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    • 32. 发明授权
    • Heat pipe
    • 热管
    • US5314011A
    • 1994-05-24
    • US079323
    • 1993-06-17
    • Bernhard LeidingerRuediger MeyerKlaus P. Nickel
    • Bernhard LeidingerRuediger MeyerKlaus P. Nickel
    • F28D15/04F28D15/02
    • F28D15/046
    • A heat pipe is divided longitudinally by a divider wall into a vapor channel and into a liquid channel. The divider wall is provided, preferably at uniform axial spacings with bulges that form a restriction in the flow cross-sectional area of the vapor channel and an increase in the flow cross-sectional area of the liquid channel. A small diameter through bore is positioned at the peak of each bulge to connect the liquid channel with the vapor channel at this point. The reduced pressure at the restriction in the vapor channel is sufficient to suck gas or vapor bubbles collected under the bulge into the vapor channel, but insufficient to pull liquid into the vapor channel. The cross-sectional flow area of the liquid channel increases steadily toward each bulge, either from a point centrally between two bulges or from a point directly downstream of a bulge toward the next bulge as viewed in the flow direction of the liquid.
    • 热管由分隔壁纵向划分成蒸汽通道并进入液体通道。 优选地,分隔壁设置有均匀的轴向间隔,其具有在蒸气通道的流动横截面积中形成限制的凸起,以及液体通道的流动横截面面积的增加。 此时,一个小直径通孔位于每个凸起的顶部,以将液体通道与蒸汽通道连接。 在蒸汽通道中的限制下的减压足以将在膨胀下收集的气体或蒸汽气体吸入蒸汽通道,但不足以将液体吸入蒸气通道。 液体通道的横截面流动区域从液体的流动方向观察时,从两个凸起之间的中心点或从凸起的直接下游的点到下一个凸起,朝向每个凸起稳定地增加。
    • 33. 发明授权
    • Evaporation heat exchanger, especially for a spacecraft
    • 蒸发换热器,特别适用于航天器
    • US5289871A
    • 1994-03-01
    • US970803
    • 1992-11-03
    • Bernhard Leidinger
    • Bernhard Leidinger
    • B64G1/50F28D7/08F28B1/02
    • F28F1/02B64G1/50F28D7/08F28D7/085Y10S165/903
    • An evaporation heat exchanger having at least one active circulating circuit for a coolant liquid to be cooled, is constructed for removing heat in a spacecraft under a gravity-free operating condition and under different acceleration conditions. For this purpose, a housing encloses an evaporating space provided with at least one inlet valve for controlling the admission of a medium to be evaporated. The produced vapor or steam is discharged through a respective outlet port. A plurality of cooling tubes interconnected in a meandering shape form a number of tube panels in which the individual tubes are arranged with a different spacing from one another in a direction from the inlet valve to the outlet port. Preferably, these spacings increase in the flow direction from the inlet port to the outlet port to establish a constant flow speed for the evaporating medium. The tubes forming a panel may be arranged in a zig-zag pattern within the panel.
    • 具有用于待冷却的冷却剂液体的至少一个有效循环回路的蒸发热交换器被构造用于在无重力运行条件下和在不同加速条件下移除航天器中的热量。 为此目的,壳体包围设置有至少一个入口阀的蒸发空间,用于控制允许要蒸发的介质。 产生的蒸气或蒸汽通过相应的出口排出。 以曲折形状互连的多个冷却管形成多个管板,其中各个管在从入口阀到出口的方向上以彼此不同的间隔布置。 优选地,这些间隔在从入口到出口的流动方向上增加,以为蒸发介质建立恒定的流速。 形成面板的管可以在面板内以锯齿形图案布置。
    • 34. 发明授权
    • Evaporation heat exchanger apparatus for removing heat
    • 用于除热的蒸发式热交换器装置
    • US5253701A
    • 1993-10-19
    • US940471
    • 1992-09-04
    • Bernhard Leidinger
    • Bernhard Leidinger
    • F25B39/02B01D1/04B64G1/50F28D5/00F28D7/16F28F9/22G05D23/12
    • F28F9/22B01D1/04B64G1/50F28D5/00F28F2009/226
    • Heat generated, for example, in a spacecraft under zero gravity conditions and different accelerations is discharged through an evaporation heat exchanger connected to at least one active coolant circulation circuit. The heat exchanger has a bundle of tubes axially arranged inside a cylindrical processing chamber. An evaporant passes through these tubes. A coolant flows into heat exchange contact with outer surfaces of said tubes. The outlet cross-sectional flow area for the evaporant, or rather its vapor, is variable so that the pressure of the evaporated medium, and thereby also its evaporation temperature are adjustable. The adjustment of the cross-sectional flow area for the vapor is controlled in response to the temperature of the cooling liquid or coolant where it enters into a processing chamber of the heat exchanger. Selectively closable apertures in an end plate (52) serve for changing the outlet cross-section flow area for the vapor. The apertures are, at least partially, closable by flaps which are controlled by bimetal springs responsive to the temperature of the entering coolant.
    • 例如,在零重力条件下的航天器中产生的热量和不同的加速度通过连接到至少一个主动冷却剂循环回路的蒸发热交换器排出。 热交换器具有轴向布置在圆柱形处理室内的一束管。 蒸发器通过这些管。 冷却剂流入与所述管的外表面的热交换接触。 蒸发器或其蒸气的出口横截面流动面积是可变的,使得蒸发介质的压力以及由此蒸发介质的蒸发温度是可调节的。 响应于其进入热交换器的处理室的冷却液体或冷却剂的温度来控制蒸汽的横截面流动面积的调节。 端板(52)中的可选择闭合的孔用于改变蒸气的出口横截面流动面积。 至少部分地,所述孔可以通过响应于进入的冷却剂的温度的双金属弹簧控制的襟翼来关闭。