专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

21. 外观设计

USD978768S1 Aircraft airframe 有权
公开(公告)号：USD978768S1
公开(公告)日：2023-02-21
申请号：US29779140
申请日：2021-05-13
申请人： Alakai Technologies Corporation
设计人： Brian D. Morrison , Andre H. De Salis , Martti J. Lampela , Adil M. Ali , Peter F. Falt

22. 发明申请

US20220135228A1 MULTIFUNCTION DYNAMIC VISUAL DISPLAY FOR INTERACTIVE USER EXPERIENCE 有权
公开(公告)号：US20220135228A1
公开(公告)日：2022-05-05
申请号：US17512148
申请日：2021-10-27
申请人： Alakai Technologies Corporation
发明人： Brian D. Morrison , Peter F. Falt
IPC分类号： B64D11/00 , H04L12/40 , G05D1/06
摘要： An integrated multifunction dynamic display system and method for an air vehicle that provides an interactive user experience. The system is based around an array of multifunction display nodes that are disposed throughout the air vehicle. The multifunction display nodes are connected through a databus or network such that the display nodes can operate individually or in combination to create a desired interactive experience. The nodes can include interior lighting, exterior lighting, interior displays, exterior displays, and windows. The multifunction dynamic display system can be used to control or otherwise provide interior lighting or displays, loading/unloading instruction, inflight entertainment or information, emergency notification and instruction, augmented reality, external lighting and displays. In addition, the multifunction dynamic display can be configured for each passenger.

23. 发明申请

US20210394914A1 METHOD OF OPERATING A LIGHTWEIGHT HIGH POWER DENSITY FAULT-TOLERANT FUEL CELL SYSTEM FOR CLEAN FUEL ELECTRIC AIRCRAFT 有权
公开(公告)号：US20210394914A1
公开(公告)日：2021-12-23
申请号：US17232611
申请日：2021-04-16
申请人： Alakai Technologies Corporation
发明人： Brian D. Morrison
IPC分类号： B64D27/24 , H01M8/04029 , H01M8/04007 , H01M8/2457 , B60L58/32 , H01M8/04858
摘要： A lightweight, high power density, fault-tolerant fuel cell system, method, and apparatus for full-scale clean fuel electric-powered aircraft having a fuel cell module including a plurality of fuel cells working together to process gaseous oxygen from air compressed by turbochargers, superchargers, blowers or local oxygen supply and gaseous hydrogen from liquid hydrogen transformed by heat exchangers, with an electrical circuit configured to collect electrons from the plurality of hydrogen fuel cells to supply voltage and current to motor controllers commanded by autopilot control units configured to select and control an amount and distribution of electrical voltage and torque or current for each of the plurality of motor and propeller assemblies, wherein electrons returning from the electrical circuit combine with oxygen in the compressed air to form oxygen ions, then the protons combine with oxygen ions to form H2O molecules and heat.

24. 外观设计

USD926665S1 Set of aircraft canards 有权
公开(公告)号：USD926665S1
公开(公告)日：2021-08-03
申请号：US29692499
申请日：2019-05-24
申请人： Alakai Technologies Corporation
设计人： Brian D. Morrison , Andre H. De Salis , Martti J. Lampela , Adil M. Ali , Peter F. Falt

25. 发明申请

US20210229822A1 LIGHTWEIGHT HIGH POWER DENSITY FAULT-TOLERANT FUEL CELL SYSTEM AND APPARATUS FOR CLEAN FUEL ELECTRIC AIRCRAFT 有权
公开(公告)号：US20210229822A1
公开(公告)日：2021-07-29
申请号：US17232556
申请日：2021-04-16
申请人： Alakai Technologies Corporation
发明人： Brian D. Morrison
IPC分类号： B64D27/24 , H01M8/04029 , H01M8/04007 , H01M8/2457 , B60L58/32 , H01M8/04858
摘要： A lightweight, high power density, fault-tolerant fuel cell system, method, and apparatus for full-scale clean fuel electric-powered aircraft having a fuel cell module including a plurality of fuel cells working together to process gaseous oxygen from air compressed by turbochargers, superchargers, blowers or local oxygen supply and gaseous hydrogen from liquid hydrogen transformed by heat exchangers, with an electrical circuit configured to collect electrons from the plurality of hydrogen fuel cells to supply voltage and current to motor controllers commanded by autopilot control units configured to select and control an amount and distribution of electrical voltage and torque or current for each of the plurality of motor and propeller assemblies, wherein electrons returning from the electrical circuit combine with oxygen in the compressed air to form oxygen ions, then the protons combine with oxygen ions to form H2O molecules and heat.

