专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

WO0158757A3 COMMUNICATIONS SYSTEM USING HIGH ALTITUDE, LONG ENDURANCE AIRCRAFT AS RELAYS 审中-公开
标题翻译：使用高海拔，长寿命航空器作为继电器的通信系统
公开(公告)号：WO0158757A3
公开(公告)日：2002-05-02
申请号：PCT/US0104624
申请日：2001-02-14
申请人： AEROVIRONMENT INC , HUGHES ELECTRONICS CORP
发明人： MACCREADY PAUL , COX EARL C , MORGAN RAY , ROSEN HAROLD , CHANG DONALD , CHANG MING , FERIA YING
IPC分类号： B64C39/00 , B64C3/42 , B64C3/52 , B64C15/02 , B64C39/02 , B64C39/10 , B64D27/24 , B64D31/06 , G05D1/00 , H04B7/185
CPC分类号： B64C3/42 , B64C3/52 , B64C15/02 , B64C39/024 , B64C39/10 , B64C2201/028 , B64C2201/042 , B64C2201/102 , B64C2201/122 , B64C2201/126 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64D27/24 , B64D31/06 , B64D2211/00 , G05D1/0022 , G05D1/0077 , H04B7/18504 , Y02T50/12 , Y02T50/145 , Y02T50/44 , Y02T50/62 , Y02T50/69
摘要： This disclosure provides a solar rechargeable aircraft (10) that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. The aircraft has a wide variety of applications as communications relay, which include serving as a long term high altitude platform that serves to link a ground station (510) using radio wave signals and a satellite using (512) optical signals.
摘要翻译：本公开提供了一种太阳能可再充电飞机（10），其生产便宜，是可操纵的，并且可以几乎无限期地保持机载。首选飞机是一个装有跨距的飞翼，没有机身或方向舵。该飞机作为通信继电器具有广泛的应用，其包括用作使用无线电波信号连接地面站（510）和使用（512）光信号的卫星的长期高空平台。

2. 发明申请

WO0158758A3 REMOTELY PILOTED AIRCRAFT 审中-公开
标题翻译：遥控飞机
公开(公告)号：WO0158758A3
公开(公告)日：2002-05-02
申请号：PCT/US0104632
申请日：2001-02-12
申请人： AEROVIRONMENT INC
发明人： MACCREADY PAUL , HIBBS BART D , COX EARL C , LISOSKI DEREK L , KENDALL GREG T
IPC分类号： B64C39/00 , B64C3/42 , B64C3/52 , B64C15/02 , B64C39/02 , B64C39/10 , B64D27/24 , B64D31/06 , G05D1/00 , H04B7/185
CPC分类号： B64C3/42 , B64C3/52 , B64C15/02 , B64C39/024 , B64C39/10 , B64C2201/028 , B64C2201/042 , B64C2201/102 , B64C2201/122 , B64C2201/126 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64D27/24 , B64D31/06 , B64D2211/00 , G05D1/0022 , G05D1/0077 , H04B7/18504 , Y02T50/12 , Y02T50/145 , Y02T50/44 , Y02T50/62 , Y02T50/69
摘要： This disclosure provides a solar rechargeable aircraft (10) that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. The aircraft can be remotely piloted through multiple, redundant communication subsystems. The availability and reliability of each separate communication subsystem is continuously monitored. The aircraft has a wide variety of applications, which include serving as a long term high altitude platform that serves to link a ground station using radio wave signals and a satellite using optical signals.
摘要翻译：本公开提供了一种太阳能可再充电飞机（10），其生产便宜，是可操纵的，并且可以几乎无限期地保持机载。首选飞机是一个装有跨距的飞翼，没有机身或方向舵。飞机可以通过多个冗余通信子系统进行远程驾驶。每个单独的通信子系统的可用性和可靠性被不断地监视。该飞机具有广泛的应用，其中包括作为长期高空平台，用于使用无线电波信号连接地面站和使用光信号的卫星。

