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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：US11565793B2
公开(公告)日：2023-01-31
申请号：US17234070
申请日：2021-04-19
申请人： Xiaoyi Zhu
发明人： Xiaoyi Zhu
摘要： The invention discloses a propeller-driven helicopter or airplane which comprises a fuselage and a propeller comprising a plurality of blades, wherein a plurality of pressure pipes are uniformly distributed between windward sides and leeward sides of the blades; a plurality of first inlets are formed in the windward sides and are communicated with outside via first channels in the blades and second outlets at tails of the blades; a high-pressure fluid of a low-speed fluid layer formed when a fluid flows through the leeward sides in a widthwise direction flows towards a low-pressure fluid of a high-speed fluid layer formed when the fluid flows through the first inlets, the first channels and the second outlets; and an upward pressure generated by the high-pressure fluid is opposite to a downward pressure generated by an external fluid above the windward sides, so that a fluid pressure above the propeller is decreased.
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公开(公告)号：US11098642B2
公开(公告)日：2021-08-24
申请号：US15800394
申请日：2017-11-01
申请人： Xiaoyi Zhu
发明人： Xiaoyi Zhu
摘要： A fluid supercharging device, comprising: a rotating shaft; a vane disc coaxially fixed to the rotating shaft; a plurality of fan blades fixed around a perimeter of the vane disc; the back side of the fan blades being provided with at least one fluid guiding inlet, an end of the back side distal from the vane disc is provided with a fluid guiding outlet, a fluid channel communicating the fluid guiding inlet with the fluid guiding outlet is provided along a lengthwise direction inside the fan blades; the fan blades 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：US10464544B2
公开(公告)日：2019-11-05
申请号：US15254613
申请日：2016-09-01
申请人： Xiaoyi Zhu
发明人： Xiaoyi Zhu
摘要： Provided are embodiments of a suspension train comprising a shell body, wheels and a flow disturbing plate connected with the wheels, a suspension train operating system comprising a non-vacuum cover body and the suspension train traveling in the cover body in an ideal vacuum state at high speeds, and first and second propelling force sources converted from fluid resistance for multiplying propelling force of the train. A fluid channel communicating with the outside is formed between the upper surface of the flow disturbing plate with the lower surface being a concave-convex flow disturbing surface and the bottom of the shell body. The high-speed suspension train is completely driven by solar energy.
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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：US09745047B2
公开(公告)日：2017-08-29
申请号：US14295350
申请日：2014-06-04
申请人： Xiaoyi Zhu
发明人： Xiaoyi Zhu
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：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：US20140345295A1
公开(公告)日：2014-11-27
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.
摘要翻译： 一种流体增压装置（3,5），包括：旋转轴（7）; 同轴地固定在旋转轴（7）上的叶片盘（308）; 围绕所述叶片盘周边固定的多个风扇叶片（301）; 风扇叶片301的后侧设置有至少一个流体引导入口（305），远离叶片盘（308）的后侧的端部设置有流体引导出口（306,307），流体 在所述风扇叶片的内部沿长度方向设置将所述流体引导入口（305）与所述流体引导出口（306,307）连通的通道（304） 风扇叶片（301）旋转以产生离心力，使得流体经由背侧的流体引导入口流入流体通道，并且沿着风扇叶片的长度方向流出流体引导出口。
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公开(公告)号：US20110075612A1
公开(公告)日：2011-03-31
申请号：US12569734
申请日：2009-09-29
申请人： JIMING GUO , William Y. Huang , Michael M. Fan , Xiaoyi Zhu , Matthew S. Grob
发明人： JIMING GUO , William Y. Huang , Michael M. Fan , Xiaoyi Zhu , Matthew S. Grob
IPC分类号： H04W8/00
CPC分类号： H04L12/189 , H04H60/80 , H04L67/26 , H04W4/06 , H04W68/00
摘要： A method, apparatus, and system for providing ad hoc venue-cast content to a plurality of receiving access terminals within a venue boundary. Ad hoc content may be generated at an access terminal, transmitted to a venue-cast server, and broadcast to a plurality of venue-cast receiving access terminals within a venue. In addition to broadcasting the ad hoc content, a notification is given to the plurality of receiving access terminals, notifying them regarding the availability of the ad hoc content.
摘要翻译： 一种用于向场地边界内的多个接收接入终端提供临时场地播放内容的方法，装置和系统。 Ad hoc内容可以在接入终端生成，发送到场所播送服务器，并且广播到场地内的多个场所播送接收接入终端。 除了广播自组织内容之外，还向多个接收接入终端通知通知他们有关特设内容的可用性。
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公开(公告)号：US20110001000A1
公开(公告)日：2011-01-06
申请号：US12699066
申请日：2010-02-03
申请人： Xiaoyi Zhu
发明人： Xiaoyi Zhu
CPC分类号： B64C39/001 , B64C3/141 , B64C39/00 , B64C39/026 , Y02T50/12
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.
摘要翻译： 本发明公开了一种从其内部产生更大升力的飞机。 飞机内的流体通道与发动机和外壳上表面上的端口相通。 通过发动机的强力吸力，外壳上表面的流体在长路径，大面积，高速和低气压的条件下通过相应的端口快速地吸入流体通道，从而导致从 飞机的内部。 在产生电梯的过程中，流体壁和流体孔的流体阻力通过飞机前部和周围区域的端口被吸入流体通道，然后高速流体从后端口 。 这种方式对现有飞机的转型作出了重大贡献。 统一的大翼机能够显着改善现有飞机降低能耗的电梯，速度和承载能力。
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