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公开(公告)号：EP0184226B1
公开(公告)日：1988-09-14
申请号：EP85116421.0
申请日：1983-10-12
Applicant: DORNIER GMBH
Inventor： Friedel, Franz , Frühauf, Werner , Harms, Günter , Heise, Georg, Dipl.-Ing. , Lükewille, Heinrich, Dipl.-Ing.
CPC classification number: F42B10/64 , B64C39/024 , B64C2201/028 , B64C2201/044 , B64C2201/165 , B64C2201/201 , F16D7/021 , F42B15/105
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公开(公告)号：EP0184226A3
公开(公告)日：1987-05-06
申请号：EP85116421
申请日：1983-10-12
Applicant: DORNIER GMBH
Inventor： Friedel, Franz , Frühauf, Werner , Harms, Günter , Heise, Georg, Dipl.-Ing. , Lükewille, Heinrich, Dipl.-Ing.
CPC classification number: F42B10/64 , B64C39/024 , B64C2201/028 , B64C2201/044 , B64C2201/165 , B64C2201/201 , F16D7/021 , F42B15/105
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公开(公告)号：EP0184226A2
公开(公告)日：1986-06-11
申请号：EP85116421.0
申请日：1983-10-12
Applicant: DORNIER GMBH
Inventor： Friedel, Franz , Frühauf, Werner , Harms, Günter , Heise, Georg, Dipl.-Ing. , Lükewille, Heinrich, Dipl.-Ing.
CPC classification number: F42B10/64 , B64C39/024 , B64C2201/028 , B64C2201/044 , B64C2201/165 , B64C2201/201 , F16D7/021 , F42B15/105
Abstract: Unbemannter Flugkörper, der in einem Behälter transportiert und aus dem Behälter mittels eines Hilfsantriebes nach Lösung einer Arretierung gestartet wird und der während des Marschfluges durch ein Propellertriebwerk antreibbar ist, wobei eine Reibschlußkupplung (64, 65) am Flugkörper vorgesehen ist, die ohne Zuführung von Energie von aussen mittels des Antriebes (7) den innerhalb des Behälters (1') stillstehenden Propeller (6) mit dem bereits im Behälter laufenden Antriebsmotor (7) nach Verlassen des Behälters kuppelt.
Abstract translation: 这是在一个容器中的锁定机构的释放和后运送并从容器推出由辅助驱动装置无人驾驶飞机是由一个螺旋桨发动机，其特征在于，摩擦离合器（64，65）被设置在导弹，巡航飞行期间驱动其中没有能量的供给 从由所述驱动装置的外侧（7），所述容器（1“）的螺旋桨（6）与当前容器内部的固定到驱动马达（7）在离开容器后脱离。
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公开(公告)号：US20190080142A1
公开(公告)日：2019-03-14
申请号：US15703948
申请日：2017-09-13
Applicant: X Development LLC
Inventor： Dinuka Abeywardena , Damien Jourdan
CPC classification number: G06K9/0063 , B64C2201/028 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64D47/08 , G01C11/06 , G01C21/32 , G05D1/101
Abstract: Described is a method that involves operating an unmanned aerial vehicle (UAV) to begin a flight, where the UAV relies on a navigation system to navigate to a destination. During the flight, the method involves operating a camera to capture images of the UAV's environment, and analyzing the images to detect features in the environment. The method also involves establishing a correlation between features detected in different images, and using location information from the navigation system to localize a feature detected in different images. Further, the method involves generating a flight log that includes the localized feature. Also, the method involves detecting a failure involving the navigation system, and responsively operating the camera to capture a post-failure image. The method also involves identifying one or more features in the post-failure image, and determining a location of the UAV based on a relationship between an identified feature and a localized feature.
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公开(公告)号：US20180022467A1
公开(公告)日：2018-01-25
申请号：US15543443
申请日：2015-11-16
Applicant: Sikorsky Aircraft Corporation
Inventor： Mark R. Alber
CPC classification number: B64D35/04 , B64C27/82 , B64C29/02 , B64C39/024 , B64C2201/028 , B64C2201/088 , B64C2201/104 , B64C2201/165 , B64D27/06 , B64D27/12 , Y02T50/44
Abstract: A vertical take-off and landing (VTOL) aircraft is provided and includes wings, first and second nacelles supported on each of the wings, each of the first and second nacelles including a propeller drivable to generate aircraft thrust, and an asymmetrical power generation unit. The asymmetrical power generation unit includes a single engine unit disposed in only one of the first and second nacelles to generate power to drive the propellers of both the first and second nacelles.
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Patent Agency Ranking
公开(公告)号：US20170328391A1
公开(公告)日：2017-11-16
申请号：US15636236
申请日：2017-06-28
Applicant: Hari Matsuda
Inventor： Hari Matsuda
CPC classification number: F16B2/22 , B64C29/02 , B64C39/024 , B64C2201/028 , B64C2201/042 , B64C2201/127 , B64C2201/128 , B64C2201/141
Abstract: A drone delivered package-to-receiver coupler is described, with a rear portion configured with one or more package attachment surface(s), with support arms extending towards a front of the coupler, being separated from each other to form a gap between them. The coupler contains a living hinge portion spanning the gap and coupled to the support arms, with a pivoting section that translates to open/closed positions, restrained by the support arms. A coupler portion is connected to at least one of the support arms and living hinge, with capture arms extending to the front of the coupler that swing open/close when the pivoting section of the living hinge is translated. Therefore, when a rod or arm is coupled to, it is substantially encompassed by the capture arms and the living hinge, so that the package-to-receiver coupler can slide along the rod or arm in the closed position.