3. 发明申请

WO0158756A9 AIRCRAFT 审中-公开
标题翻译：飞机
公开(公告)号：WO0158756A9
公开(公告)日：2002-10-31
申请号：PCT/US0104378
申请日：2001-02-07
申请人： AEROVIRONMENT INC
发明人： MACCREADY PAUL , HIBBS BART D , COX EARL C , LISOSKI DEREK L , KENDALL GREG T
IPC分类号： B64C39/00 , B64C3/42 , B64C3/52 , B64C15/02 , B64C39/02 , B64C39/10 , B64D27/24 , B64D31/06 , G05D1/00 , H04B7/185
CPC分类号： B64C3/42 , B64C3/52 , B64C15/02 , B64C39/024 , B64C39/10 , B64C2201/028 , B64C2201/042 , B64C2201/102 , B64C2201/122 , B64C2201/126 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64D27/24 , B64D31/06 , B64D2211/00 , G05D1/0022 , G05D1/0077 , H04B7/18504 , Y02T50/12 , Y02T50/145 , Y02T50/44 , Y02T50/62 , Y02T50/69
摘要： This disclosure provides a solar rechargeable aircraft (10) that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. Traveling at relatively slow speeds, and having a two-hundred foot wingspan that mounts photovoltaic cells on most all of the wing's (12) top surface (42), the aircraft uses only differential thrust of its propellers (16) to turn. Each segment of the wing has one or more motors (14) and photovoltaic arrays (32), and produces its own lift independent of the other segments, to avoid loading them. Five two-sided photovoltaic arrays, in all, are mounted on the wing, and receive photovoltaic energy both incident on top of the wing, and which is incident also from below, through a bottom, transparent surface. The aircraft includes hinges and actuators capable of providing an adjustable dihedral for the wing. The actuators can be motors or control surfaces. Alternately, the actuators can be movable masses within the wing, which may be capable of deforming the wing to alter the aerodynamics of the wing, and thereby actuate the hinges. Because of wing dihedral, the aircraft includes motors both above and below the center of drag, and the aircraft uses differential thrust to control aircraft pitch. The aircraft has a wide variety of applications, which include serving as a long term high altitude platform that serves to link a ground station using radio wave signals and a satellite using optical signals.
摘要翻译：本公开提供了一种太阳能可再充电飞机（10），其生产便宜，是可操纵的，并且可以几乎无限期地保持机载。首选飞机是一个装有跨距的飞翼，没有机身或方向舵。以相对较慢的速度行驶，并且在大部分机翼（12）顶面（42）上安装有二百英尺翼展，该飞机仅使用其推进器（16）的差动推力来转动。机翼的每个部分具有一个或多个电动机（14）和光伏阵列（32），并且独立于其它部分产生其自身的电梯，以避免装载它们。五个双面光伏阵列总体上安装在机翼上，并且接收能量入射到机翼的顶部并且从下方入射的光能通过底部的透明表面。飞机包括铰链和致动器，能够为机翼提供可调节的二面体。执行器可以是电机或控制面。或者，致动器可以是机翼内的可移动质量块，其可以使机翼变形以改变机翼的空气动力学，从而致动铰链。由于机翼二面体，飞机包括在阻力中心上方和下方的电机，飞机使用差速推力来控制飞机俯仰。该飞机具有广泛的应用，其中包括作为长期高空平台，用于使用无线电波信号连接地面站和使用光信号的卫星。

4. 发明申请

WO2004004157A3 HIGH ALTITUDE PLATFORM DEPLOYMENT SYSTEM 审中-公开
标题翻译：高海拔平台部署系统
公开(公告)号：WO2004004157A3
公开(公告)日：2004-03-25
申请号：PCT/US0312138
申请日：2003-04-17
申请人： AEROVIRONMENT INC
发明人： HIBBS BART D , COX EARL C
IPC分类号： H04B7/185
CPC分类号： H04B7/18504
摘要： A communication system for supporting communications with a target market area. The system includes one or more solar-powered aircraft maintained in, or successively passing through, flight stations or flight patterns around the market area. Each of the aircraft targets limited beamwidth communication antennas on a substantial portion of the target market area. The control system is configured to fly selective flight patterns depending on the aircraft characteristics and the flight conditions. The flight patterns may emphasize high-power-generation patterns such as flying away from the sun for aircraft with wing-mounted solar cells.
摘要翻译：支持与目标市场区域通信的通信系统。该系统包括一个或多个太阳能飞机，该飞机维持在市场区域周围的飞行站或飞行模式中，或依次通过该飞行器。每个飞机在目标市场区域的大部分目标上都有限的波束宽度通信天线。控制系统配置为根据飞机特性和飞行条件飞行选择性飞行模式。飞行模式可能会强调高功率发电模式，例如带有翼型太阳能电池的飞机从太阳飞出。

