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    • 81. 发明授权
    • Shock absorber
    • 减震器
    • US4437548A
    • 1984-03-20
    • US503650
    • 1983-06-16
    • Masahiro Ashiba
    • Masahiro Ashiba
    • B60R19/32F16F9/06F16F9/342F16F9/48F16F9/50
    • F16F9/486B60R19/32F16F9/342Y10T137/1632
    • A shock absorber is disclosed having an outer cylinder closed at one end thereof, a hollow inner cylinder closed at one end and opened at an another end thereof, the open end being inserted in the outer cylinder, a guide member for guiding the inner cylinder slidably in the outer cylinder, a member for generating a damping force, the damping force generating member being connected to the open end of the inner cylinder, and having an orifice for throttling flow of hydraulic fluid from a chamber in the outer cylinder to a chamber in the inner cylinder, the orifice being in a central portion of the inner cylinder, and a plate-like stop provided between the inner cylinder and the damping force generating member for retaining the damping force generating member against the damping force within a predetermined range, the stop having an aperture greater than the orifice.
    • 公开了一种减振器,其外端在其一端封闭,中空的内筒在一端封闭并在其另一端开口,开口端插入外筒中,导向件用于可滑动地引导内筒 在外筒中具有用于产生阻尼力的构件,所述阻尼力产生构件连接到所述内筒的开口端,并且具有用于将液压流体从所述外筒中的腔室流动到所述外筒中的腔的节流孔 所述内筒,所述孔位于所述内筒的中心部分,以及设置在所述内筒和所述阻尼力产生构件之间的板状挡块,用于将所述阻尼力产生构件抵抗所述阻尼力保持在预定范围内, 停止具有大于孔的孔径。
    • 82. 发明授权
    • Oleopneumatic suspension with variable throttle orifices, especially for
aircraft landing gear
    • 具有可变节流孔的空气悬架,特别适用于飞机起落架
    • US4405119A
    • 1983-09-20
    • US285790
    • 1981-07-22
    • Jean MascletAndre Turiot
    • Jean MascletAndre Turiot
    • B60G15/12B64C25/60F16F9/48F16F9/342
    • F16F9/346B60G15/12B64C25/60F16F9/486
    • An oleopneumatic suspension with variable throttle orifices, particularly for aircraft landing gear comprising a rod (1) enclosing a pneumatic spring (2) and being fixed with respect to a piston (4) sliding in a cylinder (3), two valves (6) and (7) with permanent throttle orifices, the valve (6), which is of greater cross-section, throttling in the compression phase and the valve (7), which is of lesser cross-section, throttling in the extension phase, the suspension comprising in addition a throttle device, the section of whose orifice varies in dependence on the position and the direction of displacement of the piston (4) in the cylinder (3) so that over a given distance around a predetermined equilibrium position the orifices ensuring throttling in the compression and extension phases are of cross-sections respectively greater than the corresponding orifices over the remainder of the distance covered by the piston (4) in the cylinder (3). While primarily for use in connection with landing gear or support bogies of aircraft, the suspension is also suitable for land vehicles or for testing.
    • 一种具有可变节流孔的油气悬架,特别是用于飞机起落架的油气悬架,包括围绕气动弹簧(2)并相对于在气缸(3)中滑动的活塞(4)固定的杆(1),两个阀(6) 和(7)具有永久性节流孔的情况下,具有较大横截面的阀(6)在压缩阶段节流,并且阀(7)的横截面较小,在延伸阶段节流, 悬架还包括节流装置,其孔口的部分根据活塞(4)在气缸(3)中的位置和位移方向而变化,使得在预定平衡位置周围的给定距离处,孔确保 在压缩和延伸阶段中的节流分别大于在气缸(3)中活塞(4)所覆盖的距离的剩余部分内的相应孔口的横截面积。 主要用于与起落架或飞机支架转向架相连接时,悬挂系统也适用于陆上车辆或进行测试。
    • 83. 发明授权
    • Hydraulic shock absorber for vehicles
    • 汽车液压减震器
    • US4226408A
    • 1980-10-07
    • US5970
    • 1979-01-24
    • Takao TomitaIsamu Morita
    • Takao TomitaIsamu Morita
    • B60G15/12B60G17/04F16F9/092F16F9/08F16F9/342
    • B60G17/0424B60G15/12F16F9/092
    • A hydraulic shock absorber including inner and outer tubes telescopically fitted together and an orifice variable in response to relative movement of the inner and outer tubes. A large diameter tubular holder is disposed coaxially around an upper portion of the outer tube to provide a space between the outer tube and the holder, the space being divided by a tubular partition membrane disposed coaxially in the space into a high-pressure gas chamber located outside of the membrane and a low-pressure gas chamber located inside of the membrane and communicating with an upper space within the outer tube. The shock absorber is of the hydraulically and pneumatically operated type, is simple in structure, and can be assembled with ease while maintaining a desired degree of performance. When the shock absorber is at the end of the extension stroke, there is a sufficient length of span between an outer tube sliding portion and an inner tube sliding portion between which the variable orifice is located so that even when the shock absorber is subjected to lateral bending forces, the orifice clearance is prevented from being varied or deformed, to ensure reliable and smooth operation of the shock absorber.
