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1. 发明公开

US20230264823A1 Charging System for Aircraft and Drones 审中-公开
公开(公告)号：US20230264823A1
公开(公告)日：2023-08-24
申请号：US17678810
申请日：2022-02-23
申请人： Elijah Abron
发明人： Elijah Abron
IPC分类号： B64D27/24 , B64D41/00
CPC分类号： B64D27/24 , B64D41/007 , H02J7/14
摘要： An auxiliary charging system comprising of: a recovering system for capturing kinetic energy from a propeller exhausted air; and at least two sets of propellers, one set of propellers is located on the electric motor, and the other set of propellers is situated on an alternator or the generator unit is in this process; the alternator can be located in the front or behind of an aircraft electric motor or aircraft wing or vice versa (Anywhere on the aircraft) for recharging batteries and supplying power back to the propeller electric motor that is powering the aircraft; the propeller electric motor and the alternator propeller is a non-connected systems. The exhausted kinetic energy air from the alternator propeller captures kinetic energy air from the propeller electric motor; this kinetic energy adds motion to the propeller driveshaft of the alternator. The propellers are arranged to transform this oscillating motion energy from one propeller to the next, propeller producing regenerated air energy from the oscillating movement of the kinetic energy air body into a mechanical motion.

2. 发明公开

US20230264585A1 Charging System for Electrical Vehicles 审中-公开
公开(公告)号：US20230264585A1
公开(公告)日：2023-08-24
申请号：US17676177
申请日：2022-02-20
申请人： Elijah Abron
发明人： Elijah Abron
IPC分类号： B60L53/52 , B60L53/20 , B60L58/10 , B60K7/00 , B60L8/00
CPC分类号： B60L53/52 , B60K7/0007 , B60L8/006 , B60L53/20 , B60L58/10 , B60L2200/32
摘要： Air power auxiliary alternators comprising a recovering system for capturing moving kinetic air energy, Using alternators for charging the batteries and supplying power to the electrical system, plus other vehicle components and the automobile’s motor. The charging system has a voltage regulator unit and a power control inverter. Giving power back to the auxiliary drive motor that electrically powers the battery and the drive process. The system is a non-contact powering unit that uses not take away from the vehicle’s electrical system the kinetic energy air from a moving vehicle. Multiple alternators force air into the pelonis intake, which is mounted in the front of the vehicle and arranged to transform this air into a rotating motion and charge the ion battery. This energy of the rotating movement of the kinetic energy action to electrical energy power for E.V. vehicles or trucks with trailers, an. This auxiliary electric trailer motor is connected to the trailer’s rear wheels, and a controller controls the motor with electrical power and torque to drive the trailer.

3. 发明申请

US20210341128A1 Control Drone Lighting Device 有权
公开(公告)号：US20210341128A1
公开(公告)日：2021-11-04
申请号：US17302134
申请日：2021-04-25
申请人： Elijah Abron
发明人： Elijah Abron
IPC分类号： F21S43/14 , B64C39/02 , F21S43/15 , F21S41/153 , F21S45/43
摘要： A control Spot lights and display drone, which has an auxiliary generator or battery to supply power for a combination of voltage, for lighting LED spot light and other auxiliary equipment and powering the drones, a wire tethering device that can move in conjunction with the drone; the drone lighting also can change colors to create a flashing lights effect (as a like police cars flashing lights). The remote LED spotlight controller is for changing colors of the LED lights for outside party lights or blinking lights; or just bright white lights, a voltage reducer that's piggyback off the power wires; a battery or a generator for supplying power to power the drone body internal and external components such as a display and lights; a mounting bracket for mount the LED spot lights; a LED spot lights mounting bracket that has at least two holes for mounting LED spot lights to bracket; a voltage reducer; whereby the allowing the drone or drones to fly for a longer period of time, also longer illumination and illustrating time in the air; also, the use of solar cells to aid in powering the drones;

4. 发明申请

US20220250763A1 Charging Wing System for Aircraft 有权
公开(公告)号：US20220250763A1
公开(公告)日：2022-08-11
申请号：US17714573
申请日：2022-04-06
申请人： Elijah Abron
发明人： Elijah Abron
IPC分类号： B64D41/00 , F03D9/32 , F03D3/04 , F03D9/25
摘要： A kinetic energy charging wing system comprising of: an energy recovery system for capturing kinetic air energy that is passing over the surface of an aircraft wing or the surface of a drone aircraft or other transport; the passing air is causing the swirl cage wheel blades shaft to rotate and also turning an alternator or a generator unit driveshaft; this kinetic energy system which transfers kinetic energy from air into mechanical energy from air passing over the surface of the aircraft and the atmosphere are being captured by swirl cage wheel blades; the system incorporates at least one swirl cage wheel unit and one alternator or generator unit that connected to a swirl cage wheel unit with a housing for the swirl cage wheel blades. This process supports the aircraft electrical system of aircraft of today and tomorrow, the system is coupled to the aircraft speed control module with a function for starting and stopping the charging system, the alternator or alternators that install within the body of an aircraft wing and run-on air pressure to start the rotating the swirl cage wheel blades also turning the charging unit to start creating electrical from the kinetic air energy, this electrical power joins to the aircraft's electrical system, and this converted electrical energy is in the Lithium-ion batteries storage bank process provides electrical energy that created from kinetic air energy that passes over an aircraft's surface and stores this electrical potential energy.

5. 发明授权

US07037564B1 Substrate sheets with removable strip 失效
标题翻译：带可移动条的底板
公开(公告)号：US07037564B1
公开(公告)日：2006-05-02
申请号：US10413672
申请日：2003-04-15
申请人： Elijah Abron
发明人： Elijah Abron
IPC分类号： B32B3/02
CPC分类号： B42D5/003 , B42C9/0081 , B42D5/00 , C09J7/20 , Y10T428/14 , Y10T428/1452 , Y10T428/1457 , Y10T428/1462 , Y10T428/1476 , Y10T428/1486 , Y10T428/15 , Y10T428/24777
摘要： A composite assembly for assembling documents and including a substrate sheet, and adhesive layer, and a release liner disposed over the adhesive layer. To assemble a document, the pages of the document are printed on the substrate sheets, the substrate sheets are ordered and aligned, the release liners are removed by the a portion of the release liner overlaying a removed tab being grasped and pulled to peel the release liners from the adhesive layers, and the pages are bonded together by pressure.
摘要翻译：一种用于组装文件并包括基片和粘合剂层的复合组件，以及设置在粘合剂层上的剥离衬垫。为了组装文件，将文件的页面印刷在基材片上，对基材片进行排序和排列，将剥离衬垫的一部分移除，将剥离衬垫重叠在被抓取并拉出的剥离的突片上以剥离释放来自粘合剂层的衬垫和页面通过压力粘合在一起。

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