专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

51. 发明申请

US20110267241A1 Multi-Mission Frameless Airship Platform 审中-公开
标题翻译：多任务无框架飞艇平台
公开(公告)号：US20110267241A1
公开(公告)日：2011-11-03
申请号：US13099385
申请日：2011-05-03
申请人： Thomas Grimm , Gregory T. Smedley , Reindy Allendra , Kathryn A. Schubel
发明人： Thomas Grimm , Gregory T. Smedley , Reindy Allendra , Kathryn A. Schubel
IPC分类号： B64B1/02 , B64D1/08 , H01Q1/28 , B25J18/00 , F03D9/00 , B64B1/08 , B64B1/22
CPC分类号： B64B1/58 , B64B1/02 , B64B1/08 , B64B1/22 , B64B1/30 , F03D9/007 , F03D9/25 , F03D9/32 , F03D13/20 , F05B2240/922 , H01Q1/246 , H01Q1/28 , H02S10/12 , Y02E10/728 , Y10T74/20305
摘要： Multi-Mission Frameless Airship Platform (MFAP) leverages composite material science to achieve a frameless lightweight airframe design enabling increased speed, lift and cargo capacity. Deployable/retrievable high-value modules provide enhanced operational and mission flexibility. Unified power electronics enable hybrid integration of propulsion, power generation (e.g. diesel generator, photovoltaic solar, etc.), energy storage and tethered wind-power generation for both on-grid and off-grid electrical power delivery for airborne operations and ground operations. Onboard antenna systems serve as cell phone towers.
摘要翻译：多任务无框架飞艇平台（MFAP）利用复合材料科学实现无框架的轻型机身设计，可提高速度，提升和货物能力。可部署/可检索的高价值模块提供增强的操作和任务灵活性。统一的电力电子技术可实现对空中操作和地面操作的并网和离网电力传输的推进，发电（例如柴油发电机，光伏太阳能等），能量存储和系留式风力发电的混合集成。机载天线系统用作手机塔。

52. 发明授权

US07744032B2 Power and imaging system for an airship 有权
标题翻译：飞艇的动力和成像系统
公开(公告)号：US07744032B2
公开(公告)日：2010-06-29
申请号：US11796493
申请日：2007-04-27
申请人： Edward W. Quinn , Jeanette Hariharan
发明人： Edward W. Quinn , Jeanette Hariharan
IPC分类号： B64B1/02
CPC分类号： H01Q1/248 , B64B1/00 , G01S13/87 , G01S13/88 , G01S13/90 , G01S17/88 , G01S2013/0245 , H01Q1/28 , H01Q9/0407
摘要： A power transmission and imaging system for an airship comprises a transmission antenna array configured to transmit an energy beam to a patch rectenna carried by the airship. Coupled to the patch rectenna is a power distribution and control network that supplies rectified power delivered by the energy beam into the proper format for delivery to a power storage system and a motor control system. The power storage system comprises one or more batteries to store the transmitted energy, while the motor control system powers various propellers, blowers, and valves maintained by the airship in order to descend the airship to the ground. The rectenna may also function as an imaging system in real-time. The image processing system uses the patch rectenna to transmit and receive signals, and in turn store and process the return signals (images).
摘要翻译：用于飞艇的动力传递和成像系统包括：发射天线阵列，被配置为将能量束传输到由飞艇携带的贴片整流天线。耦合到贴片整流天线的是配电和控制网络，其将由能量束传递的整流功率提供给适当的格式以传送到蓄电系统和电动机控制系统。电力存储系统包括一个或多个蓄电池来存储发射的能量，而电动机控制系统为由飞艇维护的各种螺旋桨，鼓风机和阀门提供动力，以将飞艇降落到地面。整流罩也可以实时地用作成像系统。图像处理系统使用贴片整流器来发送和接收信号，并且反过来存储和处理返回信号（图像）。

53. 发明申请

US20090152391A1 Multibody aircrane 失效
标题翻译：多体电极
公开(公告)号：US20090152391A1
公开(公告)日：2009-06-18
申请号：US11713493
申请日：2007-03-02
申请人： Bruce Kimberly McWhirk
发明人： Bruce Kimberly McWhirk
IPC分类号： B64B1/02 , B65G67/60
CPC分类号： B64B1/70 , B64B1/02 , B64B1/06
摘要： The MULTIBODY AIRCRANE performs relative positioning, predictive control, and ballast control to achieve very heavy-lifting tasks on land or sea. Such tasks allow station keeping and precise transfer of very heavy payloads between ships underway. This scalable multibody system features three subcomponents: AIRSHIP, SKYCRANE and LOADFRAME. This semi-autonomous system combines aerodynamic (kinetic) and aerostatic (buoyancy force) lift with efficient power and propulsion. During low-speed flight, the Airship and Skycrane are decoupled but linked via a reelable Tether Control Line. Beneath the Skycrane, centered on its hull, a patented NIST (National Institute of Standards and Technology) RoboCrane (featuring a computer controlled six degrees of freedom (DoF) cabling system,) is attached, to precisely suspend and control a Loadframe, with or without payload. During subsonic forward flight, these Airship and Skycrane are coupled as a single airframe (fuselage and delta wing.)
摘要翻译：多功能飞机执行相对定位，预测控制和镇流器控制，以实现陆上或海上非常重的任务。这些任务允许在船舶之间进行站保持和精确的非常重的有效载荷的传送。这种可扩展的多体系统具有三个子组件：AIRSHIP，SKYCRANE和LOADFRAME。这种半自主系统将空气动力学（动力学）和空气静力（浮力）升力与高效的动力和推进相结合。在低速飞行期间，飞艇和Skycrane是脱钩的，但通过可卷绕的Tether控制线连接。以Skycrane为中心，以其船体为中心，获得专利的NIST（国家标准与技术研究院）RoboCrane（具有计算机控制的六自由度（DoF）布线系统）），以精确地暂停和控制Loadframe，没有有效载荷。在亚音速向前飞行期间，这些飞艇和Skycrane作为单个机身（机身和三角翼）耦合。