    • 一种液压减震器,包括可伸缩地装配在一起的内外管和响应于内管和外管的相对运动而变化的孔。 大直径管状保持器同轴地布置在外管的上部,以在外管和保持器之间提供空间,该空间被同轴地设置在空间中的管状分隔膜分隔成高压气体室 在膜外部和位于膜内部并与外管内的上部空间连通的低压气体室。 该减震器具有液压和气动操作的类型,结构简单,并且可以轻松组装,同时保持所需的性能。 当减震器处于延伸行程结束时,在外管滑动部分和可变孔口位于其之间的内管滑动部分之间具有足够的跨度,使得即使当减震器经受横向 弯曲力,防止孔隙间隙变化或变形,以确保减震器的可靠和平稳运行。
    • 85. 发明授权
    • Shock absorber with controlled fluid bypass means
    • 具有受控流体旁路装置的减震器
    • US3990687A
    • 1976-11-09
    • US655464
    • 1976-02-05
    • Charles R. Curnutt
    • Charles R. Curnutt
    • F16F9/342
    • F16F9/342
    • The shock absorber is of the type comprising a cylinder and piston containing hydraulic fluid and wherein the piston has fluid bypass holes so that fluid can pass from one side of the piston to the other within the cylinder. Tapered pins at one end of the cylinder are receivable in the fluid bypass holes when the piston approaches the one end. A cage assembly in the form of guide rods supports the pins and passes through guide bores in the piston so that the pins and piston rotate as a unit and the pins are always held in alignment with the fluid bypass holes.
    • 该减振器是包括一个包括液压油的气缸和活塞的类型,并且其中活塞具有流体旁通孔,使得流体可以在气缸内从活塞的一侧传递到另一侧。 当活塞接近一端时,缸体一端的锥形销可接收在流体旁通孔中。 导杆形式的笼式组件支撑销并穿过活塞中的引导孔,使得销和活塞作为一个单元旋转,并且销总是保持与流体旁路孔对准。
    • 86. 发明授权
    • Oleo-pneumatic shock absorber
    • OLEO-PNEUMATIC SHOCK ABSORBER
    • US3724832A
    • 1973-04-03
    • US3724832D
    • 1971-03-09
    • MENASCO MFG CO
    • CESKA F
    • F16F9/06F16F9/342
    • F16F9/06F16F9/342
    • A two-stage oleo-pneumatic shock absorber incorporating two pneumatic (air) pressure chambers, a high air pressure chamber and a low pressure (air) chamber, separated by a hydraulic fluid (oil) pressure chamber. The oil chamber contains an orifice and metering pin, which orifice and metering pin control the rate of collapse of the low pressure air chamber. It also contains a second orifice and metering pin which control the rate of collapse of the high pressure air chamber. Both metering pins are preprogrammed so as to interact with each other and effect a nearly constant load throughout the stroke of the shock absorber, even under transient loading conditions.
    • 一个两级液压气动减震器,包括两个气动(空气)压力室,一个高压力室和一个由液压油(油)压力室隔开的低压(空气)室。 油室包含一个孔口和计量销,该孔口和计量管脚控制低压空气室的坍塌率。 它还包含一个控制高压空气室坍塌率的第二孔和计量销。 两个计量销都是预编程的,以便在冲击吸收器的整个行程中彼此相互作用并实现几乎恒定的负载,即使在瞬态负载条件下。
    • 90. 发明申请
    • フロントフォーク
    • 前锋
    • WO2016170980A1
    • 2016-10-27
    • PCT/JP2016/061218
    • 2016-04-06
    • KYBモーターサイクルサスペンション株式会社
    • 富宇賀 健
    • F16F9/44B62K25/08F16F9/32F16F9/342F16F9/348
    • B62K25/08F16F9/32F16F9/342F16F9/348F16F9/44
    • ばねアジャスタを備えつつも複数のアジャスタの設置を可能とするフロントフォークの提供を目的とする。上記した目的を達成するため、本発明の課題解決手段におけるフロントフォーク(F)では、ばねアジャスタ(A)がキャップ(4)に対して軸方向視で中心(O)から偏心した位置に回転可能に装着されるとともにフォーク本体(1)内に突出する外周に螺子部(35)を有し、ばねアジャスタ(A)の螺子部(35)に螺着されて懸架ばね(S)の支持位置を変更するプレート(P)がケース部(筒部材)(14a)に対してばねアジャスタ(A)の取付中心を通るケース部(14a)の少なくとも二箇所で接するようになっている。よって、プレート(P)を回り止めしつつも小型にでき、第一アジャスタ(5)および第二アジャスタ(6)に干渉しないように配置できる。
    • 本发明的目的是提供一种具有弹簧调节器的前叉,可以安装多个调节器。 为了实现这一目的,在该前叉(F)中,弹簧调节器(A)可旋转地安装在从轴向方向朝向中心(O)朝向帽(4)偏移的位置, 所述弹簧调节器(A)在突出到所述叉主体(1)的外周上具有螺纹部(35)。 板(P)旋入到弹簧调节器(A)的螺纹部分(35)上以改变悬架弹簧(S)的支撑位置,并且板(P)接触壳体单元(14a) 在穿过弹簧调节器(A)的安装中心的壳体单元(14a)的至少两个位置处, 因此,能够在停止板(P)的旋转的同时使该前叉更紧凑,并且能够使第一调节器(5)和第二调节器(6)不会彼此干涉。