the carburetor so that the fuel of a necessary quantity is supplied to the engine by combining a quantity of the fuel supplied by the fuel injector and a quantity of the fuel supplied by the carburetor while the engine speed is in the high engine speed range. | ||||||
| 7 | Fuel supply system for internal combustion engine | US921769 | 1986-10-22 | US4694797A | 1987-09-22 | Kyugo Hamai |
| In a single point injection system of the kind having an electronically controlled fuel injector disposed upstream of a throttle valve, a throttle body is formed with a fuel storage chamber and an idle fuel pickup passage for supplying fuel in the fuel storage chamber into an auxiliary air passage in such a manner that a quantity of fuel supplied through the idle fuel pickup passage is proportional to the flow rate of air passing through the auxiliary air passage. | ||||||
| 8 | Fuel injection apparatus for internal combustion engines | US33868173 | 1973-03-05 | US3927653A | 1975-12-23 | PAGDIN BRIAN COLIN |
| A fuel injection apparatus in which metering of the fuel is determined by adjustable stops controlling the stroke of a shuttle piston, one of the stops being positionally adjustable by an eccentric frusto-conical cam mounted for translational movement along its axis in response to an absolute pressure sensing evacuated bellows and for rotation about said axis by a temperature sensing expansible capsule with both the bellows and the capsule mounted in an air inlet duct through which air flows to the manifold of the engine served by the apparatus under the control of a manually adjustable throttle valve.
|
||||||
| 9 | Installation for producing a starting mixture for injection-type internal combustion engines | US3494340D | 1967-07-11 | US3494340A | 1970-02-10 | WEBER ANDREAS; FRICKER LUDWIG |
| 10 | JPH0475387B2 - | JP6951884 | 1984-04-05 | JPH0475387B2 | 1992-11-30 | |
| 11 | JPS5922067B2 - | JP2503973 | 1973-03-02 | JPS5922067B2 | 1984-05-24 | BURAIAN KORIN PAGUDEIN |
| 12 | JPS49100419A - | JP2503973 | 1973-03-02 | JPS49100419A | 1974-09-24 | |
| 13 | Fuel/air supply system for a fuel injector and methods of operation | US686937 | 1996-07-26 | US5666927A | 1997-09-16 | Jeffrey B. Pace; Vernon R. Warner |
| The fuel and air supply system of the present invention provides fuel from a fuel pump at a first pressure upstream of a pressure reducer, fuel being provided directly to the fuel injector at a reduced pressure on the downstream side of the pressure reducer. A bypass line in communication with the fuel line upstream of the pressure reducer provides fuel to an air reservoir at the first pressure. The air reservoir lies in communication with a porous member(s) in the fuel injector in an air inlet to a fuel volume within the injector upstream of the pressure reducer. Upon flow of fuel into the air reservoir and closure of normally open fuel and air valves in the reservoir, air at the first pressure is supplied the porous member(s), creating a pressure differential across the member(s), causing air to flow through the porous member(s) to form air bubbles in the fuel volume for two-phase flow through the fuel injector orifice. The air flows for a predetermined time until the reservoir fills with fuel which precludes further air flow into the injector. Upon shutdown of the engine, the valves in the air reservoir open, draining the fuel from the air reservoir and enabling air at atmospheric pressure to enter the reservoir, returning the system for reuse upon engine startup. | ||||||
| 14 | Cylinder injection type two cycle engine | US558246 | 1990-07-24 | US5138984A | 1992-08-18 | Kazutoshi Takashima |
| A fuel supply system for a two cycle crankcase compression internal combustion engine embodying direct cylinder injection and carburetors for supplying a fuel air mixture to the crankcase chambers of the engine for high speed cooling. The direct fuel injectors supply the fuel at the low speed operation and a fixed amount of fuel at mid range and high speed, while the carburetor supplies only the mid range and high speed requirements of the engine in combination with the fuel injectors. Fuel is supplied first to the fuel bowls of the carburetors which have a vapor vent and then from the fuel bowls to the fuel injectors so as to avoid the necessity of a separate vapor separator for the fuel injectors. | ||||||
| 15 | Dual fuel system for internal combustion engine | US93122 | 1987-09-01 | USRE32938E | 1989-06-06 | David F. Haman; Dale M. Needham |
