Heat sinks with distributed and integrated jet cooling
    43.
    发明授权
    Heat sinks with distributed and integrated jet cooling 有权
    散热器采用分布式和集成式喷射冷却

    公开(公告)号:US08496049B2

    公开(公告)日:2013-07-30

    申请号:US12421068

    申请日:2009-04-09

    IPC分类号: H05K7/20

    摘要: A heat sink with distributed jet cooling is provided. The heat sink includes a base for thermal connection to at least one heated object, an array of fins thermally coupled to the base, and at least one multi-orifice synthetic jet or multiple single orifice jets disposed on a side of the array of fins. A heat sink with distributed and integrated jet cooling is also provided and includes a base and an array of fins. Respective ones of at least a subset of the fins comprise a synthetic jet configured to eject an ambient fluid into an ambient environment of the fins and base. Another heat sink with distributed and integrated jet cooling is provided and includes a base, an array of fins and multiple synthetic jets coupled to respective ones of the fins. The synthetic jets are provided for at least a subset of the fins.

    摘要翻译: 提供分布式喷射冷却的散热器。 散热器包括用于热连接到至少一个被加热物体的基座,热耦合到基座的翅片阵列,以及设置在翅片阵列侧面的至少一个多孔合成射流或多个单孔射流。 还提供了具有分布式和集成式射流冷却的散热器,并且包括底座和翅片阵列。 翅片的至少一个子集中的各个翼片包括配置成将周围流体喷射到翅片和底座的周围环境中的合成射流。 提供了具有分布式和集成的喷射式冷却的另一散热器,并且包括底座,翅片阵列和耦合到相应散热片的多个合成射流。 合成射流被提供用于鳍的至少一个子集。

    Method and apparatus for reducing acoustic noise in a synthetic jet
    47.
    发明授权
    Method and apparatus for reducing acoustic noise in a synthetic jet 有权
    减少合成射流噪声的方法和装置

    公开(公告)号:US08006917B2

    公开(公告)日:2011-08-30

    申请号:US12198240

    申请日:2008-08-26

    IPC分类号: B05B1/08

    摘要: A synthetic jet includes a first backer structure and a first actuator coupled to the first backer structure to form a first composite unit. The synthetic jet also includes a second backer structure, and a second actuator coupled to the second backer structure to form a second composite unit. A wall member is coupled to and positioned between the first and second backer structures to form a cavity. The first composite unit has an orifice formed therethrough and the orifice is fluidically coupled to the cavity and fluidically coupled to an environment external to the cavity.

    摘要翻译: 合成射流包括第一支撑结构和耦合到第一支撑结构的第一致动器,以形成第一复合单元。 合成射流还包括第二支撑结构,以及耦合到第二支撑结构以形成第二复合单元的第二致动器。 壁构件联接到第一和第二支撑结构之间并定位在第一和第二支撑结构之间以形成空腔。 第一复合单元具有穿过其形成的孔,并且孔流体地联接到空腔并且流体耦合到空腔外部的环境。

    Systems and methods for synthetic jet enhanced natural cooling
    48.
    发明授权
    Systems and methods for synthetic jet enhanced natural cooling 有权
    合成射流的系统和方法增强了自然冷却

    公开(公告)号:US07990705B2

    公开(公告)日:2011-08-02

    申请号:US12118435

    申请日:2008-05-09

    摘要: A method and system for increasing cooling of an enclosure is provided. The component enclosure includes one or more sidewalls defining a volume, the sidewalls are configured to substantially surround a heat generating component positioned within the volume. The component enclosure further includes a synthetic jet assembly positioned adjacent at least one of the sidewalls. The synthetic jet assembly includes at least one synthetic jet ejector having a jet port. The jet port is aligned at least one of perpendicularly, parallelly, and obliquely with a surface of the at least one sidewall. The synthetic jet assembly is configured to direct a jet of fluid through the port at least one of substantially parallel to the surface, perpendicularly onto the surface, and obliquely toward the surface.

    摘要翻译: 提供了一种用于增加外壳冷却的方法和系统。 部件外壳包括限定一个体积的一个或多个侧壁,该侧壁被配置为基本上围绕定位在该体积内的发热部件。 组件外壳还包括邻近至少一个侧壁定位的合成射流组件。 合成射流组件包括具有喷射口的至少一个合成射流喷射器。 喷射口与至少一个侧壁的表面垂直,平行和倾斜地至少一个排列。 合成射流组件构造成将流体射流引导通过端口至少一个基本上平行于表面垂直于表面并且倾斜地朝向表面。