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公开(公告)号：US20240175393A1
公开(公告)日：2024-05-30
申请号：US18351481
申请日：2023-07-12
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
CPC分类号： F02C3/32 , F01D5/147 , F01D5/18 , F01D5/186 , F01D5/187 , F02C3/04 , F05D2220/32 , F05D2220/40 , Y02T50/60
摘要： A fluid supercharging device (3, 5), comprising: a rotating shaft (7); a vane disc (308) coaxially fixed to the rotating shaft (7); a plurality of fan blades (301) fixed around a perimeter of the vane disc (308); the back side of the fan blades 301 being provided with at least one fluid guiding inlet (305), an end of the back side distal from the vane disc (308) is provided with a fluid guiding outlet (306, 307), a fluid channel (304) communicating the fluid guiding inlet (305) with the fluid guiding outlet (306, 307) is provided along a lengthwise direction inside the fan blades; the fan blades (301) rotate to generate a centrifugal force such that a fluid flows into the fluid channel via the fluid guiding inlet on the back side, and flows out of the fluid guiding outlet along the lengthwise direction of the fan blades.
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公开(公告)号：US20210340909A1
公开(公告)日：2021-11-04
申请号：US17373816
申请日：2021-07-13
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
摘要： A fluid supercharging device (3, 5), comprising: a rotating shaft (7); a vane disc (308) coaxially fixed to the rotating shaft (7); a plurality of fan blades (301) fixed around a perimeter of the vane disc (308); the back side of the fan blades 301 being provided with at least one fluid guiding inlet (305), an end of the back side distal from the vane disc (308) is provided with a fluid guiding outlet (306, 307), a fluid channel (304) communicating the fluid guiding inlet (305) with the fluid guiding outlet (306, 307) is provided along a lengthwise direction inside the fan blades; the fan blades (301) rotate to generate a centrifugal force such that a fluid flows into the fluid channel via the fluid guiding inlet on the back side, and flows out of the fluid guiding outlet along the lengthwise direction of the fan blades.
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公开(公告)号：US20140152050A1
公开(公告)日：2014-06-05
申请号：US14176141
申请日：2014-02-09
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
IPC分类号： B62D35/00
CPC分类号： B62D35/00 , B62D35/001 , B62D35/02 , Y02T10/88 , Y02T70/121
摘要： A vehicle including a housing. The housing includes an outer portion, an inner portion, an air-flow channel, a plurality of air inlets, an air outlet, and a spoiler surface or a spoiler. The air-flow channel is disposed between the outer portion and the inner portion of the housing. The air inlets are disposed on the outer portion of the housing, and the air outlet is disposed at a rear of the outer portion of the housing. The air-flow channel communicates with the air inlets and the air outlet. The spoiler surface or the spoiler is disposed on a bottom of the outer portion of the housing, a top of the inner portion of the housing, or both the bottom of the outer portion and the top of the inner portion of the housing, for extending path of the air.
摘要翻译： 一种包括壳体的车辆。 壳体包括外部部分，内部部分，空气流动通道，多个空气入口，空气出口和扰流板表面或扰流板。 气流通道设置在壳体的外部部分和内部之间。 空气入口设置在壳体的外部，并且空气出口设置在壳体的外部的后部。 气流通道与空气入口和出气口连通。 扰流器表面或扰流板设置在壳体的外部的底部，壳体的内部的顶部，或者外部的底部和壳体的内部的顶部之间，用于延伸 空中之路
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公开(公告)号：US20240124131A1
公开(公告)日：2024-04-18
申请号：US18517212
申请日：2023-11-22
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
CPC分类号： B64C21/02 , B64C3/14 , B64C11/18 , B64C2230/08 , B64C2230/20 , B64C2230/28
摘要： The invention discloses an aircraft generating a larger thrust and lift by fluid continuity. First open channels used to extend fluid paths are formed in front parts and/or middle parts of windward sides of wings of the aircraft and extend from sides, close to the fuselage, of the wings to sides, away from the fuselage, of the wings, and the first open channels are concave channels or convex channels, so that a pressure difference in a direction identical with a moving direction is generated from back to front due to different flow speeds of fluid flowing over the windward sides of the wings in a lengthwise direction and a widthwise direction to reduce fluid resistance, and a larger pressure difference and lift are generated due to different flow speeds on the windward sides and leeward sides of the wings.
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公开(公告)号：US20190283857A9
公开(公告)日：2019-09-19
申请号：US15655409
申请日：2017-07-20
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
摘要： The invention discloses a flight vehicle generating a lift from an interior thereof. The fluid channel inside the flight vehicle communicates with the engine and the ports on the upper surface of the outer shell. With the powerful suction of the engine, the fluid on the upper surface of the outer shell is quickly sucked into the fluid channel via respective ports under conditions of long path, large area, high speed and low air pressure, which results in large lift from the interior of the flight vehicle. In the course of generating the lift, the fluid resistances of the fluid wall and the fluid hole are sucked into the fluid channel through the ports at the front and the surrounding area of the flight vehicle, then high-speed fluid is emitted from the rear port. This approach contributes greatly to the transformation of the existing flight vehicle. The present invention significantly improves the lift, the speed and the carrying capacity of the existing flight vehicle with lowered energy consumption.