26. 外观设计

USD895337S1 Aircraft seat headrest 有权
公开(公告)号：USD895337S1
公开(公告)日：2020-09-08
申请号：US29692517
申请日：2019-05-24
申请人： Alakai Technologies Corporation
设计人： Brian D. Morrison , Andre H. De Salis , Martti J. Lampela , Adil M. Ali , Peter F. Falt , Fazzio Youn

27. 外观设计

USD894621S1 Aircraft seat 有权
公开(公告)号：USD894621S1
公开(公告)日：2020-09-01
申请号：US29692494
申请日：2019-05-24
申请人： Alakai Technologies Corporation
设计人： Brian D. Morrison , Andre H. De Salis , Martti J. Lampela , Adil M. Ali , Peter F. Falt , Fazzio Youn

28. 发明申请

US20190329868A1 CLEAN FUEL ELECTRIC AIRCRAFT FOR PERSONAL AIR TRANSPORTATION AND MANNED OR UNMANNED OPERATION 审中-公开
公开(公告)号：US20190329868A1
公开(公告)日：2019-10-31
申请号：US16504874
申请日：2019-07-08
申请人： Alakai Technologies Corporation
发明人： Brian D. Morrison
IPC分类号： B64C13/18 , G01C23/00 , G05D1/00 , B64C27/08 , B64D27/24
摘要： Methods and systems for a clean fuel, manned or unmanned aircraft, having an electric, low-emission or zero-emission lift and propulsion system, an integrated ‘highway in the sky’ avionics system for navigation and guidance, a tablet-based motion command, or mission planning system to provide the operator with drive-by-wire style direction control, and automatic on-board-capability to provide traffic awareness, weather display and collision avoidance. Automatic computer monitoring by a programmed multiple-redundant autopilot control units control each motor-controller and motor to produce pitch, bank, yaw and elevation, while simultaneously restricting the flight regime that the pilot can command, to protect the pilot from inadvertent potentially harmful acts that might lead to loss of control or loss of vehicle stability. By using the results of the state measurements to inform motor control commands, the methods and systems contribute to the operational simplicity, reliability and safety of the vehicle.

29. 发明授权

US09242728B2 All-electric multirotor full-scale aircraft for commuting, personal transportation, and security/surveillance 有权
标题翻译：全电动多转子全尺寸飞机用于通勤，个人运输和安全/监控
公开(公告)号：US09242728B2
公开(公告)日：2016-01-26
申请号：US14452245
申请日：2014-08-05
申请人： Alakai Technologies Corporation
发明人： Brian D. Morrison
IPC分类号： G05D1/00 , B64C27/08 , B64C27/32
CPC分类号： B64C27/08 , B64C27/32 , B64C27/56 , B64C27/57 , B64D27/24 , B64D31/04 , B64D31/06 , B64D43/00 , G01C23/005 , Y02T50/54 , Y02T50/62
摘要： Methods and systems for a full-scale vertical takeoff and landing manned or unmanned electric aircraft, having an all-electric, non-hydrocarbon-powered lift and propulsion system, an integrated avionics system for navigation and guidance, and simple joystick and throttle controls to provide the operator with ‘drive by wire’ style direction control. The vehicle employs counter-rotating sets of propellers and lift is provided by multiple pairs of small electric motors driving directly-connected, counter-rotating sets of propellers. Automatic computer monitoring by one or a plurality of programmed redundant digital motor management computer or autopilot controls each motor-controller and motor to produce pitch, bank and elevation, while simultaneously restricting the flight regime that the pilot can command. Sensed multi-axis information and parameter values about vehicle state are used to provide stable vehicle control and to detect when stable vehicle operating limits are about to be exceeded.
摘要翻译：具有全电动，非碳氢化合物驱动的电梯和推进系统的全尺寸垂直起飞和着陆载人或无人电动飞机的方法和系统，用于导航和引导的集成航空电子系统，以及简单的操纵杆和节气门控制为操作员提供“通过线驱动”式方向控制。车辆采用反旋转螺旋桨组，升降机由多对小型电动马达提供，这些小型电动机驱动直接连接，反向旋转的螺旋桨组。由一个或多个编程的冗余数字电机管理计算机或自动驾驶仪进行的自动计算机监视控制每个电动机控制器和电动机以产生音高，组合和高程，同时限制驾驶员可以指挥的飞行状态。用于检测车辆状态的多轴信息和参数值用于提供稳定的车辆控制，并检测何时将要超出稳定的车辆运行极限。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式