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    • 51. 发明申请
    • CONTINUOUS DROP EMITTER WITH REDUCED STIMULATION CROSSTALK
    • 具有减少刺激性CROSSTALK的连续喷射发射器
    • WO2008045235A1
    • 2008-04-17
    • PCT/US2007/021136
    • 2007-10-02
    • EASTMAN KODAK COMPANYXU, JinquanBROST, RandolphYANG, QingLOPES, Fernando Luis de SouzaPOND, Stephen Fullerton
    • XU, JinquanBROST, RandolphYANG, QingLOPES, Fernando Luis de SouzaPOND, Stephen Fullerton
    • B41J2/03
    • B41J2/03B41J2002/022B41J2002/033B41J2202/13B41J2202/16
    • A continuous drop emitter comprising a liquid supply chamber containing a liquid held at a positive pressure; first and second nozzles in fluid communication with the liquid supply chamber nozzles emitting first and second continuous streams of a liquid; first and second stream break-up transducers adapted to independently synchronize the break up of the first and second continuous streams of the liquid into first and second streams of drops of predetermined volumes, respectively; and an acoustic damping material located adjacent to or within the liquid supply chamber for damping sound waves generated within the liquid chamber by the first and second stream break-up transducer. The continuous drop emitter may also configured with a Helmholtz resonant chamber tuned to a critical stimulation frequency having an acoustic damping material therein for absorbing acoustic stimulation energy. The Helmholtz resonant chamber may serve as a portion of the common liquid supply for the first and second jets in which case the acoustic damping material may be porous to allow the liquid to pass through. The acoustic damping materials may acoustically lossy materials that transmute energy into heat via molecular motions. The acoustic damping materials may be porous materials that absorb acoustic energy by forcing the liquid through small passages causing viscous flow energy losses. In addition the acoustic damping materials may include components that cause the disruption of acoustic waves by reflection from materials that are impedance mismatched to the liquid, either very dense materials or gas filled voids.
    • 一种连续液滴发射器,包括一个含有保持在正压力下的液体的液体供应室; 第一和第二喷嘴与液体供应室喷嘴流体连通,发射第一和第二连续的液体流; 第一和第二流分解换能器,其适于独立地将所述液体的所述第一和第二连续流的分解独立地同步到预定体积的第一和第二液滴流中; 以及声音阻尼材料,其位于液体供应室附近或内部,用于阻止由第一和第二流断裂传感器在液体室内产生的声波。 连续液滴发射器还可以配置有调谐到临界刺激频率的亥姆霍兹谐振腔,其中具有用于吸收声学刺激能量的声阻尼材料。 亥姆霍兹共振腔可以用作第一和第二射流的公共液体供应的一部分,在这种情况下,声阻尼材料可以是多孔的以允许液体通过。 声阻尼材料可以通过分子运动将能量转变成热量的声学损耗材料。 声阻尼材料可以是通过迫使液体通过小通道而引起粘性流动能量损失来吸收声能的多孔材料。 此外,声阻尼材料可以包括通过来自与液体阻抗不匹配的材料(非常致密的材料或气体填充的空隙)的反射导致声波破坏的组件。
    • 52. 发明申请
    • CONTINUOUS INK JET PRINTING WITH SATELLITE DROPLETS
    • 连续喷墨打印与卫星喷墨
    • WO2007149243A1
    • 2007-12-27
    • PCT/US2007/013592
    • 2007-06-08
    • EASTMAN KODAK COMPANYFAGERQUIST, Randy, LeeYANG, Qing
    • FAGERQUIST, Randy, LeeYANG, Qing
    • B41J2/03
    • B41J2/03B41J2002/022B41J2002/033
    • Satellite droplets (9,10,11) that have a lifetime selectable between an infinite lifetime and a finite lifetime are formed with a continuous fluid-jet system having a drop generator, a stimulation device (2), and a nozzle plate (3) with at least one nozzle opening. A force is applied to eject a fluid jet having a diameter D from the nozzle openings and an adjustable energy drive pulse is applied to the stimulation device in a manner to create a series of perturbations on the ejected fluid jet, such that the perturbations are separated by a distance lambda. The drive pulse is defined by a pulse shape, a pulse amplitude, and a pulse duty cycle. A first satellite formation state is established by adjusting the energy of the of drive pulse (12) while operating the continuous fluid-jet system in a state wherein the lambda/D values are greater than theta and correspond to the measured normalized Rayleigh growth rate within or beyond the first minimum. The drive pulse (13) is adjusted in a manner to bring about a second satellite formation state after at least 1 lambda of the first satellite formation state.
    • 具有在无限寿命和有限寿命之间具有寿命可选择的卫星液滴(9,10,11)由具有液滴发生器,刺激装置(2)和喷嘴板(3)的连续流体喷射系统形成, 具有至少一个喷嘴开口。 施加力以喷射具有来自喷嘴开口的直径D的流体射流,并且可调节的能量驱动脉冲以在喷出的流体射流上产生一系列扰动的方式施加到刺激装置,使得扰动被分离 距离λ。 驱动脉冲由脉冲形状,脉冲幅度和脉冲占空比定义。 第一卫星形成状态通过在λ/ D值大于θ并且对应于测量的归一化瑞利生长速率的状态下操作连续流体喷射系统的同时调节驱动脉冲(12)的能量来建立 或超出第一最小值。 驱动脉冲(13)以在第一卫星形成状态的至少1λ之后产生第二卫星形成状态的方式被调整。