公开(公告)号：US20180093171A1

公开(公告)日：2018-04-05

申请号：US15711695

申请日：2017-09-21

申请人： SONY INTERACTIVE ENTERTAINMENT INC.

发明人： Dominic Saul Mallinson

IPC分类号： A63F7/06 ,  B64C39/02 ,  G05D1/00

CPC分类号： A63F7/0664 ,  A63F7/0604 ,  A63F7/07 ,  A63F7/20 ,  A63F13/65 ,  A63F13/803 ,  A63H27/12 ,  A63H30/04 ,  B64C39/024 ,  B64C2201/10 ,  B64C2201/12 ,  B64C2201/146 ,  B64F1/04 ,  B65G51/00 ,  G05D1/0016

摘要： An arena includes a porous surface through which an airflow is output, thereby providing lift for an unmanned aerial vehicle (UAV) to push the UAV away from the porous surface. The airflow may also provide thrust to push the UAV in a direction that is parallel to the porous surface. The UAV may include one or more propellers that can provide lift, thrust, or both to the UAV. The airflow may be modified over a duration of time to modify lift or thrust to the UAV. The airflow may be modified based on regions of the arena to modify lift or thrust in different regions of the arena. The arena may include a scoreboard to display a score that may be modified as a result of actions undertaken by the UAV. Two or more UAVs may be used to play a game via the arena.

公开(公告)号：US20170129600A1

公开(公告)日：2017-05-11

申请号：US15345376

申请日：2016-11-07

申请人： David Rancourt ,  Etienne Demers Bouchard

发明人： David Rancourt ,  Etienne Demers Bouchard

IPC分类号： B64C39/02 ,  B64C29/00 ,  B64C19/02 ,  B64C1/00

CPC分类号： B64C39/022 ,  B64C1/00 ,  B64C19/02 ,  B64C29/0016 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/10 ,  B64C2211/00 ,  B64D2221/00 ,  G05D1/104

摘要： A vertical liftoff aircrafts system includes a plurality of unmanned wing structures configured for collective vertical liftoff; a plurality of tethers respectively connected to the plurality of wing structures; and a fuselage including a connector thereon for mechanically connecting the plurality of tethers. The fuselage includes a power pack for powering the plurality of wing structures via the plurality of tethers, whereby the plurality of wing structures is operatively interconnected to the fuselage with the plurality of tethers for lifting the fuselage. A method and a kit thereof also are disclosed.

公开(公告)号：US08205823B2

公开(公告)日：2012-06-26

申请号：US12795539

申请日：2010-06-07

申请人： Matthew Todd Keennon ,  Karl Robert Klingebiel ,  Alexander Andryukov ,  Bart Dean Hibbs ,  John Peter Zwaan

发明人： Matthew Todd Keennon ,  Karl Robert Klingebiel ,  Alexander Andryukov ,  Bart Dean Hibbs ,  John Peter Zwaan

IPC分类号： B64C33/00

CPC分类号： B64C33/025 ,  B64C19/00 ,  B64C33/02 ,  B64C2201/025 ,  B64C2201/10 ,  B64C2201/146

摘要： Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.

摘要翻译： 比空中飞行器，具有扑翼的飞机，例如鸟巢飞机，其中角度定向控制是通过在扫掠角度行程和/或控制可变翼膜张力的过程中可展开的翼的偏转的可变差分扫掠角来实现的 。

公开(公告)号：US07931239B2

公开(公告)日：2011-04-26

申请号：US11838040

申请日：2007-08-13

申请人： Brad Pedersen ,  Peter Spirov

发明人： Brad Pedersen ,  Peter Spirov

IPC分类号： B64C13/20

CPC分类号： G05D1/0816 ,  B60V1/06 ,  B60V1/10 ,  B64C15/02 ,  B64C27/08 ,  B64C27/20 ,  B64C39/001 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/10 ,  B64C2201/108 ,  B64C2201/146 ,  B64D27/24 ,  G05D1/0016 ,  G05D1/0022 ,  G05D1/0858

摘要： A homeostatic flying hovercraft preferably utilizes at least two pairs of counter-rotating ducted fans to generate lift like a hovercraft and utilizes a homeostatic hover control system to create a flying craft that is easily controlled. The homeostatic hover control system provides true homeostasis of the craft with a true fly-by-wire flight control and control-by-wire system control.

摘要翻译： 稳态飞行气垫船优选地使用至少两对反向旋转管道风扇来产生类似气垫船的升降机，并且利用稳态悬停控制系统来创建易于控制的飞行器。 稳态悬停控制系统通过真正的线控飞行控制和线控系统控制为飞行器提供真正的动态平衡。

公开(公告)号：US09957044B2

公开(公告)日：2018-05-01

申请号：US14247062

申请日：2014-04-07

申请人： AeroVironment, Inc.

