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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：US11866160B2
公开(公告)日：2024-01-09
申请号：US17982629
申请日：2022-11-08
申请人： Xiaoyi Zhu
发明人： Xiaoyi Zhu
IPC分类号： B64C27/16 , F01D5/12 , F01D1/32 , B64C11/16 , B64C1/16 , F02F3/00 , F02B23/04 , F02B19/00 , B64C11/24 , B64C27/473 , F01K25/02 , F02B39/02 , F02C3/107
CPC分类号： B64C27/16 , B64C1/16 , 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：US11858617B2
公开(公告)日：2024-01-02
申请号：US17843700
申请日：2022-06-17
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：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：US09835085B2
公开(公告)日：2017-12-05
申请号：US14456385
申请日：2014-08-11
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 , Y02T50/676
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：US20160229517A1
公开(公告)日：2016-08-11
申请号：US14295350
申请日：2014-06-04
申请人： XIAOYI ZHU
发明人： XIAOYI ZHU
IPC分类号： B64C3/14
CPC分类号： B64C3/141 , B64C21/10 , B64C39/026 , B64C2230/26 , B64D27/02 , Y02T50/12 , Y02T50/166
摘要： The invention discloses an aircraft generating a larger lift from its interior. The fluid channel inside the aircraft 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 aircraft. 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 aircraft, then high-speed fluid is emitted from the rear port. This approach contributes greatly to the transformation of the existing aircraft. The unified big wing significantly improves the lift, the speed and the carrying capacity of the existing aircraft with lowered energy consumption.
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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：US08408635B2
公开(公告)日：2013-04-02
申请号：US13335913
申请日：2011-12-22
申请人： Xiaoyi Zhu
发明人： Xiaoyi Zhu
IPC分类号： B62D35/00
摘要： An energy-saving vehicle including a housing, a pair of front wheels, a pair of rear wheels, and a steering wheel. The housing includes an outer portion, an inner portion, an air-flow channel, at least a first air inlet, and at least an air outlet. The air-flow channel is disposed between the outer portion and the inner portion of the housing. The first air inlet is disposed in the front of the vehicle. The air outlet is disposed at the back of the vehicle. The first air inlet and the air outlet are connected to the air-flow channel. The front wheels and the rear wheels are driven by a power unit. The length of the air-flow channel is no less than that of the upper portion of the housing. The vehicle consumes less energy and travels more stably compared to conventional vehicles.
摘要翻译： 一种节能车辆，包括壳体，一对前轮，一对后轮和方向盘。 壳体包括外部部分，内部部分，空气流动通道，至少第一空气入口以及至少一个空气出口。 气流通道设置在壳体的外部部分和内部之间。 第一进气口设置在车辆的前方。 出风口设置在车辆的后部。 第一进气口和出风口连接到气流通道。 前轮和后轮由动力单元驱动。 气流通道的长度不小于壳体上部的长度。 与常规车辆相比，车辆消耗的能量更少，行驶更稳定。
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公开(公告)号：US08113569B2
公开(公告)日：2012-02-14
申请号：US12559543
申请日：2009-09-15
申请人： Xiaoyi Zhu
发明人： Xiaoyi Zhu
IPC分类号： B60J7/00
摘要： An energy-saving vehicle, has a housing including an outer portion, an inner portion, an air-flow channel, at least a first air inlet, and at least an air outlet, a pair of front wheels, a pair of rear wheels, and a steering wheel. The air-flow channel is disposed between the outer portion and the inner portion of the housing. The first air inlet is disposed in the front of the vehicle The air outlet is disposed at the back of the vehicle, The first air inlet and the air outlet are connected to the air-flow channel. The front wheels and the rear wheels are driven by a power unit. The length of the air-flow channel is no less than that of the upper portion of the housing. As the vehicle travels at a high velocity, air is led in from the air inlet and sprayed from the back of the vehicle, instantly filling a low pressure region at the back of the vehicle and turning the back of the vehicle into a high pressure region, which saves energy. Moreover, since the length of the air-flow channel is larger than that of the upper portion of the housing, lift resistance is eliminated, and the vehicle travels more stably.
摘要翻译： 一种节能车，具有外壳，内部，空气流路，至少第一空气入口，至少一个空气出口，一对前轮，一对后轮， 和方向盘。 气流通道设置在壳体的外部部分和内部之间。 第一进气口设置在车辆的前部。空气出口设置在车辆的后部，第一进气口和出气口连接到空气流动通道。 前轮和后轮由动力单元驱动。 气流通道的长度不小于壳体上部的长度。 当车辆高速行驶时，空气从空气入口引入并从车辆背面喷射，立即填充车辆后部的低压区域并将车辆的后部转向高压区域 ，节省能源。 此外，由于气流通道的长度大于壳体的上部的长度，因此消除了提升阻力，并且车辆行进更稳定。
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公开(公告)号：US20220324554A1
公开(公告)日：2022-10-13
申请号：US17843700
申请日：2022-06-17
申请人： Xiaoyi ZHU
发明人： Xiaoyi ZHU
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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