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    • 31. 发明授权
    • Fuel supply system for miniature engines
    • 小型发动机燃油供应系统
    • US5488933A
    • 1996-02-06
    • US195441
    • 1994-02-14
    • Roger N. C. Pham
    • Roger N. C. Pham
    • F02B9/06F02B75/34F02D33/00F02M37/00F02M23/00
    • F02D33/003F02B75/34F02B9/06F02M37/0029F02M37/007F02M37/0082F02M37/0023F02M37/046Y10S123/03
    • Exhaust pressure of an air-cooled miniature internal combustion engine is used for fuel metering and fuel delivery to the engine under higher pressure than previously obtainable from muffler back-pressure in the prior art even though the back-pressure in the exhaust system is kept to near zero for maximum engine power and cooling. This is accomplished by tapping on to the engine's exhaust stream right at and facing the exhaust port. As the engine unloads, the muffler's exhaust is further aspirated outward by a faster-moving cooling airstream hence a further reduction muffler's back-pressure causing a decrease in fuel pressurization thus a decrease in fuel flow to the engine in corresponding with a known decrease in fuel requirement at high speed as it unloads, and vice-versa. Special fuel tanks designs for this fuel system are disclosed, as well as additional means for further boosting fuel pressure.
    • 空气冷却的微型内燃机的排气压力用于燃料计量和燃料在比现有技术中从消声器背压获得的更高的压力下向发动机输送,尽管排气系统中的背压保持为 接近零,最大发动机功率和冷却​​。 这是通过在正对着排气口的位置点击发动机排气流来实现的。 当发动机卸载时,消声器的排气通过更快的冷却气流进一步向外吸入,因此进一步减少消声器的背压导致燃料加压的降低,从而相应于已知的燃料减少对发动机的燃料流的减少 要求在高速卸载时,反之亦然。 公开了用于该燃料系统的特殊燃料箱设计,以及用于进一步提高燃料压力的附加装置。
    • 34. 发明授权
    • Model airplane engine starter
    • 型号飞机发动机起动器
    • US4440122A
    • 1984-04-03
    • US349054
    • 1982-02-16
    • Roger D. Theobald
    • Roger D. Theobald
    • F02B9/06F02B75/34F02N5/02
    • F02N5/02F02B75/34F02B9/06
    • A model internal-combustion engine having a rotatable shaft driven by an engine, a propeller secured to said shaft, and a self-starting mechanism in the form of a cylindrical hub mounted coaxially on the shaft against the propeller and having at one end an axially extending drive element at its periphery by means of which it drives the propeller and ramp-defining walls adjacent a spring-engaging element at its other end, and a helically wound spring surrounding the shaft, anchored at one end to a stationary part of the engine, and having a free end bearing against the hub with a hook formed thereon to automatically engage the spring-engaging element of the cylindrical hub and energize the spring when the propeller and hub are rotated in a contra-normal direction and to otherwise ride on the ramps of the hub in non-engaging relation to its spring-engaging element.
    • 具有由发动机驱动的旋转轴,固定在所述轴上的螺旋桨的模型内燃机以及同轴地安装在轴上的圆柱形轮毂形式的自启动机构抵靠螺旋桨,并且其一端轴向 在其周边延伸驱动元件,通过该驱动元件在其另一端驱动螺旋桨和邻近弹簧接合元件的斜坡限定壁,以及围绕轴的螺旋缠绕的弹簧,其一端锚固到发动机的静止部分 并且具有抵靠轮毂的自由端部,其上形成有钩,以自动地接合圆柱形轮毂的弹簧接合元件并且当螺旋桨和轮毂沿反方向旋转并且以其它方式骑在 轮毂与其弹簧接合元件呈非啮合关系的斜面。
    • 36. 发明授权
    • Adjustable muffler for model aircraft type engines
    • 用于模型飞机型发动机的可调消声器
    • US4031979A
    • 1977-06-28
    • US571374
    • 1975-04-24
    • Roger W. Raleigh
    • Roger W. Raleigh
    • F01N1/06F01N1/08F02B9/06F02B75/02F02B75/34F01N1/00
    • F02B75/34F01N1/06F01N1/08F02B9/06F02B2075/025Y10S181/404
    • In a muffler for a two-cycle combustion engine of the type commonly used to power miniature aircraft, cars, boats and models, the exhaust gas is directed into an expansion chamber for expansion and cooling, thence through a series of spaced baffles in a baffle chamber, and thence through a nozzle to the atmosphere. The baffle plates may comprise one or more different types having different sonic wave reflective characteristics and different impedances to gas flow. The baffle plates are spaced apart by one or more of a number of spacers providing different axial spacing between the baffle plates. THe baffle plates and their spacings are chosen by the user so as to obtain the required degree of muffling with the least amount of back pressure on the engine, as back pressure reduces engine power. The user is supplied with a kit having the various different type baffles and spacers. The user selects from the kit the desired spacers and baffles in accordance with his own experiments or in accordance with experimental data supplied by the manufacture of the kit. The nozzle includes a threaded end for mating with the threaded interior of the baffle chamber so that by removing the nozzle the baffles and the spacers may be stacked in the baffle chamber in the desired configuration and the nozzle replaced for securely holding the baffles in the desired geometry.
