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    • 3. 发明申请
    • METHOD AND APPARATUS FOR ROTATING SLEEVE ENGINE HYDRODYNAMIC SEAL
    • 旋转发动机水动力密封的方法和装置
    • US20150361838A1
    • 2015-12-17
    • US14392018
    • 2013-04-04
    • Dimitrios DARDALIS
    • Dimitrios DARDALIS
    • F01L1/46F16J15/34
    • F01B15/007F01B15/06F01L1/46F16J15/3404F16J15/3412F16J15/342F16J15/3448F16J15/3452F16J15/38
    • An improved sealing system for a poppet valve rotating sleeve internal combustion engine with rotating liners. A hydrodynamic face seal assembly includes a spring pre-load assembly provides a uniform loading to a primary sealing ring. A secondary seal is provided between the primary sealing ring and the cylinder head. Hydrodynamic face seal features are provided either on the mating face of the primary sealing ring or on the annular face of the rotating liner. The hydrodynamic face seal features include an inner sealing zone, and an outer loading zone with a plurality of hydrodynamic lift pads, and dam features which create converging surfaces. A lubricant is provided to the annular face of the rotating liner, so that a lubricant layer can be maintained between the primary sealing ring mating face and the rotating liner.
    • 一种用于带旋转衬垫的提升阀旋转套筒内燃机的改进的密封系统。 流体动力面密封组件包括弹簧预加载组件,其向主密封环提供均匀的载荷。 在主密封环和气缸盖之间设置二次密封。 流体动力学表面密封特征提供在主密封环的配合面上或旋转衬垫的环形表面上。 流体动力面密封特征包括内密封区和具有多个流体动力提升垫的外加载区,以及形成会聚表面的坝特征。 润滑剂被提供到旋转衬套的环形表面,使得可以在主密封环配合面和旋转衬垫之间保持润滑剂层。
    • 8. 发明授权
    • Apparatus and method for rotating sleeve engine hydrodynamic seal
    • 旋转套筒发动机流体动力密封的装置和方法
    • US07004119B2
    • 2006-02-28
    • US10821672
    • 2004-04-09
    • Dimitrios Dardalis
    • Dimitrios Dardalis
    • F01L7/02
    • F16J10/00F01B15/007F01B15/06F01L7/04F01L7/16F01L2101/00F01M9/109F02F11/007F16J15/342
    • A hydrodynamic face seal 100 for sealing between the cylinder head 300 and rotating sleeve 200 of a rotating liner engine. The face of the face seal provides a sealing zone 130 for maintaining a lubricant layer of about 2 micrometers between the face seal and the sleeve; and a loading zone 132. The loading zone includes hydrodynamic lift features such as inclined pads 150 or recessed step pads 152. Oil is supplied to annular oil supply passage 142 between the sealing zone and the loading zone, and flows from the annular oil supply passage to radial passages 144 located between the step pads. A spring pre-load is provided to the seal. An outer secondary seal 190 is provided to contain the lubricant. One or more inner secondary seals is provided to contain lubricant and combustion gases. Spiral oil pumping grooves may be provided.
    • 用于密封汽缸盖300和旋转衬套发动机的旋转套筒200之间的流体动力面密封件100。 面密封件的表面提供密封区域130,用于在面密封件和套筒之间保持约2微米的润滑剂层; 和装载区132。 装载区域包括诸如倾斜垫片150或凹陷步进垫片152之类的流体动力学提升特征。 油被供应到密封区域和装载区域之间的环形供油通道142,并且从环形供油通道流到位于台阶垫之间的径向通道144。 向密封件提供弹簧预加载。 提供外部次级密封件190以容纳润滑剂。 提供一个或多个内部二级密封件以容纳润滑剂和燃烧气体。 可以提供螺旋抽油槽。
    • 9. 发明授权
    • Rotating sleeve engine
    • 旋转套筒发动机
    • US06289872B1
    • 2001-09-18
    • US09244603
    • 1999-02-04
    • Dimitrios Dardalis
    • Dimitrios Dardalis
    • F01L702
    • F01B15/007F16J9/20F16J10/04
    • An internal combustion engine is provided including at least one cylinder having a conventional valvetrain. The valvetrain consists of at least one camshaft, at least one intake poppet valve per cylinder activated by the camshaft and at least one exhaust valve per cylinder activated by the camshaft as well. Rotably disposed within the engine block is a rotatable cylinder liner which is supported from the block with at least two journal bearings. A piston is mounted in each liner for reciprocating movement therein. A connecting rod connects each piston to a crankshaft converting the reciprocating motion to crank rotation. The sleeve rotates with the objective of improving the lubrication conditions of the piston rings and piston. The reduction in friction coefficient between the piston rings and liner at certain portions of the cycle will result in significant frictional benefits. The motion of the liner will result in continuous fluid lubrication which results in severe reduction of piston ring and liner wear.
    • 提供内燃机,其包括至少一个具有常规阀门的气缸。 阀门系由至少一个凸轮轴组成,每个缸体由凸轮轴启动的至少一个进气提升阀以及由凸轮轴启动的至少一个排气阀。 可旋转地设置在发动机缸体内的是可旋转的气缸套,其从具有至少两个轴颈轴承的块支撑。 活塞安装在每个衬里中,用于往复运动。 连杆将每个活塞连接到曲轴,将往复运动转换为曲柄旋转。 套筒旋转,目的是改善活塞环和活塞的润滑条件。 在循环的某些部分,活塞环和衬套之间的摩擦系数的减小将导致显着的摩擦益处。 衬套的运动将导致连续的流体润滑,导致活塞环和衬套磨损严重减少。
    • 10. 发明授权
    • Apparatus and method for sealing internal combustion engines
    • 内燃机密封装置及方法
    • US06283070B1
    • 2001-09-04
    • US09360061
    • 1999-07-23
    • Carl Robert DeckardDimitrios Dardalis
    • Carl Robert DeckardDimitrios Dardalis
    • F02B5700
    • F02B75/34F01B3/0079F01B3/04F01B15/007F02B63/02F02B75/04F02B75/16F02B75/26F02B2075/025F02F3/28F05C2201/0448
    • An improved sealing means for internal combustion engines comprising a combination of a metal primary sealing ring positioned substantially within a groove on the piston, and a compliant secondary sealing ring positioned in the groove behind the primary compression ring so that the compressed combustion gases force the compliant secondary sealing ring to form a seal between the groove and the primary sealing ring. In the preferred embodiment, the gapped ring is non-planar in order to provide effective sealing in a ported fixed-piston, rotating and translating cylinder engine such as the Deckard engine. Alternate embodiments include gapless rings with only a primary compression ring, and gapless rings with a compliant secondary sealing ring. An alternate embodiment is a single piece metal-capped compliant secondary sealing ring.
    • 一种用于内燃机的改进的密封装置,包括基本上位于活塞上的凹槽内的金属主密封圈和位于主压缩环后面的凹槽中的柔性副密封圈的组合,使得压缩的燃烧气体迫使柔性 二次密封环,以在凹槽和主密封环之间形成密封。 在优选实施例中,间隙环是非平面的,以便在诸如Deckard发动机的移动的固定活塞,旋转和平移缸发动机中提供有效的密封。 替代实施例包括仅具有主压缩环的无间隙环,以及具有柔性辅助密封环的无间隙环。 一个替代实施例是单件金属盖的顺应性次级密封环。