专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

41. 发明申请

US20170233053A1 GAS-FILLED CARRIER AIRCRAFTS AND METHODS OF DISPERSING UNMANNED AIRCRAFT SYSTEMS IN DELIVERING PRODUCTS 审中-公开
公开(公告)号：US20170233053A1
公开(公告)日：2017-08-17
申请号：US15427277
申请日：2017-02-08
申请人： Wal-Mart Stores, Inc.
发明人： Donald R. High , David C. Cox
IPC分类号： B64B1/02 , B64D5/00 , G05D1/00 , B64C39/02 , G06Q10/08 , G08G5/00
CPC分类号： B64B1/02 , B64B1/06 , B64C39/024 , B64C2201/082 , B64C2201/128 , B64C2201/146 , B64C2201/206 , B64D5/00 , G05D1/0027 , G06Q10/0833 , G08G5/0034 , G08G5/0069
摘要： In some embodiments, apparatuses and methods are provided herein useful to transport unmanned aircraft systems to delivery products. In some embodiments, gas-filled aerial transport and launch system, comprises: a transport aircraft comprising: a gas chamber; and a carrier compartment where the gas chamber induces a lifting force on the carrier compartment; at least one propulsion system; and a navigation control system that controls the direction of travel of the transport aircraft; wherein the carrier compartment comprises: an unmanned aircraft system (UAS) storage area configured to receive multiple UASs; and an UAS launching bay that enables the UAS to be launched while the transport aircraft is in flight and while the UAS is carrying a package to be delivered.

42. 发明授权

US09567055B2 Airship pitch trim and directional control system 有权
标题翻译：飞艇间距和方向控制系统
公开(公告)号：US09567055B2
公开(公告)日：2017-02-14
申请号：US15164450
申请日：2016-05-25
申请人： Raven Industries, Inc.
发明人： Michael Scott Smith , Randy E. Scott
IPC分类号： B64B1/02 , B64B1/38 , B64B1/22 , B64B1/24 , B64B1/42 , G05D1/08 , B64B1/34 , B64D27/24 , B64D41/00
CPC分类号： B64B1/38 , B64B1/22 , B64B1/24 , B64B1/34 , B64B1/42 , B64D27/24 , B64D2041/005 , G05D1/0808
摘要： An example can include a pod detachably coupled to a hull. At least one thrust generator can be fixed to the pod. A power source can be mounted to the pod and slideable fore and aft. A power source actuator can be coupled between the pod and the power source to translate the location of the power source with respect to the pod. A sensor can be coupled to the pod to detect a pitch of the hull and provide a pitch signal. A controller can be coupled to one or more of the power source, the power source actuator, the first and second thrust generators and the sensor. The controller can maintain a pitch of the hull by translating the power source within the pod in association with the pitch signal.
摘要翻译：一个示例可以包括可拆卸地联接到船体的舱。至少一个推力发生器可以固定到荚。电源可以安装到荚上，并可前后滑动。电源致动器可以耦合在容器和电源之间，以将电源相对于容器的位置转换。传感器可以耦合到舱，以检测船体的桨距并提供俯仰信号。控制器可以耦合到电源，电源致动器，第一和第二推力发生器和传感器中的一个或多个。控制器可以通过与音高信号相关联地转换盒内的电源来维持船体的音调。

43. 发明授权

US09463861B2 High altitude balloon system 有权
公开(公告)号：US09463861B2
公开(公告)日：2016-10-11
申请号：US14804038
申请日：2015-07-20
申请人： Raven Industries, Inc.
发明人： Michael S. Smith , Kurt L. Sehnert , Randy E. Scott , Justin Lee Marsh , Mark L. West
IPC分类号： B64B1/02 , B64B1/08 , B64B1/44 , B64B1/70 , B64D45/02 , B64B1/30 , B64B1/42 , B64B1/58
CPC分类号： B64B1/08 , B64B1/30 , B64B1/42 , B64B1/44 , B64B1/58 , B64B1/70 , B64D45/02 , Y10T156/10
摘要： A high altitude balloon system includes a dual chamber balloon extending from an upper apex to a lower apex with a circumferential edge between the upper and lower apexes. A deflectable diaphragm is within the dual chamber balloon and coupled along the circumferential edge. The deflectable membrane divides the dual chamber balloon into a lift gas chamber formed by an interior surface of the dual chamber balloon and the deflectable diaphragm, and a ballast chamber formed by the interior surface of the dual chamber balloon and the deflectable diaphragm. Optionally, the dual chamber balloon is constructed by interposing the deflectable diaphragm between an upper and lower balloon panels. Each of the upper and lower balloon panels and the deflectable diaphragm are then coupled together along the circumferential edge to form both the lift gas chamber and the ballast chamber.

