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    • 83. 发明授权
    • Two-cycle engine for counter-rotation especially for aviation applications
    • 双循环发动机,特别适用于航空应用
    • US06994071B2
    • 2006-02-07
    • US10884572
    • 2004-07-02
    • Paul A. Schwam
    • Paul A. Schwam
    • B64C11/00B64C27/00F02B53/00
    • B64D27/02B64D35/06F01C1/22F02B53/00F02B2053/005F04C2/10F04C11/006F04C29/0021F04C2240/603Y02T10/17
    • A counter-rotating 2 cycle piston engine with a combustion chamber and an output shaft rotatably mounted to rotate independently about the same propeller centerline of an aircraft. The Internal combustion power is transmitted to the output shaft by means of a conventional piston, rod, crankshaft configuration journaled to the combustion chamber or engine block in the traditional manner thereby producing concurrent rotation of the shaft and counter-rotation of the engine block. Interior surfaces of the combustion chamber and pistons are angled to control the oil flow inside the crankcase and eliminate unwanted ponding. The pistons are modified to transfer fluid accumulations to the combustion chamber. A throttle is located at the axis of rotation to function normally without the effects of centrifical force. Dual propellers mounted on the shaft and on the block improve thrust performance, balance the torques and moments of inertia of the two counter-rotating masses, All rotational output torque automatically balances itself between counter rotating propellers and is converted into propulsion. No rotational torque is allowed to be transmitted to the airframe through the counter-rotating engine mount.
    • 具有燃烧室的反向旋转2循环活塞发动机和可旋转地安装成可独立地围绕飞机的相同螺旋桨中心线旋转的输出轴。 通过传统的活塞,杆,曲轴配置将内燃动力传递到输出轴,传统的活塞杆,曲轴配置以传统的方式安装在燃烧室或发动机缸体上,从而产生轴的同时旋转和发动机缸体的反转。 燃烧室和活塞的内表面成角度,以控制曲轴箱内的油流并消除不必要的沉淀。 活塞被修改以将流体积聚物传递到燃烧室。 节气门位于旋转轴线上,正常工作,不受离心力的影响。 安装在轴和块上的双螺旋桨提高了推力性能,平衡了两个反向旋转质量块的转矩和转动惯量。所有旋转输出扭矩自身在反向旋转螺旋桨之间自动平衡,并被转换为推进。 不允许旋转扭矩通过反向旋转的发动机支架传递到机身。
    • 84. 发明申请
    • Two-cycle engine for counter-rotation especially for aviation applications
    • 双循环发动机,特别适用于航空应用
    • US20050098143A1
    • 2005-05-12
    • US10884572
    • 2004-07-02
    • Paul Schwam
    • Paul Schwam
    • B64D27/02B64D35/06F01C1/22F02B53/00F04C2/10F04C11/00F04C29/00F02B75/18
    • B64D27/02B64D35/06F01C1/22F02B53/00F02B2053/005F04C2/10F04C11/006F04C29/0021F04C2240/603Y02T10/17
    • A counter-rotating 2 cycle piston engine with a combustion chamber and an output shaft rotatably mounted to rotate independently about the same propeller centerline of an aircraft. the Internal combustion power is transmitted to the output shaft by means of a conventional piston, rod, crankshaft configuration journaled to the combustion chamber or engine block in the traditional manner thereby producing concurrent rotation of the shaft and counter-rotation of the engine block. Interior surfaces of the combustion chamber and pistons are angled to control the oil flow inside the crankcase and eliminate unwanted ponding. The pistons are modified to transfer fluid accumulations to the combustion chamber. A throttle is located at the axis of rotation to function normally without the effects of centrifical force. Dual propellers mounted on the shaft and on the block improve thrust performance, balance the torques and moments of inertia of the two counter-rotating masses, All rotational output torque automatically balances itself between counter rotating propellers and is converted into propulsion. No rotational torque is allowed to be transmitted to the airframe through the counter-rotating engine mount.
