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公开(公告)号：US20120279641A1
公开(公告)日：2012-11-08
申请号：US13484007
申请日：2012-05-30
Applicant: Danny Ball , Kevin Pfeiffer
Inventor： Danny Ball , Kevin Pfeiffer
CPC classification number: B64C11/26 , B32B9/00 , B32B27/00 , B32B27/38 , B32B37/00 , B32B37/02 , B32B37/18 , B64C11/00 , B64C11/02 , B64C11/04 , B64C11/20 , B64C2201/00 , Y10T29/49332 , Y10T156/1057 , Y10T156/1089
Abstract: A method for making a propeller product is disclosed. The propeller is formed using polyurethane cores adhered to a laminate hub to form a core assembly. An encapsulating structural laminate skin is then formed on the core assembly using a resin-transfer-molding process to create a single-piece composite propeller.
Abstract translation: 公开了制造螺旋桨产品的方法。 螺旋桨使用粘附到叠层轮毂上的聚氨酯芯形成芯组件。 然后使用树脂传递模塑工艺在芯组件上形成封装的结构层压板表层以产生单件复合螺旋桨。
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公开(公告)号：US08109462B2
公开(公告)日：2012-02-07
申请号：US12957989
申请日：2010-12-01
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
CPC classification number: B64B1/06 , B64B1/10 , B64B1/12 , B64B1/30 , B64B1/34 , B64B2201/00 , B64C2201/00
Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.
Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。
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公开(公告)号：US20100270424A1
公开(公告)日：2010-10-28
申请号：US12429542
申请日：2009-04-24
Applicant: James D. DeLaurier
Inventor： James D. DeLaurier
CPC classification number: B64B1/06 , B64B1/14 , B64B1/20 , B64B1/30 , B64B2201/00 , B64C2201/00 , G09F21/08 , G09F21/10
Abstract: A hybrid airship comprises a non-rigid body having a delta-wing shape and an airfoil cross-section. The body is shaped for generating aerodynamic lift during forward flight, and contains a gas for generating buoyancy lift. At least one splitter plate is pivotally connected along a trailing edge of the body. The splitter plate is configured to be controllably pivoted for controlling the airship.
Abstract translation: 混合式飞艇包括具有三角翼形状和翼型横截面的非刚性体。 身体形状适合在向前飞行期间产生空气动力升力，并且包含产生浮力升力的气体。 至少一个分离板沿主体的后缘枢转地连接。 分离板构造成可控地枢转以控制飞艇。
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公开(公告)号：US1288318A
公开(公告)日：1918-12-17
申请号：US24078318
申请日：1918-06-19
Applicant: WASHINGTON ELWOOD
Inventor： WASHINGTON ELWOOD
CPC classification number: B64C2201/00
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公开(公告)号：US1084099A
公开(公告)日：1914-01-13
申请号：US1912690639
申请日：1912-04-13
Applicant: MCMAHON CONNELL M
Inventor： MCMAHON CONNELL M
CPC classification number: B64C2201/00
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Patent Agency Ranking
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公开(公告)号：EP3282335A1
公开(公告)日：2018-02-14
申请号：EP17185061.3
申请日：2017-08-07
Applicant: Parrot Drones
IPC: G05D1/00
CPC classification number: G05D1/0088 , A63H30/04 , B64C39/024 , B64C39/10 , B64C2201/00 , B64C2201/028 , B64C2201/104 , B64C2201/141 , B64C2201/146 , B64C2203/00 , B64D47/08 , G05D1/0038 , G05D1/101
Abstract: Le module intègre dans un même boitier monobloc (48) un circuit électronique (100) et une pluralité de capteurs d'attitude, d'altitude, de vitesse, d'orientation et/ou de position du drone (104-116). Il intègre également un circuit électronique de puissance (200) recevant des consignes de commande élaborées par le processeur du circuit électronique en fonction des données délivrées par les capteurs intégrés, et délivrant en sortie des signaux correspondants pour l'alimentation directe en courant ou en tension des moyens propulseurs du drone et des gouvernes.
