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    • 4. 发明授权
    • Cooling system for aerospace vehicle components
    • 航空航天部件冷却系统
    • US08950468B2
    • 2015-02-10
    • US11747467
    • 2007-05-11
    • David E. Blanding
    • David E. Blanding
    • F28F3/12F28F1/32B64D13/00B64D13/06
    • B64D47/00B64D13/006B64D2013/0614H05K7/20854Y02T50/44
    • A cooling system for removing heat generated by electrical components onboard aerospace vehicles flows coolant between an evaporator that removes heat from the component, and a condenser within the skin of the vehicle. The skin is formed from facesheets comprising multiple layers of polymer resin reinforced with meshes of single and double wall nanotubes. The nanotubes conduct the heat directionally so as to both distribute the heat over the skin and direct the heat to the outer surface of the skin where the heat can be carried away by air flowing over the skin. The skin may also include conductive carbon foam surrounding the condenser to reduce thermal resistance between the condenser and the facesheets.
    • 用于去除航空航天车辆上的电气部件产生的热量的冷却系统在从部件移除热量的蒸发器与车辆皮肤内的冷凝器之间流动冷却剂。 皮肤由包含多层聚合物树脂的面板形成,所述聚合物树脂用单壁和双壁纳米管的网格增强。 纳米管定向地引导热量,以便将热量分布在皮肤上并将热量引导到皮肤的外表面,在该外表面可以通过流过皮肤的空气带走热量。 皮肤还可以包括围绕冷凝器的导电碳泡沫,以减少冷凝器和面板之间的热阻。
    • 6. 发明申请
    • Cooling System for Aerospace Vehicle Components
    • 航空航天部件冷却系统
    • US20100132915A1
    • 2010-06-03
    • US11747467
    • 2007-05-11
    • David E. Blanding
    • David E. Blanding
    • B60H1/00B64G1/52B64G1/58
    • B64D47/00B64D13/006B64D2013/0614H05K7/20854Y02T50/44
    • A cooling system for removing heat generated by electrical components onboard aerospace vehicles flows coolant between an evaporator that removes heat from the component, and a condenser within the skin of the vehicle. The skin is formed from facesheets comprising multiple layers of polymer resin reinforced with meshes of single and double wall nanotubes. The nanotubes conduct the heat directionally so as to both distribute the heat over the skin and direct the heat to the outer surface of the skin where the heat can be carried away by air flowing over the skin. The skin may also include conductive carbon foam surrounding the condenser to reduce thermal resistance between the condenser and the facesheets.
    • 用于去除航空航天车辆上的电气部件产生的热量的冷却系统在从部件移除热量的蒸发器与车辆皮肤内的冷凝器之间流动冷却剂。 皮肤由包含多层聚合物树脂的面板形成,所述聚合物树脂用单壁和双壁纳米管的网格增强。 纳米管定向地引导热量,以便将热量分布在皮肤上并将热量引导到皮肤的外表面,在该外表面可以通过流过皮肤的空气带走热量。 皮肤还可以包括围绕冷凝器的导电碳泡沫,以减少冷凝器和面板之间的热阻。
    • 9. 发明授权
    • Amplifier for amplification of a microactuator
    • 用于放大微致动器的放大器
    • US6034466A
    • 2000-03-07
    • US996377
    • 1997-12-22
    • David E. BlandingJimmy L. Schmidt
    • David E. BlandingJimmy L. Schmidt
    • H01L41/09H02N2/04H01L41/08
    • H02N2/043
    • The amplifier assembly includes a driver bellows and an output bellows. The driver bellows includes a first end and a second end. The first end is positionable adjacent a microactuator. The output bellows includes a first end and a second end. The first end of the output bellows is securely attached to the second end of the driver bellows. The second end of the output bellows is positionable adjacent a device to be actuated. The output bellows has a smaller volume than the driver bellows. Each bellows is filled with a working fluid. When the driver bellows is compressed by the microactuator the fluid displacement of the driver bellows is translated to the output bellows causing a displacement in the output bellows equal to the fluid displaced in the driver bellows. Thus, an amplified output stroke is provided of the desired magnitude.
    • 放大器组件包括驱动器波纹管和输出波纹管。 驱动器波纹管包括第一端和第二端。 第一端可定位在微致动器附近。 输出波纹管包括第一端和第二端。 输出波纹管的第一端牢固地连接到驱动器波纹管的第二端。 输出波纹管的第二端可定位在要被致动的装置附近。 输出波纹管的体积小于驱动器波纹管。 每个波纹管都装有工作流体。 当驱动器波纹管被微型致动器压缩时,驱动器波纹管的流体位移被转换成输出波纹管,导致输出波纹管中的位移等于在驱动器波纹管中移位的流体。 因此,提供期望幅度的放大输出冲程。