| Disclosed herein is an internal combustion engine comprising a crankcase, a cylinder extending from the crankcase and having an inlet port, a piston located in the cylinder, a transfer passage located between the crankcase and the cylinder inlet port, a fuel pump adapted to communicate with a source of fuel for normal operation, a carburetor having an air induction passage communicating with the crankcase and including a venturi, which carburetor also includes a float bowl communicating with the fuel pump and a high speed nozzle communicating between the float bowl and the venturi, a low speed fuel nozzle communicating with the transfer passage adjacent the inlet port, and a fuel line communicating between the float bowl and the low speed nozzle and including therein check valve means preventing flow from the transfer passage to the float bowl and permitting flow from the float bowl to the transfer passage, which fuel line also includes fuel flow metering means. | ||||||
| 16 | Auxiliary fuel supply system | US59791 | 1987-06-09 | US4777913A | 1988-10-18 | Richard E. Staerzl; Norman H. Radtke; Leonard S. Hummel |
| An auxiliary fuel supply system is provided for a two cycle internal combustion engine (302). A first fuel line (350) supplies fuel from the fuel pump (338) to a solenoid (352) which is continuously cyclable between ON and OFF states during running of the engine, includig high speed operation where detonation may occur. Fuel then flows through a second fuel line (354) to a restriction orifice metering housing (356), and then to a plurality of third branch fuel lines (358, 384, 386, 388, 390 and 392) for delivery to respective cylinders. The restriction orifices provide a pressure drop from the second fuel line to the plurality of third fuel lines, to provide lower fuel pressure in the third fuel lines, to reduce the chance of leakage at the intake manifold (326), and also to reduce fuel pressure fluctuations in the third fuel lines otherwise due to cycling of the solenoid. Metering housing structure is disclosed. The solenoid is controlled by a variable duty cycle oscillator (408), which in turn is controlled by a fuel enrichment signal (84) output by an electronic control which is responsive to engine knock and/or temperature. Control circuitry is disclosed. | ||||||
| 17 | Fuel injection system and method for internal combustion engine | US834875 | 1977-09-20 | US4157084A | 1979-06-05 | Marvin E. Wallis |
| An air and fuel mixing device incorporates a Venturi throat or other mixing means for feeding a highly combustible mixture of fuel and pressurized air to an electrical fuel injector valve or directly to the intake manifold in a system for starting an internal combustion engine. The system replaces the choke in a conventional electrical ignition type internal combustion engine. The fuel injector valve is controlled to inject a limited quantity of a highly combustible atomized air-fuel mixture into the engine intake manifold during engine startup. Startup is achieved with minimum fuel waste and produces a minimum of exhaust pollutants. A modified form of the invention is shown as employed in a fuel injection type internal combustion engine system wherein high pressure air-fuel mixture is fed to the fuel injectors solely through use of a conventional low pressure fuel pump and air supply. The injectors operate to discharge a highly volatile, combustible, air-fuel mixture under pressure, instead of raw fuel thus significantly increasing combustion efficiency during engine startup to minimize fuel waste and reduce deleterious exhaust emissions. Another modified form of the invention is shown wherein the system is employed to feed a mixture of fuel and pressurized air to the engine intake manifold in response to an acceleration command from the engine throttle control during normal engine operation. This eliminates the need for the notoriously troublesome carburetor accelerator pump now in conventional use. | ||||||
| 18 | Fuel injection apparatus for internal combustion engines | US33868073 | 1973-03-05 | US3839998A | 1974-10-08 | PAGDIN B |
| A fuel injection apparatus incorporating a carburettor means for starting wherein the carburettor means comprises a fuel jet element mounted in fuel delivery relation to a carburettor air inlet passageway communicating with a main air inlet duct through the fuel injection apparatus at a position downstream of manually controlled throttle valve means, and air and fuel cut-off valves are provided for cutting off the flow of air and fuel respectively through the carburettor air inlet passageway and the fuel jet element by operation of a plunger in a carburettor bore in the body of the apparatus under pressure of fuel from a high pressure fuel pump feeding fuel injectors when injecting pressure is attained.
|
||||||
| 19 | Internal combustion engine,fuel supply system and process | US3443552D | 1966-12-13 | US3443552A | 1969-05-13 | SEGGERN ERNEST A VON; SEGGERN HENRY E VON |
| 20 | Fuel control | US56215056 | 1956-01-30 | US3006327A | 1961-10-31 | HOLLEY JR GEORGE M; CLAIRE JR ALTON G DE; CAMERON DONALD J |
QQ群二维码
意见反馈
意见反馈