54. 发明授权

US07490794B2 Airship having a central fairing to act as a stall strip and to reduce lift 失效
标题翻译：飞艇有一个中央整流罩作为摊位条，并减少电梯
公开(公告)号：US07490794B2
公开(公告)日：2009-02-17
申请号：US11234443
申请日：2005-09-21
申请人： George H. Heaven, Jr.
发明人： George H. Heaven, Jr.
IPC分类号： B64B1/02
CPC分类号： B64B1/06 , B64B1/42
摘要： An airship including a hull having a lenticular shape and a fairing attached to the hull to act as a stall strip and reduce the lift generated by the hull. The hull is symmetrical along a central horizontal plane and the fairing may be positioned along the central horizontal plane. The fairing may have a triangular shape, a semi-circular shape or any other shape capable of disrupting the flow of air over the hull.
摘要翻译：飞艇包括具有透镜形状的船体和附接到船体的整流罩，用作失速条并减少船体产生的升力。船体沿中心水平面对称，整流罩可沿中心水平面定位。整流罩可以具有三角形形状，半圆形形状或能够破坏船体上的空气流的任何其它形状。

55. 发明申请

US20080011900A1 Apparatus and method to control the flight dynamics in a lighter-than-air airship 审中-公开
标题翻译：用于控制轻型飞艇的飞行动力学的装置和方法
公开(公告)号：US20080011900A1
公开(公告)日：2008-01-17
申请号：US11778107
申请日：2007-07-16
申请人： Javier Quintana
发明人： Javier Quintana
IPC分类号： B64B1/02
CPC分类号： B64B1/34 , B64B1/30 , B64C11/006
摘要： An apparatus and method to control the attitude, heading course, altitude and position of a lighter-than-air airship. In one aspect, a hybrid airship including a lighter-than-air gas filled envelope, a thrust vectored front propulsion system, a back rotary wing system and a onboard control system. In one aspect, at least one system to modify the on board mass, a system to control the internal pressure, at least a power battery pack and a radio link communications for unmanned piloting. Said hybrid airship has improved maneuverability, safely flights and is capable to fly as Lighter-than-air airship and Heavy-than-air aircraft.
摘要翻译：一种用于控制轻型飞艇的姿态，航向，高度和位置的装置和方法。一方面，一种混合式飞艇，包括比空气中的气体填充的外壳，推力矢量前推进系统，后旋转翼系统和车载控制系统。在一个方面，至少一个系统来修改船上质量，控制内部压力的系统，至少一个动力电池组和用于无人驾驶的无线电链路通信。所述混合飞艇具有改进的机动性，安全航班，能够作为轻型飞机和重型飞机飞行。

56. 发明申请

US20070267537A1 Internal Support Structure for an Airship 失效
标题翻译：飞艇的内部支援结构
公开(公告)号：US20070267537A1
公开(公告)日：2007-11-22
申请号：US11383996
申请日：2006-05-18
申请人： Daniel Nachbar , Michael Kuehlmuss
发明人： Daniel Nachbar , Michael Kuehlmuss
IPC分类号： B64B1/02
CPC分类号： B64B1/04
摘要： A system and method for internally supporting a flexible envelope such as an airship is described, comprising a truss structure and supporting struts attached to a central support member. The internal structure may be foldable so as to allow the envelope to be collapsed when not in use.
摘要翻译：描述了用于内部支撑诸如飞艇的柔性封套的系统和方法，其包括桁架结构和附接到中央支撑构件的支撑支柱。内部结构可以是可折叠的，以便在不使用时允许信封被折叠。

