-
公开(公告)号：EP2331353A1
公开(公告)日：2011-06-15
申请号：EP09835366.7
申请日：2009-09-23
申请人： Aerovironment inc.
IPC分类号： B60H1/00
CPC分类号： F02B43/00 , F01P2050/20 , F01P2060/02 , F01P2060/10 , F02B29/0412 , F02B29/0493 , F02C6/12 , F02C7/143 , F02C7/16 , F02C7/224 , F02M31/02 , F02M31/16 , F02M31/20 , F05D2260/205 , Y02T10/126 , Y02T10/146 , Y02T50/675
摘要： A high-altitude aircraft powerplant including an engine, a two-stage turbocharger having an intercooler and an aftercooler, a cryogenic hydrogen fuel source, and a cooling system including a hydrogen heat exchanger. Aided by a ram-air cooler that cools a coolant to a near-ambient temperature, the heat exchanger is configured to heat the hydrogen using the coolant, and to cool the coolant to a temperature well below the ambient temperature during high-altitude flight. The intercooler and aftercooler use the sub-ambient temperature coolant, as does a separate sensor. The ram-air cooler includes a front portion and a rear portion. The cooling system includes three cooling loops which respectively incorporate only the front portion, only the rear portion, and both portions of the ram-air cooler.
-
公开(公告)号：EP2328772A1
公开(公告)日：2011-06-08
申请号：EP09818085.4
申请日：2009-09-23
申请人： Aerovironment inc.
IPC分类号： B60K6/00
CPC分类号： F02B37/12 , B60W2710/0644 , B60Y2400/435 , F01N3/20 , F01N9/00 , F02B29/0412 , F02B33/40 , F02B37/013 , F02B37/18 , F02B37/20 , F02B43/10 , F02B73/00 , F02C7/26 , F02D19/024 , F02D29/06 , F02D41/0007 , F02D41/0025 , F02D41/065 , F02D41/083 , F02D41/1446 , F02M21/0206 , Y02T10/144 , Y02T10/146 , Y02T10/32
摘要： A hydrogen fueled powerplant including an internal combustion engine that drives a motor-generator, and has a two-stage turbocharger, for an aircraft. A control system controls the operation of the motor-generator to maintain the engine at a speed selected based on controlling the engine equivalence ratio. The control system controls an afterburner, an intercooler and an aftercooler to maximize powerplant efficiency. The afterburner also adds power to the turbochargers during high-altitude restarts. The turbochargers also include motor-generators that extract excess power from the exhaust.
-
公开(公告)号：EP1820153A4
公开(公告)日：2010-07-07
申请号：EP05824969
申请日：2005-10-25
申请人： AEROVIRONMENT INC
IPC分类号： G06Q10/00
CPC分类号： B60L11/185 , B60L3/12 , B60L11/1816 , B60L11/1822 , B60L11/1838 , B60L11/1846 , B60L11/1861 , B60L11/1887 , B60L2230/16 , B60L2260/32 , B60L2260/54 , G06Q10/087 , Y02T10/7044 , Y02T10/705 , Y02T10/7088 , Y02T90/121 , Y02T90/124 , Y02T90/128 , Y02T90/14 , Y02T90/163 , Y02T90/169 , Y02T90/34 , Y04S30/14
-
公开(公告)号：EP1831677A4
公开(公告)日：2009-09-02
申请号：EP05815358
申请日：2005-10-25
申请人： AEROVIRONMENT INC
CPC分类号： B60L3/12 , B60L11/1809 , B60L11/1816 , B60L11/1822 , B60L11/1838 , B60L11/1846 , B60L11/185 , B60L11/1861 , B60L11/1887 , B60L2200/10 , B60L2200/12 , B60L2200/26 , B60L2200/32 , B60L2200/42 , B60L2200/44 , B60L2230/16 , B60L2260/32 , H01M10/4207 , H01M10/482 , H04L67/12 , H04L67/303 , H04L67/306 , Y02P90/60 , Y02T10/7011 , Y02T10/7016 , Y02T10/7044 , Y02T10/705 , Y02T10/7088 , Y02T90/121 , Y02T90/124 , Y02T90/128 , Y02T90/14 , Y02T90/163 , Y02T90/169 , Y02T90/34 , Y04S30/14
摘要： Reactive replenishable device management comprises receiving device measurement data from at least one device, updating one or more device usage profiles associated with the at least one device, and if an analysis of the one or more device usage profiles indicates usage of the least one device is sub-optimal, performing one or more of: controlling at least one of an attribute or an operation of the at least one device, issuing one or more device management recommendations to a user of the at least one device, and issuing one or more user alerts to the user. The at least one device comprises at least one of one or more replenishable devices, one or more replenishers associated with the one or more replenishable devices, and one or more other devices associated with the one or more replenishable devices.
-
公开(公告)号：EP1820153A2
公开(公告)日：2007-08-22
申请号：EP05824969.9
申请日：2005-10-25
申请人： Aerovironment inc.
IPC分类号： G06Q99/00
CPC分类号： B60L11/185 , B60L3/12 , B60L11/1816 , B60L11/1822 , B60L11/1838 , B60L11/1846 , B60L11/1861 , B60L11/1887 , B60L2230/16 , B60L2260/32 , B60L2260/54 , G06Q10/087 , Y02T10/7044 , Y02T10/705 , Y02T10/7088 , Y02T90/121 , Y02T90/124 , Y02T90/128 , Y02T90/14 , Y02T90/163 , Y02T90/169 , Y02T90/34 , Y04S30/14
摘要： Replenishable device asset management comprises accumulating device usage information for fleet assets comprising a plurality of replenishable devices and vehicles associated with the replenishable devices, storing the device usage information for the fleet assets in a global memory, and using the device usage information to manage the fleet assets.
