专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

91. 发明公开

EP3590835A1 TRAILER MOUNTED AIRCRAFT FUSELAGES WITH VIRTUAL ENVIRONMENT SYSTEMS 审中-公开
公开(公告)号：EP3590835A1
公开(公告)日：2020-01-08
申请号：EP19179864.4
申请日：2019-06-13
申请人： Gulfstream Aerospace Corporation
发明人： Toler, Brian , Holbrook, Drew , Patterson, Larry
IPC分类号： B64D1/00 , B64C1/00 , B62D65/14 , G09B9/08
摘要： A system for virtually experiencing an aircraft includes a a trailer, an aircraft fuselage, a cabin module, a head mounted display, and a controller. The aircraft fuselage is disposed in the trailer and defines an interior with a first portion and a second portion. The first portion is substantially unfurnished. The cabin module is disposed in the second portion and includes furnishings. The head mounted display is configured for movement within the interior. The controller is configured for generating a virtual aircraft interior based on a position and an orientation of the head mounted display relative to the interior of the aircraft fuselage and for controlling the head mounted display to display the virtual aircraft interior.

92. 发明公开

EP3552972A3 PROPULSION SYSTEM USING LARGE SCALE VORTEX GENERATORS FOR FLOW REDISTRIBUTION AND SUPERSONIC AIRCRAFT EQUIPPED WITH THE PROPULSION SYSTEM 审中-公开
公开(公告)号：EP3552972A3
公开(公告)日：2019-11-27
申请号：EP19168085.9
申请日：2014-02-05
申请人： Gulfstream Aerospace Corporation
发明人： RYBALKO, Michael , CONNORS, Timothy , WAYMAN, Tom
IPC分类号： B64D33/02
摘要： An arrangement for use with a propulsion system for a supersonic aircraft includes a center body configured for coupling to an inlet and to support a boundary layer formed when the supersonic aircraft is flown at a predetermined altitude supersonic speed. The arrangement further includes a first vortex generator disposed on the center body. The first vortex generator extends a first height above the center body. The arrangement still further includes a second vortex generator disposed on the center body. The second vortex generator extends a second height above the center body, the second height being greater than the first height. The first height and the second height are greater than approximately seventy-five percent of a thickness of the boundary layer proximate a location of the first vortex generator and the second vortex generator, respectively, when the aircraft if flown at the predetermined altitude and the predetermined speed.

93. 发明公开

EP3553004A1 DEVICES AND METHODS FOR DISPENSING ADHESIVE ELEMENTS 审中-公开
公开(公告)号：EP3553004A1
公开(公告)日：2019-10-16
申请号：EP19167166.8
申请日：2019-04-03
申请人： Gulfstream Aerospace Corporation
发明人： Huebner, Phillip , Mollen, Robert , Gosz, Charles , Meier, Paul
IPC分类号： B65H35/00 , B65H16/00
摘要： A device (200), a system and a method for dispensing adhesive elements (301) are provided. The device comprising a first holder (201), a second holder (203), and an alignment element (205). The first holder (201) is configured to rotatably hold a film (315) having adhesive elements (301) and a protective layer (305) attached on adhesive areas of the adhesive elements (301). The second holder (203) is configured to receive the protective layer (305) as the protective layer (305) is peeled off the adhesive areas of the adhesive elements (301) while the adhesive elements are moved towards an alignment element (205). The alignment element (205) is arranged in a direction of movement (313) of the adhesive elements (301) and configured to receive and align the adhesive elements (301) at a predetermined position on the alignment element (205).

94. 发明公开

EP3524933A1 METHOD AND SYSTEM FOR DISPLAYING INFORMATION 审中-公开
公开(公告)号：EP3524933A1
公开(公告)日：2019-08-14
申请号：EP18199549.9
申请日：2013-02-28
申请人： Gulfstream Aerospace Corporation
发明人： Martin, Scott
IPC分类号： G01C21/30 , G01S13/89 , G06T17/05 , G01C23/00
摘要： A display system for an aircraft includes a controller in communication with a display. The controller receives a category associated with a phase of flight of the aircraft. Information related to operation of the aircraft and associated with the received category is displayed on the display.

95. 发明授权

EP2956358B1 SYSTEMS AND METHODS FOR CONTROLLING A MAGNITUDE OF A SONIC BOOM 有权
公开(公告)号：EP2956358B1
公开(公告)日：2019-05-22
申请号：EP14751884.9
申请日：2014-02-10
申请人： Gulfstream Aerospace Corporation
发明人： FREUND, Donald
IPC分类号： B64C3/18 , B64C3/20 , B64C3/38 , B64C17/10 , B64C23/00 , B64C30/00 , B64D37/00

96. 发明授权

EP2956363B1 PROPULSION SYSTEM USING LARGE SCALE VORTEX GENERATORS FOR FLOW REDISTRIBUTION AND SUPERSONIC AIRCRAFT EQUIPPED WITH THE PROPULSION SYSTEM 有权
公开(公告)号：EP2956363B1
公开(公告)日：2019-04-10
申请号：EP14798514.7
申请日：2014-02-05
申请人： Gulfstream Aerospace Corporation
发明人： RYBALKO, Michael , CONNORS, Timothy , WAYMAN, Tom
IPC分类号： B64D33/02

97. 发明公开

EP3434600A1 LOW VISIBILITY LANDING SYSTEM AND METHOD 审中-公开
公开(公告)号：EP3434600A1
公开(公告)日：2019-01-30
申请号：EP18193111.4
申请日：2010-11-02
申请人： Gulfstream Aerospace Corporation
发明人： TAKACS, Robert S. , FREEMAN, Gary M.
IPC分类号： B64D45/04 , G08G5/02 , G01C21/00 , G05D1/06 , G08G5/00
摘要： The present invention includes a low visibility landing system for guiding aircraft on landing approaches which may aid a pilot during landing in low visibility conditions such that an aircraft may descend to lower altitudes without visual contact with the runway than is possible with other landing systems.
The system may use various navigational systems to provide guidance to the pilot to get the aircraft back onto the landing approach plan.

