High speed rotating atomizer assembly
    11.
    发明申请
    High speed rotating atomizer assembly 有权
    高速旋转雾化器总成

    公开(公告)号:US20060208102A1

    公开(公告)日:2006-09-21

    申请号:US11250303

    申请日:2005-10-14

    IPC分类号: B05B3/10 B05B3/00

    摘要: An atomizer assembly (10) drives an atomizing bell (108) to apply paint onto a part (14). The atomizer assembly (10) includes a core (24) having at least one paint line (26) extending therethrough, a turbine device (40) circumscribing an axis (A) and disposed in the core (24), and a turbine unit (62) surrounding the pain line (26) and having a shaft (104) rotatable relative the turbine device (40) with several turbine blades (130) connected to the shaft (104). A plurality of nozzles (64, 66, 68) are defined in the turbine device (40) and are positioned relative a turbine wheel (106) connected to the shaft (104) to drive fluid, i.e. gas onto the turbine blades (130). An annular wall (94) extends outwardly from one of the terminal ends of the turbine device (40) to define a seat (96) for engaging the core (24) to maintain a fixed gap between the paint line (26) and the shaft (104) and to eliminate contact therebetween.

    摘要翻译: 雾化器组件(10)驱动雾化钟(108)以将油漆施加到部件(14)上。 雾化器组件(10)包括具有延伸穿过其中的至少一个涂漆线(26)的芯(24),围绕轴线(A)并设置在芯部(24)中的涡轮机装置(40) 围绕疼痛线(26)并且具有可相对于涡轮机装置(40)旋转的轴(104),其中多个涡轮机叶片(130)连接到轴(104)。 多个喷嘴(64,66,68)限定在涡轮机装置(40)中,并且相对于连接到轴(104)的涡轮机叶轮(106)定位,以驱动流体,即气体到涡轮叶片(130)上, 。 环形壁(94)从涡轮机装置(40)的一个端部向外延伸,以限定用于接合芯(24)的座(96),以在油漆线(26)和轴之间保持固定间隙 (104)并且消除它们之间的接触。

    Rotational atomizer turbine and rotational atomizer
    13.
    发明申请
    Rotational atomizer turbine and rotational atomizer 有权
    旋转雾化器涡轮机和旋转雾化器

    公开(公告)号:US20050258270A1

    公开(公告)日:2005-11-24

    申请号:US10895446

    申请日:2003-12-17

    IPC分类号: B05B5/04 B05B3/10

    CPC分类号: B05B5/0415

    摘要: A rotational atomizer turbine of the present invention is designed to drive a bell-shaped disk in a rotational atomizer for a coating unit. The rotational atomizer turbine includes a housing, a rotatable turbine wheel with several turbine blades connected to a shaft and rotatably disposed in the housing. A plurality of nozzles are defined in the housing and are positioned relative the turbine wheel to drive fluid, i.e. gas onto the turbine blades. An intermediate chamber formed in the housing is fluidly communicated with and connected to the nozzles to hold gas therein. The intermediate chamber has a first inlet to supply gas. At least a second inlet is defined in the intermediate chamber for delivering gas into the intermediate chamber thereby increasing amount of gas therein to multiply a rotational speed of the rotatable turbine wheel as increased amount of gas is introduced to the turbine blades.

    摘要翻译: 本发明的旋转雾化器涡轮机被设计成驱动用于涂覆单元的旋转雾化器中的钟形盘。 旋转雾化器涡轮机包括壳体,具有连接到轴并且可旋转地设置在壳体中的多个涡轮叶片的可旋转涡轮机叶轮。 多个喷嘴限定在壳体中并且相对于涡轮机轮定位以驱动流体,即气体到涡轮机叶片上。 形成在壳体中的中间室与喷嘴流体连通并连接到喷嘴以在其中保持气体。 中间室具有供应气体的第一入口。 至少第二入口限定在中间室中,用于将气体输送到中间室中,从而增加其中的气体量,以随着气体的量增加到涡轮叶片而增加可旋转涡轮机叶轮的转速。

    ROTARY ATOMIZER WITH A SPRAYING BODY
    16.
    发明申请
    ROTARY ATOMIZER WITH A SPRAYING BODY 有权
    带喷雾体的旋转原型

    公开(公告)号:US20100206962A1

    公开(公告)日:2010-08-19

    申请号:US12692067

    申请日:2010-01-22

    IPC分类号: B05B3/10

    摘要: A rotary sprayer for a coating apparatus is disclosed. An exemplary rotary sprayer may include a spraying body configured to be mounted on a drive shaft of a drive motor for rotation with the drive shaft. The spraying body may further include a detachable mounting device for coaxial connection of the spraying body to the drive shaft. The detachable mounting device may include a spraying body thread that mates with a driveshaft thread defined by the drive shaft, and a plurality of elastic tabs configured to abut a corresponding cavity defined by the driveshaft, such that rotation of the spraying body increases an abutment force between the elastic tabs and the corresponding cavity of the driveshaft.

    摘要翻译: 公开了一种用于涂布装置的旋转喷雾器。 示例性旋转喷雾器可以包括喷雾体,其构造成安装在驱动马达的驱动轴上,用于与驱动轴一起旋转。 喷雾体还可以包括可拆卸的安装装置,用于使喷射体与驱动轴同轴连接。 可拆卸的安装装置可以包括与由驱动轴限定的驱动轴线配合的喷射体螺纹,以及构造成邻接由驱动轴限定的相应空腔的多个弹性突出部,使得喷射体的旋转增加邻接力 在弹性翼片和驱动轴的相应空腔之间。