Abstract translation: 该模块将电子电路（100）和无人驾驶飞机（104-116）的多个传感器姿态，高度，速度，取向和/或位置集成到同一整体式封装（48）中。 它还集成了电子电源电路（200），接收由电子电路的处理器根据由集成传感器传送的数据开发的控制命令，并输出用于直接电源或电压的相应信号 无人机和控制表面的推进手段。
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公开(公告)号：EP3274255A1
公开(公告)日：2018-01-31
申请号：EP16769780.4
申请日：2016-03-25
Applicant: Matternet, Inc.
Inventor： HINKLE, Christopher , RAPTOPOULOS, Andreas , LARSEN, Kendall , BARUCHIN, Ido
CPC classification number: G08G5/0034 , B64C39/024 , B64C2201/00 , B64C2201/027 , B64C2201/14 , G01C21/20 , G08G5/0013 , G08G5/0026 , G08G5/0039 , G08G5/006 , G08G5/0069
Abstract: A system and process for dynamically determining a route for an unmanned aerial vehicle (UAV) is provided. In one example, at a computer system including one or more processors and memory, the process includes receiving a route request, the route request including an origin location and destination location for a UAV, receiving geospatial information associated with the origin location and the destination location, the geospatial information comprising at least one of physical obstacles and no-fly zones, determining a route of the UAV from the origin location to the destination location based at least in part on the geo-spatial information, and causing the route to be communicated to the UAV.
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公开(公告)号：EP3180245A1
公开(公告)日：2017-06-21
申请号：EP15754067.5
申请日：2015-08-07
Applicant: Amazon Technologies, Inc.
Inventor： BUCHMUELLER, Daniel , BECKMAN, Brian C. , NAVOT, Amir , PORTER, Brandon William , KIMCHI, Gur , BEZOS, Jeffrey P. , SCHAFFALITZKY, Frederik
CPC classification number: B64D31/06 , B64C11/00 , B64C39/02 , B64C39/024 , B64C2201/00 , B64C2201/042 , B64C2201/108 , B64C2201/128 , B64D1/12 , B64D27/24 , B64D45/00 , F16D43/00 , F16P3/00 , G08G5/04 , H02P3/04 , H02P3/10
Abstract: The disclosure describes an automated aerial vehicle (AAV) and system for automatically detecting a contact or an imminent contact between a propeller of the AAV and an object (e.g., human, pet, or other animal). When a contact or an imminent contact is detected, a safety profile may be executed to reduce or avoid any potential harm to the object and/or the AAV. For example, if a contact with a propeller of the AAV by an object is detected, the rotation of the propeller may be stopped to avoid harming the object. Likewise, an object detection component may be used to detect an object that is nearing a propeller, stop the rotation of the propeller, and/or navigate the AAV away from the detected object.
Abstract translation: 本公开描述了用于自动检测AAV的螺旋桨和物体（例如，人，宠物或其他动物）之间的接触或即将接触的自动化飞行器（AAV）和系统。 当检测到联系人或即将发生的联系人时，可以执行安全配置文件以减少或避免对物体和/或AAV的任何潜在伤害。 例如，如果检测到物体与AAV的螺旋桨的接触，螺旋桨的旋转可以停止以避免危害物体。 类似地，可以使用物体检测部件来检测靠近螺旋桨的物体，停止螺旋桨的旋转，和/或使AAV远离检测到的物体。
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公开(公告)号：EP2909689B1
公开(公告)日：2016-10-05
申请号：EP13785582.1
申请日：2013-10-22
Applicant: BCB International Limited , Torquing Group Ltd.
Inventor： REEDMAN, Ivan , DAVIES, Barry
IPC: G05D1/10
CPC classification number: B64C39/024 , B64C19/00 , B64C39/028 , B64C2201/00 , B64C2201/14 , B64C2201/141 , B64C2230/00 , B64C2230/02 , G01S15/06 , G01S15/88 , G01S15/89 , G01S15/8913 , G01S15/8929 , G01S15/8993 , G01S15/93 , G05D1/0088 , G05D1/0202 , G05D1/101 , G05D1/102 , Y10S367/909
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