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公开(公告)号：US20170029100A1
公开(公告)日：2017-02-02
申请号：US15293223
申请日：2016-10-13
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
CPC分类号： B64C27/16 , B64C11/16 , B64C11/24 , B64C27/473 , F01D1/32 , F01D5/12 , F01K25/02 , F02B39/02 , F02C3/107
摘要： The present invention provides a power device generating greater propelling force and finds that traditional power devices do not include all propelling forces based on the fundamental core propelling force source problem. External pressure is guided to the traditional power devices since the inner speed is higher the outer speed, power consumption for overcoming fluid resistance is high, and mutual contradiction results are obtained. The unique difference between the present invention and general common sense lies in opposite fluid pressure directions; inner fluid channels and outer fluid channels with higher flow speeds are formed to generate pressure differences which guides the fluid pressure to the outside and serve as propelling force, and thus the present invention creatively finds three propelling force sources, two lifting force or propelling force sources of helicopters or airplanes driven by propellers and two propelling force sources for sufficient burning of fuel in combustion chambers of engines.
摘要翻译： 本发明提供了一种产生更大推进力的动力装置，并且发现传统的动力装置不包括基于基本的推进力源问题的所有推进力。 外部压力被引导到传统的功率器件，因为内部速度较高，外部的速度更高，克服流体阻力的功耗高，并且获得了相互矛盾的结果。 本发明和一般常识之间的独特差异在于相反的流体压力方向; 形成具有较高流速的内部流体通道和外部流体通道以产生将流体压力引导到外部并用作推进力的压力差，因此本发明创造性地找到三个推进力源，两个提升力或推进力源 由螺旋桨驱动的直升机或飞机和两个推进力源，用于在发动机的燃烧室中充分燃烧燃料。
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公开(公告)号：US20240083572A1
公开(公告)日：2024-03-14
申请号：US18517685
申请日：2023-11-22
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
IPC分类号： B64C27/16 , B64C11/16 , B64C11/24 , B64C27/473 , F01D1/32 , F01D5/12 , F01K25/02 , F02B19/00 , F02B23/04 , F02B39/02 , F02C3/107 , F02F3/00
CPC分类号： B64C27/16 , B64C11/16 , B64C11/24 , B64C27/473 , F01D1/32 , F01D5/12 , F01K25/02 , F02B19/00 , F02B23/04 , F02B39/02 , F02C3/107 , F02F3/0076
摘要： The present invention provides a power device generating greater propelling force and finds that traditional power devices do not include all propelling forces based on the fundamental core propelling force source problem. External pressure is guided to the traditional power devices since the inner speed is higher the outer speed, power consumption for overcoming fluid resistance is high, and mutual contradiction results are obtained. The unique difference between the present invention and general common sense lies in opposite fluid pressure directions; inner fluid channels and outer fluid channels with higher flow speeds are formed to generate pressure differences which guides the fluid pressure to the outside and serve as propelling force, thus the present invention creatively finds three propelling force sources, two lifting force or propelling force sources of helicopters or airplanes driven by propellers and two propelling force sources for sufficient burning of fuel in combustion chambers of engines.
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公开(公告)号：US20200017198A1
公开(公告)日：2020-01-16
申请号：US16564844
申请日：2019-09-09
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
摘要： The invention discloses a lift source for an aircraft comprising a fuselage and wings, wherein first channels are formed in the wings, a plurality of first inlets are formed in upper surfaces of the wings, a plurality of first pressure ports are formed in lower surfaces of the wings and are communicated with the first inlets via the first channels; and spoiler devices are arranged in the first channels and under the effect of the spoiler devices, form high-speed fluid layers on the upper surfaces of the wings, thereby generating a pressure difference from the lower surfaces of the wings which counteracts an external fluid pressure on the upper surfaces of the wings in the opposite direction, so a lift is generated by reduction of fluid resistance when fluid flows through the upper and lower surfaces of the wings, thereby developing a high-speed aircraft with a larger lift and thrust.
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公开(公告)号：US20190113051A1
公开(公告)日：2019-04-18
申请号：US16163539
申请日：2018-10-17
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
摘要： The present disclosure relates to a bladeless fan, which includes a housing and a power device, wherein the power device communicates with a fluid passage and a negative pressure passage disposed in the housing respectively; the fluid passage communicates with the outside through a plurality of exhaust ports, and the negative pressure communicates with the outside through a plurality of suction ports; a middle region inside the fluid passage is provided with a spoiler device so that a path along which the fluid passes through the spoiler device is larger than a path along which the fluid passes around the corresponding inner wall, thereby generating a pressure difference. The present disclosure enables a higher-speed flow of the fluid inside the fluid passage through pressure difference without adding extra power, and generates a faster air speed in a more energy-saving way, thereby achieving a remarkable effect of cooling.
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公开(公告)号：US20180362103A1
公开(公告)日：2018-12-20
申请号：US16117925
申请日：2018-08-30
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
摘要： Disclosed is an automobile, comprising an automobile body, wheels, a suspension device and a spoiler. The path of a fluid flowing through a lower spoiler surface is longer than the path of the fluid flowing through the upper spoiler surface, so that a lift force generated in the driving process of the automobile is reduced or even eliminated. The general understanding that the wheels bear the dead weight of the automobile, loads and all weights generated by the gravitational acceleration is changed. The dead weight of the automobile body is reduced by the lift force generated by the automobile body, the road holding of the automobile is improved after the wheels eliminate the lift force, and thus, the automobile can save more energy and can run more safely.
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