44. 发明申请

US20160052614A1 VARIABLE BUOYANCY LIGHTER THAN AIR GLIDER 审中-公开
标题翻译：可变的BUOYANCY照明器比AIR GLIDER
公开(公告)号：US20160052614A1
公开(公告)日：2016-02-25
申请号：US14835196
申请日：2015-08-25
申请人： Aether Industries, LLC.
发明人： Benjamin Wesley Longmier , John Mark Guthery , John Patrick Sheehan , Benjamin Natan Wachs
IPC分类号： B64B1/02 , G01W1/08 , G05D1/04
CPC分类号： B64B1/02 , B64B2201/00 , G01W1/08 , G05D1/105
摘要： A payload delivery and recovery system, having a payload including a data collection device arranged to collect data, and a controllable ascent vehicle comprising a controllable lighter than air (LTA) mechanism detachably coupled to the payload and used during an ascent phase to deliver the payload to a pre-determined altitude. The payload delivery and recovery system also having a controllable descent mechanism releasably attached to the controllable ascent vehicle and that can be used during a descent phase for reducing a rate of descent of the payload subsequent to release of the payload at the pre-determined altitude and including a control system for navigating the payload to a desired ground location during a recovery phase.
摘要翻译：一种有效载荷递送和恢复系统，其具有包括布置成收集数据的数据收集装置的有效载荷，以及包括可拆卸地耦合到有效载荷并在上升阶段期间用于传递有效载荷的空气（LTA）机构的可控的轻量级车辆到一个预定的高度。有效载荷递送和恢复系统还具有可释放地附接到可控升降车辆的可控下降机构，并且可以在下降阶段期间使用，用于在预定高度释放有效载荷之后降低有效载荷的下降速率，以及包括用于在恢复阶段将有效载荷导航到所需地面位置的控制系统。

45. 发明申请

US20150284065A1 Near-space operation systems 有权
标题翻译：近空操作系统
公开(公告)号：US20150284065A1
公开(公告)日：2015-10-08
申请号：US14188581
申请日：2014-02-24
申请人： WORLD VIEW ENTERPRISES, INC.
发明人： Taber K. MacCallum , Jacob H. Dang , Robert Alan Eustace , John Zaniel Maccagnano , Julian R. Nott , Sebastian A. Padilla , Sreenivasan Shankarnarayan , John Straus
IPC分类号： B64B1/02 , B64D17/64 , B64D17/62 , B64D17/00 , B64D17/22
CPC分类号： B64D17/64 , B64B1/02 , B64B1/40 , B64D10/00 , B64D17/00 , B64D17/22 , B64D17/62 , B64D2010/005 , B64D2010/007
摘要： A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.
摘要翻译：一个能够在极高海拔地区（高于70,000英尺）进行安全人员和无人操作的系统。该系统利用气球发射系统和降落伞和/或parafoil恢复。

46. 发明申请

US20140158823A1 HIGH ALTITUDE BALLOON SYSTEM 有权
标题翻译：高海拔气球系统
公开(公告)号：US20140158823A1
公开(公告)日：2014-06-12
申请号：US13827779
申请日：2013-03-14
申请人： Michael Smith , Kurt Sehnert , Randy Scott , Justin Lee Marsh , Mark L. West
发明人： Michael Smith , Kurt Sehnert , Randy Scott , Justin Lee Marsh , Mark L. West
IPC分类号： B64B1/02 , B29C65/00 , B64B1/70 , B64D45/02 , B64B1/40 , B64B1/44
CPC分类号： B64B1/08 , B64B1/30 , B64B1/42 , B64B1/44 , B64B1/58 , B64B1/70 , B64D45/02 , Y10T156/10
摘要： A high altitude balloon system includes a dual chamber balloon extending from an upper apex to a lower apex with a circumferential edge between the upper and lower apexes. A deflectable diaphragm is within the dual chamber balloon and coupled along the circumferential edge. The deflectable membrane divides the dual chamber balloon into a lift gas chamber formed by an interior surface of the dual chamber balloon and the deflectable diaphragm, and a ballast chamber formed by the interior surface of the dual chamber balloon and the deflectable diaphragm. Optionally, the dual chamber balloon is constructed by interposing the deflectable diaphragm between an upper and lower balloon panels. Each of the upper and lower balloon panels and the deflectable diaphragm are then coupled together along the circumferential edge to form both the lift gas chamber and the ballast chamber.
摘要翻译：高空气球系统包括从上顶点延伸到下顶点的双室气囊，其中上和下顶点之间具有圆周边缘。可偏转隔膜位于双室气囊内并且沿圆周边缘连接。可偏转膜将双室气囊分成由双室气囊和可偏转隔膜的内表面形成的提升气室，以及由双室气囊的内表面和可偏转膜片形成的镇流室。可选地，双室气囊通过将可偏转隔膜插入在上气囊面板和下气囊面板之间来构造。上，下气囊板和可偏转隔膜中的每一个然后沿着圆周边缘连接在一起以形成提升气室和镇流器室。

