-
1.发明申请Aircraft having a jet engine, an adjustable aft nozzle, and an electric vertical fan 审中-公开具有喷气发动机，可调节后喷嘴和电动垂直风扇的飞机公开(公告)号：US20090121073A1
公开(公告)日：2009-05-14
申请号：US11396969
申请日：2006-04-03
申请人： Paul M. Doane , Thomas W. Omohundro
发明人： Paul M. Doane , Thomas W. Omohundro
CPC分类号： B64C29/0025 , B64C29/0066 , B64D27/24 , Y02T50/62
摘要： An adjustable nozzle is mounted on the airframe downstream from the powerplant for selectively directing powerplant exhaust to exit the aircraft at an angle between about rearward and downward. An electricity source mounted on the airframe powers a magnetically driven fan positioned in front of the powerplant in the fuselage.
摘要翻译： 可动喷嘴安装在动力装置下游的机身上，用于选择性地引导动力装置排气以大约向后和向下的角度离开飞行器。 安装在机身上的电源为位于机身前方的动力装置前面的磁力驱动的风扇供电。
-
公开(公告)号：US20120181856A1
公开(公告)日：2012-07-19
申请号：US13428768
申请日：2012-03-23
IPC分类号： B60L1/00
CPC分类号： B60L7/14 , H02J7/1438 , H02J7/34
摘要： An actuator control system includes a controller and a buck-boost circuit. The controller is configured to direct power from a power source to an actuator. The actuator is coupled to a control device to apply a force related to operation of a vehicle. The buck-boost circuit is configured to direct excess power generated by the actuator to an energy storage device when an actuator power level satisfies an anticipated power level.
摘要翻译： 致动器控制系统包括控制器和降压 - 升压电路。 控制器被配置为将电力从电源引导到致动器。 致动器联接到控制装置以施加与车辆的操作相关的力。 降压 - 升压电路被配置为当致动器功率电平满足预期功率电平时，将由致动器产生的过剩功率引导到能量存储装置。
-
公开(公告)号：US08164283B2
公开(公告)日：2012-04-24
申请号：US12264488
申请日：2008-11-04
IPC分类号： H02P3/14
CPC分类号： B60L7/14 , H02J7/1438 , H02J7/34
摘要： Systems and methods are provided for capturing and using power generated by the application of an external force or by an inertial force on a vehicle control device that back-drive or forward-drive an actuator coupled to the control device. An actuator is coupled to a control device configured to apply a force related to operation of a vehicle. A bus is configured to conduct power to the actuator. An actuator control system is configured to receive power from a power source via an electrical bus and direct the power to the actuator. The actuator control system is also configured to monitor an actuator power level to determine when the actuator power level does not meet an anticipated power level. When the actuator power level exceeds the anticipated power level, the excess power generated is directed to an energy storage device. When the actuator power level is less than the anticipated power level, supplemental power is distributed from the energy storage device to the bus.
摘要翻译： 提供了系统和方法，用于捕获和使用通过施加外力或通过惯性力而产生的电力，该车辆控制装置用于后驱动或前向驱动耦合到控制装置的致动器。 致动器联接到被配置为施加与车辆的操作相关的力的控制装置。 总线被配置为向致动器供电。 致动器控制系统被配置为经由电总线从电源接收电力并将电力引导到致动器。 致动器控制系统还被配置为监视致动器功率水平以确定致动器功率水平何时不满足预期的功率水平。 当致动器功率级别超过预期功率水平时，产生的多余功率被引导到储能装置。 当执行器功率水平低于预期功率水平时，补充功率从能量存储装置分配到总线。
-
公开(公告)号：US08614555B2
公开(公告)日：2013-12-24
申请号：US13428768
申请日：2012-03-23
IPC分类号： H02P3/14
CPC分类号： B60L7/14 , H02J7/1438 , H02J7/34
摘要： An actuator control system includes a controller and a buck-boost circuit. The controller is configured to direct power from a power source to an actuator. The actuator is coupled to a control device to apply a force related to operation of a vehicle. The buck-boost circuit is configured to direct excess power generated by the actuator to an energy storage device when an actuator power level satisfies an anticipated power level.