摘要翻译： 可补充设备资产管理包括累积用于车队资产的设备使用信息，所述车队资产包括与可补充设备相关联的多个可补充设备和车辆，将车队资产的设备使用信息存储在全局存储器中，以及使用设备使用信息来管理车队 资产。
-
公开(公告)号：EP0843822B1
公开(公告)日：2005-11-30
申请号：EP96930301.5
申请日：1996-07-29
申请人： Aerovironment inc.
CPC分类号： H02M3/285 , B60R16/03 , G01R31/006 , G01R31/2841 , G01R31/34 , G01R31/3631 , H02M2001/008
摘要： A system and mehtod for cycling loads and sources can be connected to one or more loads and sources to controllable supply or absorb current with respect thereto. For example, DC voltages can be controllably supplied to each load from a DC bus using a plurality of DC-DC converters. Various DC converter configurations are available including independent, parallel and differential, to expand the types of simulations which can be performed on the load(s).
-
公开(公告)号：EP1364872A2
公开(公告)日：2003-11-26
申请号：EP03012874.8
申请日：2001-02-07
申请人： Aerovironment Inc.
CPC分类号： B64D27/24 , B64C15/02 , B64C39/10 , B64D31/06 , B64D2211/00 , G05D1/0808 , Y02T50/12 , Y02T50/55 , Y02T50/62
摘要： An aircraft (10) has a plurality of motors (14) mounted on its wing (12), the wing being configured to produce a dihedral during flight, wherein the dihedral causes at least one of the motors (14) to produce thrust above the center of drag (202) and at least one motor (14) to produce thrust below the center of drag (202), such that control of the relative thrusts can control the pitch of the aircraft (10).
摘要翻译： 飞机（10）具有安装在其翼（12）上的多个马达（14），所述机翼构造成在飞行期间产生二面体，其中所述二面体使所述马达（14）中的至少一个在所述马达 阻力中心（202）和至少一个马达（14），以产生在牵引中心（202）下方的推力，使得相对推力的控制可以控制飞行器（10）的俯仰。
-
98.发明公开COMMUNICATIONS SYSTEM WITH SUBORBITAL PLATFORM CARRYING A COMMUNICATION DEVICE 审中-公开随着通信设备的通信系统所穿亚轨道BODY
公开(公告)号：EP1352486A2
公开(公告)日：2003-10-15
申请号：EP01923249.5
申请日：2001-04-10
申请人： Aerovironment Inc.
发明人： COX, Earl , MORGAN, Walter Ray
IPC分类号： H04B7/185
CPC分类号： H04B7/18508 , H04B7/18504
摘要： This disclosure provides a communications system using a span-loaded flying wing, traveling at relatively slow speeds, that can remain airborne for long periods of time. The communications system uses the airplane as a long term high altitude platform that can serve at least one of a number of potential functions. One function is to link to a ground station using radio wave signals and a satellite using optical signals. Another function is to serve as a relay station between ground communication nodes and individual end-users. Because the aircraft can tightly hold a station, the end-user's antennas do not need to be continuously adjustable. For such a system, a large number of aircraft can be used, with the end-user antennas being configured for a narrow beamwidth so as to allow frequency reuse for different communication links.
-
公开(公告)号：EP1280700A2
公开(公告)日：2003-02-05
申请号：EP01954575.5
申请日：2001-04-03
申请人： Aerovironment Inc.
CPC分类号： B64D27/24 , B64C1/26 , B64C3/10 , B64C3/14 , B64C9/24 , B64C39/024 , B64C39/10 , B64C2201/021 , B64C2201/028 , B64C2201/042 , B64C2201/086 , B64C2201/104 , B64C2201/122 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/187 , B64D27/02 , B64D37/30 , B64D2041/005 , Y02T50/12 , Y02T50/32 , Y02T50/44 , Y02T50/64 , Y02T90/36
摘要： Disclosed is an aircraft (101), configured to have a wide range of flight speeds, consuming low levels of power for an extended period of time, while supporting a communications platform with an unobstructed downward-looking view. The aircraft (101) includes an extendable slat (205) at the leading edge of the wing (103), and a reflexed trailing edge. The aircraft comprises a flying wing (103) extending laterally between two ends and a center point. The wing (103) is swept and has a relatively constant chord. The aircraft (101) also includes a power module configured to provide power via a fuel cell (131). The fuel cell (131) stores liquid hydrogen as fuel, but uses gaseous hydrogen in the fuel cell (131). A fuel tank heater is used to control the boil-rate of the fuel in the fuel tank. The aircraft (101) of the invention includes a support structure including a plurality of supports, where the supports form a tetrahedron that affixes to the wing (103).
-
公开(公告)号：EP0843822A4
公开(公告)日：1998-11-25
申请号：EP96930301
申请日：1996-07-29
申请人： AEROVIRONMENT INC
发明人： RIPPEL WALLY E , BUCHANAN DARRELL
IPC分类号： G01R31/34 , B60R16/02 , B60R16/03 , G01M17/007 , G01R31/00 , G01R31/28 , G01R31/36 , H02M3/28
CPC分类号： H02M3/285 , B60R16/03 , G01R31/006 , G01R31/2841 , G01R31/34 , G01R31/3631 , H02M2001/008
摘要： A system and mehtod for cycling loads and sources can be connected to one or more loads and sources to controllable supply or absorb current with respect thereto. For example, DC voltages can be controllably supplied to each load from a DC bus using a plurality of DC-DC converters. Various DC converter configurations are available including independent, parallel and differential, to expand the types of simulations which can be performed on the load(s).
-
-
-
-
-
-
-
-
-
搜索结果
136 条记录 (耗时 0.017 秒)
