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    • 1. 发明申请
    • CONTINUOUS PRINTING SYSTEM INCLUDING COMMON CHARGE ELECTRODE
    • 连续打印系统,包括通用电极
    • WO2010016867A1
    • 2010-02-11
    • PCT/US2009/004312
    • 2009-07-24
    • EASTMAN KODAK COMPANYPIATT, Michael JosephFAGERQUIST, Randy Lee
    • PIATT, Michael JosephFAGERQUIST, Randy Lee
    • B41J2/115
    • B41J2/115B41J2/09
    • A continuous inkjet system includes a plurality of nozzles producing a respective liquid jet through each nozzle. A stimulation device (42) at each nozzle is responsive to different types of stimulation signals to produce a modulation in the respective liquid jet to selectively control droplet break off relative to phases of the cycle of a varying voltage source (51) that is connected to a charge electrode (44). The break off phase of a droplet relative to the voltage phase of the voltage source will determine whether the droplet is charged or not charged. Droplets that become charged may be deflected from their paths and a deflection mechanism including the charge electrode determines which droplets are allowed to reach a surface for say printing and which droplets are collected and not deposited upon the surface.
    • 连续喷墨系统包括通过每个喷嘴产生相应液体射流的多个喷嘴。 每个喷嘴处的刺激装置(42)响应于不同类型的刺激信号,以在相应的液体射流中产生调制,以选择性地控制相对于变化的电压源(51)的周期的相位的液滴分离,所述变化的电压源 充电电极(44)。 液滴相对于电压源的电压相位的断开相位将决定液滴是充电还是未充电。 变得带电的液滴可能从其路径偏转,并且包括充电电极的偏转机构确定允许哪些液滴到达用于所述印刷的表面,哪些液滴被收集并且不沉积在表面上。
    • 4. 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。