发明人： Matthew Todd Keennon ,  Karl Robert Klingebiel ,  Alexander Andryukov ,  Bart Dean Hibbs ,  John Peter Zwaan

IPC分类号： B64C33/02 ,  B64C19/00

CPC分类号： B64C33/025 ,  B64C19/00 ,  B64C33/02 ,  B64C2201/025 ,  B64C2201/10 ,  B64C2201/146

摘要： Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.

公开(公告)号：US20180057164A1

公开(公告)日：2018-03-01

申请号：US15425066

申请日：2017-02-06

申请人： INVENTEC APPLIANCES (PUDONG) CORPORATION ,  INVENTEC APPLIANCES CORP. ,  Inventec Appliances (Shanghai) Co. Ltd.

发明人： De-Zheng Lan ,  Shih-Chin Tseng ,  Shih-Kuang Tsai

IPC分类号： B64C39/02 ,  B64D27/24 ,  B64D33/04 ,  B64C15/02 ,  F02K1/15

CPC分类号： B64C39/024 ,  B64C15/02 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/10 ,  B64C2201/108 ,  B64C2201/162 ,  B64D27/24 ,  B64D33/04 ,  F02K1/15 ,  F04D25/06 ,  F04D29/284 ,  F05D2240/90

摘要： An unmanned aerial vehicle (UAV) including a vehicle body and an airflow thruster is provided. The vehicle body has a center hub, an airflow guiding structure and an outer circumferential portion. An interior of the airflow guiding structure is interconnected between the center hub and the outer circumferential portion. The center hub has an airflow inlet. The outer circumferential portion has a plurality of lateral guiding outlets facing downward and corresponding to a gravity direction of the gravity direction of the unmanned aerial vehicle. The airflow thruster is disposed inside the center hub for generating a plurality of jet streams, such that the jet streams flow to the lateral guiding outlets through the airflow guiding structure to generate a propulsion.

公开(公告)号：US20170113787A1

公开(公告)日：2017-04-27

申请号：US14997510

申请日：2016-01-16

申请人： Kim F. Hein

发明人： Kim F. Hein

IPC分类号： B64C15/02 ,  B64C39/02

CPC分类号： B64C39/022 ,  A62C31/03 ,  A62C31/05 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/10 ,  B64C2201/12

摘要： A hydraulically propelled drone is provided for delivering firefighting fluid to an elevated location. The drone comprises a housing having a primary inlet configured to receive the distal end of a fire hose, a primary outlet configured to receive the inlet end of a primary nozzle, a central passageway configured to conduct fluid from the primary inlet to the primary outlet, and at least one secondary outlet communicating with the central passageway. At least one lift nozzle communicates with the secondary outlet and is configured to direct fluid in a generally downward direction so as to produce an upward thrust on the drone housing, and at least one valve is contained within the housing and configured to control the flow of said fluid through the primary nozzle and the at least one lift nozzle nozzle.

公开(公告)号：US20160160353A1

公开(公告)日：2016-06-09

申请号：US14903861

申请日：2014-07-09

申请人： UNITED TECHNOLOGIES CORPORATION

发明人： Michael S. Miarecki ,  Charles R. Watson ,  Grant O. Cook ,  Joseph Parkos

IPC分类号： C23C18/16 ,  C25D3/02

CPC分类号： C25D5/56 ,  B05D5/00 ,  B05D7/02 ,  B22C7/023 ,  B22C9/043 ,  B22C9/10 ,  B28B1/24 ,  B28B7/342 ,  B28B11/04 ,  B28B11/243 ,  B32B3/263 ,  B32B7/12 ,  B32B15/04 ,  B32B15/08 ,  B32B15/20 ,  B32B37/12 ,  B32B37/1284 ,  B32B37/14 ,  B32B2255/10 ,  B32B2307/202 ,  B32B2307/554 ,  B32B2603/00 ,  B33Y10/00 ,  B33Y80/00 ,  B62D35/00 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/10 ,  C04B35/76 ,  C04B35/806 ,  C09D5/26 ,  C23C14/20 ,  C23C16/06 ,  C23C18/1633 ,  C23C18/165 ,  C23C18/2013 ,  C23C18/22 ,  C23C18/31 ,  C23C26/00 ,  C23C28/02 ,  C25D3/02 ,  C25D3/38 ,  C25D3/46 ,  C25D5/48 ,  C25D9/04 ,  C25D11/20 ,  F01D5/00 ,  F01D5/147 ,  F01D5/187 ,  F01D5/284 ,  F01D5/288 ,  F01D9/02 ,  F01D9/041 ,  F01D11/08 ,  F01D25/005 ,  F04D29/023 ,  F04D29/324 ,  F04D29/542 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/22 ,  F05D2230/30 ,  F05D2230/312 ,  F05D2230/314 ,  F05D2240/122 ,  F05D2240/304 ,  F05D2300/10 ,  F05D2300/11 ,  F05D2300/121 ,  F05D2300/132 ,  F05D2300/133 ,  F05D2300/1616 ,  F05D2300/171 ,  F05D2300/177 ,  F05D2300/20 ,  F05D2300/30 ,  F05D2300/44 ,  F05D2300/501 ,  F05D2300/603 ,  F05D2300/611 ,  F05D2300/614 ,  F42B10/02

摘要： A plated polymer component is disclosed. The plated polymer component may comprise a polymer substrate having an outer surface, a metal plating attached to the outer surface of the polymer substrate, and at least one interlocking feature connecting the polymer substrate and the metal plating. The interlocking feature may improve the interfacial bond strength between the polymer substrate and the metal plating.