57. 发明申请

US20070145188A1 Component, particularly a lightweight hybrid component 审中-公开
标题翻译：组件，特别是轻型混合组件
公开(公告)号：US20070145188A1
公开(公告)日：2007-06-28
申请号：US10579905
申请日：2004-11-19
申请人： Gregor Specht
发明人： Gregor Specht
IPC分类号： B64B1/02
CPC分类号： B29C66/1122 , B29C65/00 , B29C65/02 , B29C65/48 , B29C65/56 , B29C65/562 , B29C65/601 , B29C66/112 , B29C66/131 , B29C66/1312 , B29C66/43 , B29C66/532 , B29C66/5346 , B29C66/536 , B29C66/54 , B29C66/549 , B29L2009/003 , B29L2023/22 , B29L2031/003 , B62D25/142 , B62D25/145 , B62D29/001 , B62D29/004 , B62D29/005 , F16L9/003 , F16L9/147 , F16L9/17
摘要： The invention relates to a component (1) comprising a particularly shell-shaped base carrier (2) and at least one core element (6). The aim of the invention is to provide an improved component (1), wherein an intermediate layer (5) is inserted in between the base carrier (2) and the core element (6) in order to compensate tolerances, resulting in a positive power flow via the intermediate layer (4) and improved tolerance compensation.
摘要翻译：本发明涉及一种包括特别是壳状基底载体（2）和至少一个芯元件（6）的部件（1）。本发明的目的是提供一种改进的部件（1），其中中间层（5）插入在基座（2）和芯元件（6）之间，以补偿公差，导致正的功率经由中间层（4）流动并改善了公差补偿。

58. 发明申请

US20070138336A1 LIGHTER-THAN-AIR AIRCRAFT INCLUDING A CLOSED LOOP COMBUSTION GENERATING SYSTEM AND RELATED METHODS FOR POWERING THE SAME 失效
标题翻译：包括封闭式循环燃烧系统的照明装置及其相关方法
公开(公告)号：US20070138336A1
公开(公告)日：2007-06-21
申请号：US10977791
申请日：2004-10-29
申请人： William Palmer
发明人： William Palmer
IPC分类号： B64B1/02
CPC分类号： B64B1/02 , B64B1/14 , B64B1/24
摘要： A lighter-than-air aircraft includes a gas envelope for containing a buoyant gas, and a propulsion system is carried by the gas envelope. A solar panel is carried by the gas envelope for powering the propulsion system when generating sufficient power. A closed loop combustion generating system is also carried by the gas envelope for powering the propulsion system when the solar panel is not generating sufficient power. The fuel for the closed loop combustion generator is regenerated by the solar panel from its exhaust when the solar panel is generating sufficient power.
摘要翻译：一架轻型飞机包括一个用于容纳浮力气体的气体信封，并且一个推进系统由气体信封携带。太阳能电池板由气体封套携带，用于在产生足够的电力时为推进系统供电。当太阳能电池板不产生足够的功率时，闭环燃烧产生系统也由气体封套携带，用于为推进系统供电。当太阳能电池板产生足够的功率时，用于闭环燃烧发生器的燃料由太阳能电池板从其排气再生。

59. 发明申请

US20070075186A1 Airship with lifting gas cell system 有权
标题翻译：具有提升气体细胞系统的飞艇
公开(公告)号：US20070075186A1
公开(公告)日：2007-04-05
申请号：US11241336
申请日：2005-09-30
申请人： Thomas Marimon , Gordon Schmidt , Dennis Carter
发明人： Thomas Marimon , Gordon Schmidt , Dennis Carter
IPC分类号： B64B1/02
CPC分类号： B64B1/60
摘要： An airship with a lifting gas cell system comprises an airship that contains a plurality of partitions and a plurality of diaphragms, wherein the partitions and diaphragms are configured to form a number of gas cells that contain a lifting gas such as helium, and a single air cell that contains air. As a result, during the ascent and descent of the airship the number of gas cells ensures that the lifting gas is uniformly distributed over the entire length of the airship, whereas the air cell allows a large amount of air to be retained during a descent.
摘要翻译：具有提升气室系统的飞艇包括包含多个隔板和多个隔膜的飞艇，其中隔板和隔膜被配置成形成多个包含诸如氦气的提升气体的气室，以及单个空气含有空气的电池。结果，在飞艇的上升和下降期间，气室的数量确保提升气体在飞艇的整个长度上均匀分布，而空气室允许在下降期间保持大量的空气。

60. 发明申请

US20070075184A1 Direct mounted propulsion for non-rigid airships 有权
标题翻译：非刚性飞艇的直接推进
公开(公告)号：US20070075184A1
公开(公告)日：2007-04-05
申请号：US11244383
申请日：2005-10-05
申请人： Thomas Marimon , Jonathan Peritt , James Houmard
发明人： Thomas Marimon , Jonathan Peritt , James Houmard
IPC分类号： B64B1/02
CPC分类号： B64B1/32 , B64B1/02 , B64B1/42
摘要： A propulsion assembly for attachment to the enclosing material of an airship which includes a base which is positioned proximate to the enclosing material. An extension member having opposed ends projects away from the base and includes opposed ends. A motor assembly is attached to the end of the extension member opposed to the base. A mounting assembly is attached to the enclosing material and a plurality of pre-tensioned guy cables connect the mounting assembly to the extension member.
摘要翻译：用于附接到飞艇的封闭材料的推进组件，其包括靠近封闭材料定位的基座。具有相对端的延伸构件从基座突出并且包括相对的端部。电机组件附接到与基座相对的延伸构件的端部。安装组件附接到封闭材料，并且多个预张紧的铠装电缆将安装组件连接到延伸构件。

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