    • 具有燃烧室的反向旋转2循环活塞发动机和可旋转地安装成可独立地围绕飞机的相同螺旋桨中心线旋转的输出轴。 内燃动力通过常规的活塞杆,曲轴配置传递到输出轴,传统的方式是以传统方式轴颈安装在燃烧室或发动机缸体上,从而产生轴的同时旋转和发动机缸体的反转。 燃烧室和活塞的内表面成角度,以控制曲轴箱内的油流并消除不必要的沉淀。 活塞被修改以将流体积聚物传递到燃烧室。 节气门位于旋转轴线上,正常工作,不受离心力的影响。 安装在轴和块上的双螺旋桨提高了推力性能,平衡了两个反向旋转质量块的转矩和转动惯量。所有旋转输出扭矩自身在反向旋转螺旋桨之间自动平衡,并被转换为推进。 不允许旋转扭矩通过反向旋转的发动机支架传递到机身。
    • 87. 发明授权
    • Variable volume liquid pumping system
    • 可变体积液体泵送系统
    • US3975910A
    • 1976-08-24
    • US557871
    • 1975-03-12
    • Benjamin F. Harvey
    • Benjamin F. Harvey
    • F04B1/04F04B49/12F04B53/00F04C11/00F16H43/00
    • F04C11/006F04B1/0413F04B49/12F04B53/00F16H43/00
    • A rotary input shaft is provided having an axially shiftable cam mounted thereon including circumferentially spaced and axially tapering cam lobes. A pair of reciprocating piston oil pumps are provided and include piston actuating followers engaged with the cam and operable thereby to pump oil through the pumps. An oil turbine is also provided and oil lines extend to and from the turbine from the pumps whereby operation of the pumps will cause oil to be pumped through the turbine which includes a rotary output shaft. By axially shifting the cam on the rotary input shaft the volume of oil pumped by the pumps during each cycle of operation thereof is varied whereby the input of oil to the turbine is similarly varied. The hydraulic system connecting the pumps to the turbine includes oil reservoir means from which oil may be admitted into the working portion of the system and into which oil from the working portion of the system may be withdrawn. Further, structure is provided for expressing oil from the reservoir in response to shifting of the cam to increase the discharge from the pumps and to withdraw oil from the working portion of the hydraulic system into the reservoir in response to shifting of the cam to reduce the output of the pumps. In this manner, even though the amount of oil pumped into and out of the pumps during each cycle of operation thereof varies with the axial shifting of the cam, a closed hydraulic system may be maintained.
    • 旋转输入轴设置有安装在其上的可轴向移动的凸轮,其包括周向间隔开的和轴向渐缩的凸轮凸角。 提供了一对往复活塞式油泵,并且包括与凸轮啮合的活塞致动从动件,从而将油泵送通过泵。 还提供了一个油轮机,并且油管线从泵向泵和/或从涡轮机延伸,从而泵的运行将导致油被泵送通过包括旋转输出轴的涡轮机。 通过轴向移动旋转输入轴上的凸轮,在其每个操作循环期间由泵泵送的油的体积变化,由此输入到涡轮机的油类似地变化。 将泵连接到涡轮机的液压系统包括储油装置,油可从该储油装置进入系统的工作部分,并且可从该系统的工作部分抽出油。 此外,提供了用于响应于凸轮的移动而响应于凸轮的移动来增加来自泵的排出并且将油从液压系统的工作部分引入油箱的结构,用于响应于凸轮的移动而将油从储存器表达以减少 输出泵。 以这种方式,即使在每个循环操作期间泵入和泵出的油的量随着凸轮的轴向移动而变化,可以保持闭合的液压系统。
    • 88. 发明授权
    • Variable speed hydraulic transmission
    • 变速液压传动
    • US3892072A
    • 1975-07-01
    • US35893773
    • 1973-05-10
    • HARVEY BENJAMIN F
    • HARVEY BENJAMIN F
    • F04B1/04F04B49/12F04B53/00F04C11/00F16H43/00F16H39/46
    • F04B53/00F04B1/0413F04B49/12F04C11/006F16H43/00
    • A rotary input shaft is provided having an axially shiftable cam mounted thereon including circumferentially spaced and axially tapering cam lobes. A pair of reciprocating piston oil pumps are provided and include piston actuating followers engaged with the cam and operable thereby to pump oil through the pumps. An oil turbine is also provided and oil lines extend to and from the turbine from the pumps whereby operation of the pumps will cause oil to be pumped through the turbine which includes a rotary output shaft. By axially shifting the cam on the rotary input shaft the volume of oil pumped by the pumps during each cycle of operation thereof is varied whereby the input of oil to the turbine is similarly varied. The hydraulic system connecting the pumps to the turbine includes oil reservoir means from which oil may be admitted into the working portion of the system and into which oil from the working portion of the system may be withdrawn. Further, structure is provided for expressing oil from the reservoir in response to shifting of the cam to increase the discharge from the pumps and to withdraw oil from the working portion of the hydraulic system into the reservoir in response to shifting of the cam to reduce the output of the pumps. In this manner, even though the amount of oil pumped into and out of the pumps during each cycle of operation thereof varies with the axial shifting of the cam, a closed hydraulic system may be maintained.
    • 旋转输入轴设置有安装在其上的可轴向移动的凸轮,其包括周向间隔开的和轴向渐缩的凸轮凸角。 提供了一对往复活塞式油泵,并且包括与凸轮啮合的活塞致动从动件,从而将油泵送通过泵。 还提供了一个油轮机,并且油管线从泵向泵和/或从涡轮机延伸,从而泵的运行将导致油被泵送通过包括旋转输出轴的涡轮机。 通过轴向移动旋转输入轴上的凸轮,在其每个操作循环期间由泵泵送的油的体积变化,由此输入到涡轮机的油类似地变化。 将泵连接到涡轮机的液压系统包括储油装置,油可从该储油装置进入系统的工作部分,并且可从该系统的工作部分抽出油。 此外,提供了用于响应于凸轮的移动而响应于凸轮的移动来增加来自泵的排出并且将油从液压系统的工作部分引入油箱的结构,用于响应于凸轮的移动而将油从储存器表达以减少 输出泵。 以这种方式,即使在每个循环操作期间泵入和泵出的油的量随着凸轮的轴向移动而变化,可以保持闭合的液压系统。