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公开(公告)号：US12145712B2
公开(公告)日：2024-11-19
申请号：US18307139
申请日：2023-04-26
Applicant: Herns Louis
Inventor： Herns Louis
Abstract: The present invention relates to a high-altitude wind farm aircraft system. The aircraft has a plurality of wind turbines for capturing wind energy and converting same into electric energy which is stored in an onboard battery system. The electric energy, before storage, is stepped down by a transformer and converted into DC by an AC-DC converter. For use of the stored energy, the aircraft is brought to the ground and the batteries are removed to connect to a microgrid or any other electric circuit. The batteries can be installed again in the aircraft system for recharging with the aircraft going to high altitude for recharging the batteries. In one embodiment, the aircraft has an altitude indicator for indicating an appropriate altitude level for maximum efficiency of the system.
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公开(公告)号：US08807098B1
公开(公告)日：2014-08-19
申请号：US13713474
申请日：2012-12-13
Applicant: Herns Louis
Inventor： Herns Louis
CPC classification number: F02B75/18 , F02B73/00 , F02B75/225 , F02B75/228 , F02D19/0634 , F02D19/0647 , F02D41/0025 , F02D41/0027 , F02D2200/604 , Y02T10/36
Abstract: A twin vertical bank hybrid internal combustion H-engine system; an assembly having an engine block with parallel left side and right side vertical inline piston banks, each having a crankshaft and pistons, a cylinder head, and individual fuel feeds operable on a first and second fuel type respectively. Each piston bank operates independently of the other but is housed within the same engine block and has separate lubrication systems. An operator selects which engine to run based on fuel availability, convenience, or lower cost of a certain fuel type. The chosen engine is mechanically or electrically selected via an engine bank selector box using a selector control which selects the fuel type and engages a drive gear on the crankshaft of the selected engine, and transfers power to the transmission. The selector control actuates a transfer system that prevents simultaneous operation of both engines.
Abstract translation: 双立式立式混合内燃式H型发动机系统; 具有具有平行的左侧和右侧的垂直的在线活塞组的发动机缸体的组件，每个具有曲轴和活塞，气缸盖和分别可在第一和第二燃料类型上操作的单个燃料供给。 每个活塞组独立于另一个运行，但是容纳在相同的发动机缸体内并具有单独的润滑系统。 操作员根据燃料的可用性，方便性或某种燃料类型的较低成本来选择运行哪个发动机。 所选择的发动机通过使用选择器控制器的发动机组选择箱机械或电气选择，所述选择器控制器选择燃料类型并与所选择的发动机的曲轴上的驱动齿轮接合，并将动力传递到变速器。 选择器控制致动传动系统，防止两个发动机的同时操作。
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公开(公告)号：US20230365244A1
公开(公告)日：2023-11-16
申请号：US18307139
申请日：2023-04-26
Applicant: Herns Louis
Inventor： Herns Louis
IPC: B64B1/34 , B60L50/60 , B64D27/24 , B60L8/00 , B64D45/00 , F03D9/32 , F03D9/11 , H01M10/46 , H01M10/44 , H02K7/18
CPC classification number: B64B1/34 , B60L50/60 , B64D27/24 , B60L8/006 , B64D45/00 , F03D9/32 , F03D9/11 , H01M10/46 , H01M10/44 , H02K7/183 , B60L2200/10 , B60L2210/30 , F05B2240/92 , H01M2220/20
Abstract: The present invention relates to a high-altitude wind farm aircraft system. The aircraft has a plurality of wind turbines for capturing wind energy and converting same into electric energy which is stored in an onboard battery system. The electric energy, before storage, is stepped down by a transformer and converted into DC by an AC-DC converter. For use of the stored energy, the aircraft is brought to the ground and the batteries are removed to connect to a microgrid or any other electric circuit. The batteries can be installed again in the aircraft system for recharging with the aircraft going to high altitude for recharging the batteries. In one embodiment, the aircraft has an altitude indicator for indicating an appropriate altitude level for maximum efficiency of the system.
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