    • 在用于为微型飞机,汽车,船只和型号供电的类型的两循环内燃机的消声器中,排气被引导到用于膨胀和冷却的膨胀室中,从而通过隔板中的一系列间隔开的挡板 室,然后通过喷嘴进入大气。 挡板可以包括具有不同声波反射特性和气流不同阻抗的一种或多种不同类型。 挡板由多个间隔件间隔开一个或多个,从而在挡板之间提供不同的轴向间隔。 使用者选择挡板及其间距,以便在发动机上以最小量的背压获得所需的消声程度,因为背压降低了发动机功率。 用户被提供有具有各种不同类型的挡板和间隔件的套件。 用户根据他自己的实验或根据由试剂盒的制造提供的实验数据,从试剂盒中选择所需的间隔物和挡板。 喷嘴包括用于与挡板室的螺纹内部配合的螺纹端,使得通过移除喷嘴,挡板和间隔件可以以期望的构造堆叠在挡板室中,并且更换喷嘴以将挡板牢固地保持在期望的 几何。
    • 38. 发明授权
    • Combustion device for heat motors
    • 燃烧电动机燃烧装置
    • US3892206A
    • 1975-07-01
    • US34315073
    • 1973-03-20
    • TOYODA CHUO KENKYUSHO KK
    • KOBAYASHI AKIRA
    • F02B53/00F01C1/344F01C11/00F02B1/04F02B9/06F02B53/10F02B53/12F02C7/264F02M69/00F23Q3/00F23R3/00F23R3/28
    • F02M69/00F01C11/004F02B1/04F02B9/06F02B53/10F02B53/12Y02T10/17
    • A combustion device for use with motors for igniting and burning fuel-air mixture in which a cylindrical member (28) is airtightly fitted into a hole formed through the cylinder wall of the combustion chamber in such a manner that a plug chamber (35) with a bottom of the cylindrical member may be disposed within the combustion chamber, and an air discharge port (49), the fuel emerging surface of a fuel diffusion member (55) fitted into a fuel supply passage and electric spark ignition means are positioned within the plug chamber, whereby in starting the motor the fuel-air mixture in the combustion chamber is ignited by the combustion flame of the fuel-air mixture in the plug chamber (35) ignited by the ignition means and after the motor has been started the fuel-air mixture is ignited by the naked flame burning at the fuel emerging surface of the fuel diffusion member made of porous and refractory material.
    • 一种用于点燃和燃烧燃料 - 空气混合物的电动机的燃烧装置,其中圆柱形构件(28)气密地装配到通过燃烧室的气缸壁形成的孔中,使得塞子室(35) )可以设置在燃烧室内,并且排出口(49),安装在燃料供给通道中的燃料扩散部件(55)的燃料出口表面和电火花点火装置 由此在起动电动机时,燃烧室中的燃料 - 空气混合物被由点火装置点燃的插塞室(35)中的燃料 - 空气混合物的燃烧火焰点燃,并且在电动机起动之后 燃料 - 空气混合物由在由多孔耐火材料制成的燃料扩散构件的燃料出口表面燃烧的明火点燃。