摘要翻译： 公开了镀覆的聚合物组分。 镀覆的聚合物组分可以包括具有外表面的聚合物基材，附着到聚合物基材的外表面的金属电镀以及连接聚合物基材和金属电镀的至少一个互锁特征。 互锁特征可以改善聚合物基材和金属电镀之间的界面粘结强度。

公开(公告)号：US20160158964A1

公开(公告)日：2016-06-09

申请号：US14903903

申请日：2014-07-09

申请人： UNITED TECHNOLOGIES CORPORATION

发明人： Michael S. Miarecki ,  Joseph Parkos ,  Gary M. Lomasney ,  Charles R. Watson

IPC分类号： B28B7/34 ,  B28B11/04 ,  B28B11/24 ,  F01D11/08 ,  C04B35/76 ,  F01D5/28 ,  F01D5/18 ,  B28B1/24 ,  C04B35/80

CPC分类号： C25D5/56 ,  B05D5/00 ,  B05D7/02 ,  B22C7/023 ,  B22C9/043 ,  B22C9/10 ,  B28B1/24 ,  B28B7/342 ,  B28B11/04 ,  B28B11/243 ,  B32B3/263 ,  B32B7/12 ,  B32B15/04 ,  B32B15/08 ,  B32B15/20 ,  B32B37/12 ,  B32B37/1284 ,  B32B37/14 ,  B32B2255/10 ,  B32B2307/202 ,  B32B2307/554 ,  B32B2603/00 ,  B33Y10/00 ,  B33Y80/00 ,  B62D35/00 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/10 ,  C04B35/76 ,  C04B35/806 ,  C09D5/26 ,  C23C14/20 ,  C23C16/06 ,  C23C18/1633 ,  C23C18/165 ,  C23C18/2013 ,  C23C18/22 ,  C23C18/31 ,  C23C26/00 ,  C23C28/02 ,  C25D3/02 ,  C25D3/38 ,  C25D3/46 ,  C25D5/48 ,  C25D9/04 ,  C25D11/20 ,  F01D5/00 ,  F01D5/147 ,  F01D5/187 ,  F01D5/284 ,  F01D5/288 ,  F01D9/02 ,  F01D9/041 ,  F01D11/08 ,  F01D25/005 ,  F04D29/324 ,  F04D29/542 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/22 ,  F05D2230/30 ,  F05D2230/312 ,  F05D2230/314 ,  F05D2240/122 ,  F05D2240/304 ,  F05D2300/10 ,  F05D2300/11 ,  F05D2300/121 ,  F05D2300/132 ,  F05D2300/133 ,  F05D2300/1616 ,  F05D2300/171 ,  F05D2300/177 ,  F05D2300/20 ,  F05D2300/30 ,  F05D2300/44 ,  F05D2300/501 ,  F05D2300/603 ,  F05D2300/611 ,  F05D2300/614 ,  F42B10/02

摘要： A method for fabricating a ceramic component is disclosed. The method may comprise: 1) forming a polymer template having a shape that is an inverse of a shape of the ceramic component, 2) placing the polymer template in a mold; 3) injecting the polymer template with a ceramic slurry, 4) firing the ceramic slurry at a temperature to produce a green body, and 5) sintering the green body at an elevated temperature to provide the ceramic component.

摘要翻译： 公开了一种制造陶瓷部件的方法。 该方法可以包括：1）形成具有与陶瓷组分形状相反的形状的聚合物模板，2）将聚合物模板放置在模具中; 3）用陶瓷浆料注入聚合物模板，4）在一温度下烧制陶瓷浆料以产生生坯，和5）在升高的温度下烧结生坯以提供陶瓷组分。

公开(公告)号：US20130168493A1

公开(公告)日：2013-07-04

申请号：US13532699

申请日：2012-06-25

申请人： Matthew Todd Keennon ,  Karl Robert Klingebiel ,  Alexander Andryukov ,  Bart Dean Hibbs ,  John Peter Zwaan

发明人： Matthew Todd Keennon ,  Karl Robert Klingebiel ,  Alexander Andryukov ,  Bart Dean Hibbs ,  John Peter Zwaan

IPC分类号： B64C33/02

CPC分类号： B64C33/025 ,  B64C19/00 ,  B64C33/02 ,  B64C2201/025 ,  B64C2201/10 ,  B64C2201/146

摘要： Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.