-
公开(公告)号：US11548657B2
公开(公告)日：2023-01-10
申请号：US16980541
申请日：2019-03-11
发明人： Gil Gelman , David Elnekave , Yoav Herzig
摘要： An aerial vehicle securing system for use with a base portion of an aerial vehicle, comprising: at least one substantially flat platform for supporting said base portion upon landing of the vehicle thereon; at least one magnetizable element configured to be integrated in one of said platform or base portion; at least one electropermanent magnet configured to be integrated in another one of said platform or base portion, said electropermanent magnet configured for generating a magnetic field, so that upon a distance between said base portion and said platform reaching a pre-determined value during the landing of the vehicle on the platform, said magnetic field is configured to cause magnetizable element to be attracted to at least said one electropermanent magnet; and a power supply module configured for generating an electric current to said at least one electropermanent magnet for selectively generating and cancelling said magnetic field.
-
公开(公告)号：US20210002002A1
公开(公告)日：2021-01-07
申请号：US16980541
申请日：2019-03-11
发明人： Gil Gelman , David Elnekave , Yoav Herzig
摘要： An aerial vehicle securing system for use with a base portion of an aerial vehicle, comprising: at least one substantially flat platform for supporting said base portion upon landing of the vehicle thereon; at least one magnetizable element configured to be integrated in one of said platform or base portion; at least one electropermanent magnet configured to be integrated in another one of said platform or base portion, said electropermanent magnet configured for generating a magnetic field, so that upon a distance between said base portion and said platform reaching a pre-determined value during the landing of the vehicle on the platform, said magnetic field is configured to cause magnetizable element to be attracted to at least said one electropermanent magnet; and a power supply module configured for generating an electric current to said at least one electropermanent magnet for selectively generating and cancelling said magnetic field.
-
公开(公告)号：US11174024B2
公开(公告)日：2021-11-16
申请号：US16470429
申请日：2017-12-27
发明人： Yoav Herzig , Daniel Marom
摘要： An aircraft pylon is provided, configured for mounting to the underside of an aircraft wing projecting from a fuselage and for carrying an external payload suspended therefrom. The pylon comprises an attachment mechanism configured for facilitating mounting of the pylon to the aircraft wing, and a carrying arrangement configured for carrying the payload and being pivotally articulated to the attachment mechanism. The pylon is configured to selectively pivot the carrying arrangement about a pylon axis between a vertical position in which it is suspended in a substantially vertical orientation, and a tilted position in which it is tilted toward the fuselage.
-
公开(公告)号：US20170096223A1
公开(公告)日：2017-04-06
申请号：US15128169
申请日：2015-03-22
发明人： Yoav Herzig
摘要： An aircraft pylon comprising a body for mounting to an aircraft, a suspension mechanism mounted on said body and being configured for attaching thereto a payload, and a moving door configured for selectively covering and uncovering at least a part of said suspension mechanism
-
公开(公告)号：US20200247541A1
公开(公告)日：2020-08-06
申请号：US16835684
申请日：2020-03-31
发明人： Yoav Herzig
摘要： A pylon for mounting to a bottom surface of an aircraft and for carrying an external payload is provided. The pylon comprises a body spanning along a vertical axis between an upper face and a lower face, the upper face comprising one or more mounting arrangements configured to facilitate mounting the pylon to the bottom surface of the aircraft, the lower face comprising at least one suspension mechanism configured to facilitate selective attachment of the payload to the pylon. The pylon further comprises a covering arrangement configured for selective shifting between a closed position in which it covers the suspension mechanism and an open position in which the suspension mechanism is uncovered. The width of the body varies smoothly along the vertical axis between, inclusively, the upper and lower faces.
-
公开(公告)号：US20200010195A1
公开(公告)日：2020-01-09
申请号：US16470429
申请日：2017-12-27
发明人： Yoav Herzig , Daniel Marom
摘要： An aircraft pylon is provided, configured for mounting to the underside of an aircraft wing projecting from a fuselage and for carrying an external payload suspended therefrom. The pylon comprises an attachment mechanism configured for facilitating mounting of the pylon to the aircraft wing, and a carrying arrangement configured for carrying the payload and being pivotally articulated to the attachment mechanism. The pylon is configured to selectively pivot the carrying arrangement about a pylon axis between a vertical position in which it is suspended in a substantially vertical orientation, and a tilted position in which it is tilted toward the fuselage.
-
公开(公告)号：US11370543B2
公开(公告)日：2022-06-28
申请号：US16835684
申请日：2020-03-31
发明人： Yoav Herzig
摘要： A pylon for mounting to a bottom surface of an aircraft and for carrying an external payload is provided. The pylon comprises a body spanning along a vertical axis between an upper face and a lower face, the upper face comprising one or more mounting arrangements configured to facilitate mounting the pylon to the bottom surface of the aircraft, the lower face comprising at least one suspension mechanism configured to facilitate selective attachment of the payload to the pylon. The pylon further comprises a covering arrangement configured for selective shifting between a closed position in which it covers the suspension mechanism and an open position in which the suspension mechanism is uncovered. The width of the body varies smoothly along the vertical axis between, inclusively, the upper and lower faces.
-
公开(公告)号：US09840336B2
公开(公告)日：2017-12-12
申请号：US14163515
申请日：2014-01-24
发明人： Moshe Barsheshet , Yoav Herzig , Elie Koskas , Michael Litvak , Daniel Frydman
IPC分类号： B64D39/04
CPC分类号： B64D39/04
摘要： A Wireless Communication and Sensor System (WSCC) serving a refueled entity and a refueling entity, the system comprising nozzle load sensing functionality for a nozzle Boom Tip Unit; and apparatus for wirelessly transmitting loads sensed by the nozzle load sensing functionality to at least one of a boom operator and a boom flight control computer.
-
公开(公告)号：US20160325928A1
公开(公告)日：2016-11-10
申请号：US15112260
申请日：2015-01-18
发明人： Hanan Lepek , Yoav Herzig , Omer Einav , Doron Shabanov
CPC分类号： B65D90/0006 , B65G1/0471 , B65G63/004 , F16B2/04 , F16B2/14 , F16B2/18
摘要： A securing mechanism for securing thereto a load. The securing mechanism comprises a locking member having at least one planner with a peripheral shape, a cam follower mechanism having a follower with a load facing end and being configured to translate a linear displacement along an axis being perpendicular to said load facing end to a rotational movement thereof about said axis, and being so disposed relative to said locking member such that said rotational movement thereof sequentially shifts said locking member between a released position in which at least one dimension of said peripheral shape has a first size and a secured position in which said dimension has a second size, said second size being larger than said first size.
摘要翻译： 用于固定负载的固定机构。 固定机构包括具有至少一个具有外围形状的计划器的锁定构件，凸轮从动件机构，其具有带有负载的端部的从动件，并且构造成沿着垂直于所述面向负载端的轴线平移直线位移至旋转 并且相对于所述锁定构件设置成使得所述旋转运动顺序地将所述锁定构件移动到释放位置，其中所述周边形状的至少一个尺寸具有第一尺寸和固定位置，其中， 所述尺寸具有第二尺寸，所述第二尺寸大于所述第一尺寸。
-
-
-
-
-
-
-
-
搜索结果
9 条记录 (耗时 0.012 秒)
