Chassis with distributed jet cooling
    13.
    发明公开
    Chassis with distributed jet cooling 审中-公开
    底盘具有集成冷却射流

    公开(公告)号:EP2378848A3

    公开(公告)日:2017-02-22

    申请号:EP11162122.3

    申请日:2011-04-12

    IPC分类号: H05K7/02 H05K7/20

    摘要: A chassis (10) with distributed jet cooling is provided. The chassis includes one or more sidewalls (12) defining a volume configured to substantially surround one or more heat generating components positioned within the volume. The chassis further includes at least one array of fins (14) thermally coupled to a respective one of the one or more sidewalls and at least one synthetic jet assembly (30) comprising a multi-orifice synthetic jet (30) or a number of single orifice synthetic jets (2) disposed on a side (15, 16) of a respective one of the array(s) of fins. The chassis further includes at least one attachment means (4, 6, 9, 11, 20, 44) for attaching a respective one of the at least one synthetic jet assemblies to a respective one of the one or more sidewalls.

    Systems and methods for synthetic jet enhanced natural cooling
    15.
    发明公开
    Systems and methods for synthetic jet enhanced natural cooling 有权
    由合成射流系统和增强自然冷却的方法

    公开(公告)号:EP2116730A2

    公开(公告)日:2009-11-11

    申请号:EP09159255.0

    申请日:2009-04-30

    IPC分类号: F15D1/08

    摘要: A component enclosure (100,300) is provided. The component enclosure includes one or more sidewalls (102,302) defining a volume configured to substantially surround a heat generating component (506) positioned within the volume, and a synthetic jet assembly (304,600) positioned adjacent at least one of the sidewalls, the synthetic jet assembly including at least one synthetic jet ejector (502) including a jet port (306), the jet port aligned at least one of perpendicularly, parallelly, and obliquely with a surface (504) of the at least one sidewall, the synthetic jet assembly is configured to direct a jet of fluid (510) 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: A组分外壳(100,300)被提供。 该组件外壳包括一个或多个侧壁(102.302) - 定义配置成基本上包围的体积内定位的发热构件(506)的体积,并且定位的合成射流组件(304.600)的侧壁的相邻的至少一个,所述合成射流 组件包括至少一个合成射流喷射器(502)包括一个喷射口(306),以垂直的至少一个喷射口,平行,并与所述至少一个侧壁的表面(504)倾斜,所述合成射流组件 被配置为通过端口将流体引导(510)的喷射的大致平行于所述表面,垂直地在表面上的至少一个,并且倾斜地朝向表面。

    Methods and apparatus for operating gas turbine engines
    17.
    发明公开
    Methods and apparatus for operating gas turbine engines 审中-公开
    Methode und Vorrichtung zum Betrieb einer Gurburbine

    公开(公告)号:EP1760291A2

    公开(公告)日:2007-03-07

    申请号:EP06254487.9

    申请日:2006-08-29

    IPC分类号: F02C7/047

    摘要: A method for assembling a turbine engine (10) to facilitate preventing ice accumulation on the turbine engine during engine operation. The method includes coupling a manifold to the gas turbine engine such that the manifold (102) is coupled in thermal communication with a heat source, coupling a first heat pipe (100) to the manifold such that the first heat pipe partially circumscribes the gas turbine engine in a clockwise orientation, and coupling a second heat pipe to the manifold such that the second heat pipe partially circumscribes the gas turbine engine in a counter-clockwise orientation.

    摘要翻译: 一种用于组装涡轮发动机(10)的方法,以便于在发动机运转期间防止在涡轮发动机上积聚积雪。 该方法包括将歧管联接到燃气涡轮发动机,使得歧管(102)与热源热连通地联接,将第一热管(100)联接到歧管,使得第一热管部分地包围燃气轮机 发动机,并且将第二热管联接到歧管,使得第二热管以逆时针方向部分地包围燃气涡轮发动机。

    ADDITIVELY MANUFACTURED COOLING ASSEMBLIES FOR THERMAL AND/OR MECHANICAL SYSTEMS, AND METHODS FOR MANUFACTURING THE ASSEMBLIES

    公开(公告)号:EP3633305A1

    公开(公告)日:2020-04-08

    申请号:EP19200941.3

    申请日:2019-10-01

    IPC分类号: F28D21/00

    摘要: A multi-domain cooling assembly 100 configured to be coupled with one or more heat sources 104 includes a body 118 having an outer surface 102 and at least one cooling chamber 106, 114 disposed inside the body 118. The at least one cooling chamber 106, 114 extends in at least two orthogonal dimensions and includes a working fluid to extract thermal energy from the one or more heat sources 104. The assembly 100 includes a cooling channel 108 disposed within the body 118 and fluidly coupled with a passageway 110, 112 that carries cooling fluid into and out of the cooling channel 108. At least a portion of the cooling fluid is a liquid phase, a gas phase, or a liquid-gas mix phase. The cooling channel 108 is fluidly separate from the at least one cooling chamber 106, 114. The cooling channel 108 is thermally coupled with the at least one cooling chamber 106, 114. The at least one cooling chamber 106, 114 transfers thermal energy from the working fluid to the cooling fluid.