摘要翻译： 致动器控制系统包括控制器和降压 - 升压电路。 控制器被配置为将电力从电源引导到致动器。 致动器联接到控制装置以施加与车辆的操作相关的力。 降压 - 升压电路被配置为当致动器功率电平满足预期功率电平时，将由致动器产生的过剩功率引导到能量存储装置。
-
公开(公告)号：US20100109581A1
公开(公告)日：2010-05-06
申请号：US12264488
申请日：2008-11-04
CPC分类号： B60L7/14 , H02J7/1438 , H02J7/34
摘要： Systems and methods are provided for capturing and using power generated by the application of an external force or by an inertial force on a vehicle control device that back-drive or forward-drive an actuator coupled to the control device. An actuator is coupled to a control device configured to apply a force related to operation of a vehicle. A bus is configured to conduct power to the actuator. An actuator control system is configured to receive power from a power source via an electrical bus and direct the power to the actuator. The actuator control system is also configured to monitor an actuator power level to determine when the actuator power level does not meet an anticipated power level. When the actuator power level exceeds the anticipated power level, the excess power generated is directed to an energy storage device. When the actuator power level is less than the anticipated power level, supplemental power is distributed from the energy storage device to the bus.
摘要翻译： 提供了系统和方法，用于捕获和使用通过施加外力或通过惯性力而产生的电力，该车辆控制装置用于后驱动或前向驱动耦合到控制装置的致动器。 致动器联接到被配置为施加与车辆的操作相关的力的控制装置。 总线被配置为向致动器供电。 致动器控制系统被配置为经由电总线从电源接收电力并将电力引导到致动器。 致动器控制系统还被配置为监视致动器功率水平以确定致动器功率水平何时不满足预期的功率水平。 当致动器功率级别超过预期功率水平时，产生的多余功率被引导到储能装置。 当执行器功率水平低于预期功率水平时，补充功率从能量存储装置分配到总线。
-
6.发明授权Airframe mounted accessory drive (AMAD) power take-off shaft auxiliary power generation 失效机身安装附件驱动（AMAD）动力输出轴辅助发电公开(公告)号：US06840479B1
公开(公告)日：2005-01-11
申请号：US10728634
申请日：2003-12-05
IPC分类号： B64D41/00
CPC分类号： B64D41/00
摘要： In an aircraft having an engine and an AMAD, a power take off shaft is rotationally connected to the engine, and the power take off shaft provides rotational power from the engine. A power producing device having an internal shaft is provided for producing additional auxiliary power. The power producing device may be an electrical generator with an internal shaft rotationally connected to the power take off shaft. The electrical generator converts one portion of the rotational power to additional electrical power, and fits in a pre-existing unused space within the aircraft, located between the engine and the AMAD. An output shaft is rotationally connected to the power take off shaft and rotationally connects to the AMAD to provide another portion of the rotational power to the AMAD. Additional electrical power generation is produced without modification to the engine, AMAD, or existing electrical generators.
摘要翻译： 在具有发动机和AMAD的飞行器中，动力输出轴旋转地连接到发动机，动力输出轴提供来自发动机的旋转动力。 提供具有内部轴的动力产生装置，用于产生额外的辅助动力。 发电装置可以是具有与动力输出轴旋转地连接的内部轴的发电机。 发电机将旋转功率的一部分转换成额外的电力，并且装配在位于发动机和AMAD之间的飞机内的预先存在的未使用空间中。 输出轴旋转地连接到动力输出轴并且旋转地连接到AMAD，以向AMAD提供另一部分旋转动力。 在不修改发动机，AMAD或现有发电机的情况下生产额外的发电。
-
-
-
-
-
搜索结果
6 条记录 (耗时 0.02 秒)
