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    • 1. 发明授权
    • Gas bearing piston assembly
    • 气体轴承活塞组件
    • US4455974A
    • 1984-06-26
    • US223314
    • 1981-01-08
    • Wilbur ShapiroSargit S. Bupara
    • Wilbur ShapiroSargit S. Bupara
    • F16C32/06F16J1/02F01L11/00
    • F16C32/0685F16J1/02
    • A gas bearing supported piston assembly (2) for an internal combustion engine including a piston body (14, 14') and a segmented piston ring (3) arranged to expand to compensate for wear. A piston supporting gas layer (27) is formed between the cylinder walls (8) and the exterior surface of each piston ring segment (32) by means of a plurality of restricted flow passages (40) formed in each segment (32) and extending between the inner and outer surfaces of the segment (32). In one embodiment, gas under pressure is supplied to the ring segments (32) through a single annular cavity (36) formed in piston body (14). In another embodiment, gas under pressure is supplied to the ring segments (32) through a plurality of corresponding holes (70) in piston body (14').
    • 一种用于内燃机的气体轴承支撑活塞组件(2),其包括活塞体(14,14')和分段式活塞环(3),所述分段式活塞环(3)被布置成膨胀以补偿磨损。 活塞支撑气体层(27)通过形成在每个段(32)中的多个限制流动通道(40)形成在气缸壁(8)和每个活塞环段(32)的外表面之间,并延伸 在所述段(32)的内表面和外表面之间。 在一个实施例中,压力下的气体通过形成在活塞体(14)中的单个环形空腔(36)供应到环形段(32)。 在另一个实施例中,在压力下的气体通过活塞体(14')中的多个对应的孔(70)供应到环形段(32)。
    • 3. 发明授权
    • Face seal with hydrodynamic thrust pads
    • 流体动力推力垫面密封
    • US5399024A
    • 1995-03-21
    • US180637
    • 1994-01-12
    • Wilbur Shapiro
    • Wilbur Shapiro
    • F16C17/06F16J15/34F16C32/06F16J15/38
    • F16J15/3432F16C17/06
    • A face seal with hydrodynamic thrust pads assembly is provided. The assembly comprises a ring structure with a front side facing in an axial direction that has a seal face continuous about the ring structure and a plurality of cut-outs with concave surfaces spaced concentrically around the seal face. A plurality of elastomeric laminates having a convex side are disposed in the concave surfaces. A plurality of thrust pads are bonded to the laminates such that one side of the thrust pads are all in a plane parallel to the plane of the seal face. When a closing load is transmitted against an opposing member by the sealing pressure against the back face of the assembly while the opposing member rotates relative to the assembly, friction and pressure forces cause the thrust pads to swing about a pivot point located towards the opposing member such that the fluid film converges in the direction of movement of the opposing member. Simultaneously, the seal face seals against the opposing member.
    • 提供了具有流体动力推力垫组件的面密封件。 组件包括环形结构,其具有面向轴向方向的前侧,该环形结构具有围绕环形结构连续的密封面以及具有与密封面同心地间隔开的凹面的多个切口。 具有凸面的多个弹性体层压体设置在凹面中。 多个推力垫结合到层压板,使得止推垫的一侧都处于与密封面的平面平行的平面中。 当相对构件相对于组件旋转时,通过对组件的背面的密封压力相对于相对构件传递关闭负载,摩擦和压力使得止推垫围绕位于相对构件的枢转点摆动 使得流体膜在相对构件的运动方向上会聚。 同时,密封面密封在相对的构件上。
    • 5. 发明授权
    • Single ring sector seal
    • 单环扇形密封
    • US5192083A
    • 1993-03-09
    • US821789
    • 1992-01-16
    • Henry F. Jones, Jr.Wilbur Shapiro
    • Henry F. Jones, Jr.Wilbur Shapiro
    • F16J15/44
    • F16J15/441Y10S277/928
    • A single ring sector seal (10) has multiple arcuate sectors (12a, 12b, 12c) arranged circumferentially around a rotating shaft and in floating engagement with a seal housing. Each sector (12) engages each adjacent sector (12) with a slot seal (40) and overlapping joint (38) therebetween to deter leakage. A protruding ridge (36) on each sector (12) engages a low pressure end cover (18) to form a secondary seal. Spring balance seals (28) provide a further seal between the high pressure chambers (20b, 20c) and the chamber (20a) which can be vented while the shaft is rotating and pressurized when the shaft is stationary. Each sector (12) is radially, axially and moment balanced.
    • 单环扇形密封件(10)具有围绕旋转轴周向布置并与密封壳体浮动接合的多个弓形扇形体(12a,12b,12c)。 每个扇区(12)在每个相邻的扇区(12)处与其间具有狭缝密封(40)和重叠接头(38)接合以阻止泄漏。 每个扇区(12)上的突出脊(36)接合低压端盖(18)以形成二次密封。 弹簧平衡密封件(28)在高压室(20b,20c)和腔室(20a)之间提供进一步的密封,当轴处于静止状态时,可以在轴旋转时加压。 每个扇区(12)在径向,轴向和力矩平衡。