5. 发明申请

WO0158756A3 AIRCRAFT 审中-公开
标题翻译：飞机
公开(公告)号：WO0158756A3
公开(公告)日：2002-01-03
申请号：PCT/US0104378
申请日：2001-02-07
申请人： AEROVIRONMENT INC
发明人： MACCREADY PAUL , HIBBS BART D , COX EARL C , LISOSKI DEREK L , KENDALL GREG T
IPC分类号： B64C39/00 , B64C3/42 , B64C3/52 , B64C15/02 , B64C39/02 , B64C39/10 , B64D27/24 , B64D31/06 , G05D1/00 , H04B7/185
CPC分类号： B64C3/42 , B64C3/52 , B64C15/02 , B64C39/024 , B64C39/10 , B64C2201/028 , B64C2201/042 , B64C2201/102 , B64C2201/122 , B64C2201/126 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64D27/24 , B64D31/06 , B64D2211/00 , G05D1/0022 , G05D1/0077 , H04B7/18504 , Y02T50/12 , Y02T50/145 , Y02T50/44 , Y02T50/62 , Y02T50/69
摘要： This disclosure provides a solar rechargeable aircraft (10) that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. Traveling at relatively slow speeds, and having a two-hundred foot wingspan that mounts photovoltaic cells on most all of the wing's (12) top surface (42), the aircraft uses only differential thrust of its propellers (16) to turn. Each segment of the wing has one or more motors (14) and photovoltaic arrays (32), and produces its own lift independent of the other segments, to avoid loading them. Five two-sided photovoltaic arrays, in all, are mounted on the wing, and receive photovoltaic energy both incident on top of the wing, and which is incident also from below, through a bottom, transparent surface. The aircraft includes hinges and actuators capable of providing an adjustable dihedral for the wing. The actuators can be motors or control surfaces. Alternately, the actuators can be movable masses within the wing, which may be capable of deforming the wing to alter the aerodynamics of the wing, and thereby actuate the hinges. Because of wing dihedral, the aircraft includes motors both above and below the center of drag, and the aircraft uses differential thrust to control aircraft pitch. The aircraft has a wide variety of applications, which include serving as a long term high altitude platform that serves to link a ground station using radio wave signals and a satellite using optical signals.
摘要翻译：本公开提供了一种太阳能可再充电的飞机（10），其生产成本低，可操纵且可以几乎无限期地保持在空中。首选的飞机是跨越式飞行机翼，没有机身或方向舵。以相对较低的速度行驶，并且具有将光伏电池安装在大部分机翼（12）顶部表面（42）上的二百英尺翼展，飞机仅使用其推进器（16）的差动推力旋转。机翼的每个部分都有一个或多个马达（14）和光伏阵列（32），并且独立于其他部分生成自己的升力，以避免加载它们。总共五个双面光伏阵列安装在机翼上，并且接收入射在机翼顶部并且也从下面入射的光伏能量，通过底部透明表面。该飞机包括能够为机翼提供可调整的二面角的铰链和致动器。执行器可以是电机或控制面。或者，致动器可以是机翼内的可移动质量块，其可以使机翼变形以改变机翼的空气动力学，并由此致动铰链。由于机翼的二面角，该机包括在阻力中心上方和下方的电机，并且该机使用差速推力来控制飞机俯仰。该飞机有多种应用，其中包括作为一个长期的高空平台，用于连接使用无线电波信号的地面站和使用光信号的卫星。

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