47. 发明授权

US08678309B2 Lifting gas replenishment in a tethered airship system 有权
标题翻译：在拴系的飞艇系统中提升天然气补给
公开(公告)号：US08678309B2
公开(公告)日：2014-03-25
申请号：US13227966
申请日：2011-09-08
申请人： Stephen Heppe
发明人： Stephen Heppe
IPC分类号： B64B1/02
CPC分类号： B64B1/40 , B64B1/00 , B64B1/50 , B64B1/58
摘要： A system for lifting gas replenishment in a tethered airship system includes an upper airship with a first end of a tether attached to the upper airship. A balloon is configured to travel up the tether toward the upper airship carrying a payload of lifting gas. A method for gas replenishment of an airship is also provided.
摘要翻译：用于在系留式飞艇系统中提升气体补给的系统包括上部飞艇，其具有连接到上部飞艇的系绳的第一端。一个气球被配置成朝着上面的飞艇向上行进，从而携带提升气体的有效载荷。还提供了一种用于补充飞艇的气体的方法。

48. 发明授权

US08448894B2 Method and apparatus for a mobile aerial sustained solar power-plant 失效
公开(公告)号：US08448894B2
公开(公告)日：2013-05-28
申请号：US12455241
申请日：2009-05-28
申请人： Stuart Park LaForge
发明人： Stuart Park LaForge
IPC分类号： B64B1/02 , B64B1/06
CPC分类号： H01M8/0656 , H01M8/184 , H01M2250/405 , H01Q1/248 , H01Q1/28 , Y02B90/16 , Y02E60/528
摘要： The mobile aerial sustained solar power-plant (MASP) provides an improved method and device for the highly efficient collection, storage, transport, and wireless delivery of renewable energy from an airborne platform. This energy can be used to supply electrical power to clients or be used to power directed energy weapons.

49. 发明申请

US20120138733A1 High-Altitude Aerial Vehicle 审中-公开
标题翻译：高空飞行器
公开(公告)号：US20120138733A1
公开(公告)日：2012-06-07
申请号：US13310125
申请日：2011-12-02
申请人： Manfred Hiebl , Hans-Wolfgang Pongratz
发明人： Manfred Hiebl , Hans-Wolfgang Pongratz
IPC分类号： B64B1/02 , B64B1/40
CPC分类号： B64B1/58
摘要： A high-altitude aerial vehicle, in particular an aerial vehicle for the stratosphere that is designed as a non-rigid aerial vehicle with a hull, that has an at least partially inflated envelope with a buoyant gas other than air, which is lighter than air, in particular hydrogen. The hull is provided with at least a first chamber for the buoyant gas and at least a second chamber that can be inflated with air. Between the first and second chambers a flexible partition wall is provided that is preferably formed by a flexible membrane. Inflating of the second chamber, preferably with hot air depending on the flight altitude, can be controlled or regulated in such a way that the envelope of hull is always tautly inflated.
摘要翻译：高空飞行器，特别是用于平流层的空中飞行器，其被设计为具有船体的非刚性空中飞行器，其具有至少部分充气的信封，其具有比空气轻的空气的浮力气体，其比空气轻，特别是氢。船体设置有至少一个用于浮力气体的第一室和至少一个可以用空气充气的第二室。在第一和第二腔室之间设置有优选由柔性膜形成的柔性分隔壁。可以以这样一种方式来控制或调节第二室的膨胀，优选地依赖于飞行高度的热空气，使得船体的外壳总是被张紧地膨胀。

50. 发明授权

US08152092B2 Aerial transporter 失效
标题翻译：空中运输
公开(公告)号：US08152092B2
公开(公告)日：2012-04-10
申请号：US12095385
申请日：2006-12-06
申请人： Rolf Zulkowski , Jürgen Henk , Carl Von Gablenz , Christoph Von Kessel
发明人： Rolf Zulkowski , Jürgen Henk , Carl Von Gablenz , Christoph Von Kessel
IPC分类号： B64B1/02
CPC分类号： B64B1/32 , B64B1/06 , B64B1/08 , B64D1/22
摘要： This invention relates to an aerial transporter comprising rigid cell structures which are covered with light materials as a skin, composed of modules. The invention aerial transporter represents some type of airship without a tail unit as well as an approximate balloon construction comprising a rigid structure and an independent drive unit. Said aerial transporter can transport loads in the range of about 20 t and more over short to medium distances using lighter-than-air technology while meeting air traffic regulations. Furthermore, the disclosed aerial transporter can be used as an air crane in the tied state.
摘要翻译：本发明涉及一种航空运输机，其包括由轻质材料作为皮肤覆盖的刚性电池结构，其由模块组成。本发明的空中运输机代表某种类型的没有尾部单元的飞艇以及包括刚性结构和独立驱动单元的近似气囊结构。所述空中运输机可以在短时间至中等距离的情况下使用轻于空气技术在满足空中交通管制的条件下运输大约20t以上的载荷。此外，公开的空中运输机可以用作捆扎状态的空气起重机。

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