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    • 6. 发明申请
    • DETACHABLE HULA HOOP HAVING WATERPROOF RESERVOIRS
    • 具有防水储藏室的可拆卸的HULA HOUSE
    • US20160016093A1
    • 2016-01-21
    • US14738826
    • 2015-06-12
    • CHENG-HSIUNG HSUSU-CHEN LI
    • CHENG-HSIUNG HSUSU-CHEN LI
    • A63H33/00A63B19/00
    • A63H33/00A63B19/00A63B2210/50
    • A detachable hula hoop having waterproof reservoirs is provided with hollow arc sections each including a neck; a first connection end at a first end and including an opening, a channel, and a first recess on a surface; a plug including a cylindrical member and a head; a second connection end at a second end and including a closed member and a second recess on a surface; and a reservoir. The first recess is complimentarily disposed in the second recess to fasten the first and second connection ends together. The cylindrical member is disposed in the neck, the head urges against an annular shoulder to block the neck, and the head is urged against by the closed member.
    • 具有防水容器的可分离的呼啦圈设置有各自包括颈部的中空弧形部分; 在第一端处的第一连接端,并且包括开口,通道和表面上的第一凹部; 包括圆柱形构件和头部的塞子; 在第二端处的第二连接端,并且包括封闭构件和表面上的第二凹部; 和一个水库。 第一凹部被补充地设置在第二凹部中,以将第一和第二连接端紧固在一起。 圆柱形构件设置在颈部中,头部抵靠环形肩部阻止颈部,并且头部被封闭构件推靠。
    • 7. 发明申请
    • VTOL aircraft with a thrust-to-weight ratio smaller than 0.08
    • 垂直起落飞机的推力重量比小于0.08
    • US20150336665A1
    • 2015-11-26
    • US14285462
    • 2014-05-22
    • Chen Li Jing
    • Chen Li Jing
    • B64C29/00B64C15/02B64C23/00B64D27/20B64D35/02B64C9/00B64D27/02
    • B64C29/0066B64C29/0025
    • VTOL aircraft with a thrust-to-weight ratio smaller than 0.08, during vertical take-off/landing, obtains most vertical lift, besides traditional small vertical lift by high-temp bypass slot outlet (6) directing, under its opening, the closing of the tail of the power-off jet engine (3) by the valve (7) in tail cone, the closing and the stretching of the propelling nozzle (5), high-temp air (8) to spout out along the inclined downward direction of the wingspan, by a centrifugal impeller (13) accelerating, under the connecting of the transmission shaft (11) with a jet engine (4), and the opening of the cabin doors (15, 17) of the inlet (18) of the low-temp duct (16) and the auxiliary engine's inlet (14), low-temp air (21) to flow through the low-temp duct (21) and flow over the upper surface of the wing but not burn up it along the wingspan direction, thereby generating most vertical lift and enabling ailerons (1, 2) to control balances of the aircraft.
    • 垂直起升/着陆期间,推力重量比小于0.08的垂直起降飞机,除了传统的小型垂直升降机外,还有高温旁路槽出口(6),在其开启时指示关闭 通过阀门(7)在尾锥中的关闭喷气发动机(3)的尾部,推进喷嘴(5)的关闭和拉伸,高温空气(8)沿倾斜向下喷出 通过在传动轴(11)与喷气发动机(4)的连接下的离心式叶轮(13)加速翼展的方向,以及入口(18)的舱门(15,17)的开口, 的低温管道(16)和辅助发动机的入口(14),低温空气(21)流过低温管道(21)并流过机翼的上表面但不燃烧 沿翼展方向,从而产生大多数垂直升降机,并使副翼(1,2)能够控制飞机的平衡。
    • 10. 发明授权
    • Water-cooled heat sink
    • 水冷散热器
    • US08550149B2
    • 2013-10-08
    • US12650871
    • 2009-12-31
    • Jun WangChien-Ming ChihChen-Li Kao
    • Jun WangChien-Ming ChihChen-Li Kao
    • F28F7/00H05K7/20F04B17/00
    • H01L23/473G06F1/20G06F2200/201H01L2924/0002H01L2924/00
    • A water-cooled heat sink includes a base, a box, a propelling module, a driving module, and a plurality of conduits. The box is disposed above the base, and receives a cooled liquid. The driving module includes a first magnet. The base defines a plurality of channels. The propelling module includes a cylinder, a piston, a second magnet, and a valve. The cylinder is disposed on an inner wall of the box. The piston is disposed in the cylinder, and defines a through hole in a middle portion thereof. The second magnet is fixed to the piston. The valve is fixed in the through hole. The conduits interconnect the cylinder and the box. The first magnet can repel or attract the second magnet, thereby sliding the piston toward the cylinder to close the valve or away from the cylinder to open the valve.
    • 水冷散热器包括基座,箱体,推进模块,驱动模块和多个导管。 箱体设置在基座上方,并接收冷却液体。 驱动模块包括第一磁体。 基座定义了多个通道。 推进模块包括气缸,活塞,第二磁体和阀。 气缸设置在箱体的内壁上。 活塞设置在气缸中,并在其中间部分形成通孔。 第二个磁体固定在活塞上。 阀固定在通孔中。 导管将气缸和箱体相互连接。 第一磁体可以排斥或吸引第二磁体,从而将活塞滑向气缸以关闭阀门或离开气缸以打开阀门。