98. 发明公开

EP3154151A1 INTEGRATED POWER DISTRIBUTION, DATA NETWORK, AND CONTROL ARCHITECTURES FOR A VEHICLE 审中-公开
标题翻译： INTEGRIERTE LEISTUNGSVERTEILUNG，DATENNETZ UND STEUERUNGSARCHITEKTURFÜREIN FAHRZEUG
公开(公告)号：EP3154151A1
公开(公告)日：2017-04-12
申请号：EP16192280.2
申请日：2016-10-04
申请人： Gulfstream Aerospace Corporation
发明人： CARLEIAL, Pedro R. , KNIGHT, Michael
IPC分类号： H02J13/00 , H02J4/00 , H02J3/00
CPC分类号： B60R16/03 , B60R16/023 , H02J3/00 , H02J4/00 , H02J13/00
摘要： An integrated power distribution, data network, and control architecture for a vehicle is provided that includes nodes distributed throughout the vehicle. Each node includes power distribution (PD) and data collection and distribution (DCD) components. The PD components receive electrical power from a source external to the node and distribute and control the electrical power supplied to active and passive electrical loads that are external to the node. The PD components include an electrical power input interface configured to receive an electrical power input from a source external to the node, and one or more power control modules. Each power control module can control the electrical power supplied to one or more electrical power output interfaces that supply power to the active and passive electrical loads. The DCD components receive data from data sources external to the node and transmit data to data consumers external to the node.
摘要翻译：提供了一种用于车辆的集成配电，数据网络和控制架构，其包括分布在整个车辆上的节点。每个节点包括功率分配（PD）和数据采集和分配（DCD）组件。 PD组件从节点外部的源接收电力，并分配和控制提供给节点外部的主动和无源电负载的电力。 PD组件包括被配置为从节点外部的源接收电力输入的电力输入接口以及一个或多个功率控制模块。每个功率控制模块可以控制提供给向主动和被动电负载供电的一个或多个电力输出接口的电力。 DCD组件从节点外部的数据源接收数据，并将数据传输到节点外部的数据使用者。

99. 发明授权

EP2744999B1 NOZZLE ARRANGEMENT AND METHOD OF MAKING THE SAME 有权
标题翻译： JETS系统及其制造方法
公开(公告)号：EP2744999B1
公开(公告)日：2016-08-03
申请号：EP12844128.4
申请日：2012-08-17
申请人： Gulfstream Aerospace Corporation
发明人： Conners, Timothy R. , Henne, Preston A. , Howe, Donald C.
IPC分类号： F02K1/46 , F02K1/34 , F02K1/04
CPC分类号： F02K1/46 , B64D33/02 , B64D2033/026 , B64D2033/0273 , B64D2033/0286 , F02C7/00 , F02C7/04 , F02C7/045 , F02K1/04 , F02K1/34 , F02K3/02 , F02K7/00 , F02K7/10 , F02K7/16 , F02K7/20 , F05D2210/12 , F05D2220/323 , F05D2220/80 , F05D2230/60 , F05D2250/70 , F05D2260/96 , Y10T29/49346 , Y10T137/0536

100. 发明公开

EP2942864A2 APPARATUS AND SYSTEMS FOR ENGINE AND GENERATOR CONTROL WITHIN AN AIRCRAFT 审中-公开
标题翻译： VORRICHTUNG UND SYSTEME ZUR MOTOR- UND GENERATORSTEUERUNG IN EINEM FLUGZEUG
公开(公告)号：EP2942864A2
公开(公告)日：2015-11-11
申请号：EP15165461.3
申请日：2015-04-28
申请人： Gulfstream Aerospace Corporation
发明人： Palfreyman, Gary , Knight, Michael
IPC分类号： H02P9/02
CPC分类号： H02P9/02
摘要： A system is provided for engine and generator control. The system includes a compound AC generator, a generator control unit (GCU) module and an engine electronic controller (EEC) module. The compound AC generator includes a shaft, and a permanent magnet generator (PMG) configured to be driven by the shaft to generate an AC power signal. The GCU module is configured to control the compound AC generator. The PMG is coupled to the GCU module and the EEC module such that it is configured to simultaneously supply the AC power signal to the GCU module and to the EEC module.
摘要翻译：提供一种用于发动机和发电机控制的系统。该系统包括复合交流发电机，发电机控制单元（GCU）模块和发动机电子控制器（EEC）模块。复合式交流发电机包括轴和永久磁铁发电机（PMG），永久磁铁发电机被配置为由轴驱动以产生交流电力信号。 GCU模块配置为控制复合式交流发电机。 PMG耦合到GCU模块和EEC模块，使其配置为同时向GCU模块和EEC模块提供AC电源信号。

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