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公开(公告)号：US09669924B2
公开(公告)日：2017-06-06
申请号：US14347375
申请日：2012-09-14
Applicant: Keen Ian Chan
Inventor： Keen Ian Chan
CPC classification number: B64C29/02 , A63H27/12 , B64C13/24 , B64C27/08 , B64C39/02 , B64C39/024 , B64C2201/028 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/165 , G05D1/0669 , Y10T29/49826
Abstract: An unmanned aerial vehicle (UAV) capable of vertical and horizontal flight modes, a method for assembling a UAV, and a kit of parts for assembling a UAV. The UAV comprises a wing structure comprising elongated equal first and second wings; a support structure comprising first and second sections coupled to a middle position of the wing structure and extending in opposite directions perpendicular to the wing structure; and four propellers, each mounted to a respective one of the first and second wings, and first and second sections, for powering the UAV during both vertical and horizontal flight modes.
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公开(公告)号：US20170131717A1
公开(公告)日：2017-05-11
申请号：US15369774
申请日：2016-12-05
Applicant: Airphrame, Inc
Inventor： Bret Kugelmass
CPC classification number: H04Q9/00 , B64C39/024 , B64C2201/021 , B64C2201/028 , B64C2201/042 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/145 , G05D1/0088 , G05D1/0094 , G05D1/042 , G05D1/101 , G05D1/104 , G06T1/0014 , G06T11/206 , G06T11/60 , G08G5/0013 , G08G5/0039 , G08G5/0069 , H04N7/181 , H04Q2209/40 , H04W28/065
Abstract: One variation of a method for imaging an area of interest includes: within a user interface, receiving a selection for a set of interest points on a digital map of a physical area and receiving a selection for a resolution of a geospatial map; identifying a ground area corresponding to the set of interest points for imaging during a mission; generating a flight path over the ground area for execution by an unmanned aerial vehicle during the mission; setting an altitude for the unmanned aerial vehicle along the flight path based on the selection for the resolution of the geospatial map and an optical system arranged within the unmanned aerial vehicle; setting a geospatial accuracy requirement for the mission based on the selection for the mission type; and assembling a set of images captured by the unmanned aerial vehicle during the mission into the geospatial map.
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公开(公告)号：US20170021943A1
公开(公告)日：2017-01-26
申请号：US15291870
申请日：2016-10-12
Applicant: Aurora Flight Sciences Corporation
Inventor： James Peverill , Adam Woodworth , Benjamin Freudberg , Dan Cottrell
CPC classification number: B64F1/02 , B60L11/1816 , B60L11/1838 , B60L2200/10 , B64C25/68 , B64C39/024 , B64C2201/028 , B64C2201/042 , B64C2201/06 , B64C2201/066 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/182 , B64D47/04 , B64D47/08 , B64F1/362 , G05D1/101 , G06K9/0063 , Y02T10/7005 , Y02T10/7072 , Y02T90/121 , Y02T90/128 , Y02T90/14 , Y02T90/16 , Y02T90/163
Abstract: A capturing hook for engaging a cable during capture and release of an aerial vehicle may comprise a first and second gate pivotally supported at their first ends by a base portion and each being movable between a closed position and an open position, but spring-biased to the closed position. The capturing hook may further include a latch device comprising a movable locking part biased by a return spring to a locked position to lock the second gate in the closed position.
Abstract translation: 用于在捕捉和释放空中飞行器期间接合电缆的捕获钩可以包括第一和第二门，其第一和第二门在其第一端处由基部枢转地支撑，并且每个可在关闭位置和打开位置之间移动，但是弹簧偏置到 关闭位置。 捕获钩还可以包括闩锁装置，其包括由复位弹簧偏压到锁定位置的可移动锁定部件，以将第二闸门锁定在关闭位置。
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120.发明申请公开(公告)号：US20160375981A1
公开(公告)日：2016-12-29
申请号：US15111133
申请日：2015-01-13
Applicant: ADVANCED PRODUCT DEVELOPMENT, LLC
Inventor： William Randall McDonnell
CPC classification number: B64C3/10 , B63H9/0685 , B64C39/024 , B64C2201/028 , B64C2201/082 , B64C2201/182 , B64C2201/205 , B64C2201/208 , B64F1/02 , B64F1/04 , B64F1/222 , Y02T50/12 , Y02T50/826
Abstract: An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft slide into and out of the hangar on dollies (90) like circuit boards in a computer and are launched and recovered using a large towed parafoil (6).
Abstract translation: 一架不对称的飞机（1）和一架可从小型船只运行的飞机（1），并在一架直升机机库（107）内以三个或更多的飞机高密度存储，无需起落架或机翼折叠。 这些飞机在计算机上像电路板一样滑入和移出机库（90）的机库，并使用大型拖缆机（6）发射和恢复。
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