专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US09352820B2 Device mount for an inflatable structure 有权
标题翻译：用于充气结构的设备安装
公开(公告)号：US09352820B2
公开(公告)日：2016-05-31
申请号：US13466415
申请日：2012-05-08
申请人： Robert B. Williams , Kyle W. Maxhimer , Larry L. Lai , Thomas Brennan
发明人： Robert B. Williams , Kyle W. Maxhimer , Larry L. Lai , Thomas Brennan
IPC分类号： B64B1/00 , B64B1/58 , B64B1/14 , H01Q1/12
CPC分类号： B64B1/58 , B64B1/14 , H01Q1/1292
摘要： An inflatable structure mount is used for mounting a device to an inflatable structure. An example is mounting of radar panels to an inflatable structure within an airship. The mount includes the device, and inserts coupled to the back side of the device, which mechanically couple to flexures mounted on the inflatable structure. Some of the flexures may have slotted holes, used in positioning the inserts on the inflatable structure at positions that will allow the flexures to mate with the inserts. A jig or tool may be used as part of the installation process, to locate the flexures at points where they will properly engage the inserts. The flexures may also each face a center point that is underneath the device to be mounted. The flexures may engage the inserts in ways that allow for quick installation and de-installation of devices, and may allow for visual inspection of proper installation.
摘要翻译：可充气结构安装座用于将装置安装到可充气结构上。一个例子是将雷达面板安装到飞艇内的可充气结构中。该安装件包括该装置，以及联接到该装置的后侧的插入件，其机械地联接到安装在该可充气结构上的挠曲件。一些弯曲部可以具有开槽孔，用于将插入件定位在可膨胀结构上的位置，以允许挠曲件与插入件配合。可以使用夹具或工具作为安装过程的一部分，以便在将它们正确接合插入件的位置处定位挠曲件。挠曲件也可以各自面向要安装的装置下方的中心点。挠曲件可以以允许快速安装和拆卸设备的方式接合插入件，并且可以允许目视检查正确的安装。

2. 发明授权

US09306271B1 Integration of antenna structures into balloon envelopes 有权
公开(公告)号：US09306271B1
公开(公告)日：2016-04-05
申请号：US14841894
申请日：2015-09-01
申请人： Google Inc.
发明人： Cliff L. Biffle , Richard Wayne DeVaul , Joshua Weaver , Anton Valdemar Staaf , Eric Teller , Michael Cassidy
IPC分类号： H04B1/06 , H04B1/38 , H01Q1/28 , H01Q9/04 , H04B1/44 , H04B7/185
CPC分类号： H01Q1/286 , H01Q1/1292 , H01Q9/04 , H01Q9/0407 , H01Q9/30 , H04B1/06 , H04B1/44 , H04B7/18502
摘要： Methods and apparatus are disclosed for receiving and transmitting signals at a balloon. Received signals can be received at the balloon, which can include a payload and an envelope. The envelope can include at least a first antenna section and a second antenna section. Both the first and second antenna sections are configured at least to receive the received signals and convey at least the received signals to the payload. The first antenna section can include a first metallization pattern to receive a first type of signal. The second antenna section can include a second metallization pattern to receive a second type of signal, with the first metallization pattern being different from the second metallization pattern.

3. 发明申请

US20140352755A1 RADIO FREQUENCY TRANSPARENT PHOTOVALTIC CELL 有权
标题翻译：无线电频闪透明细胞
公开(公告)号：US20140352755A1
公开(公告)日：2014-12-04
申请号：US14460298
申请日：2014-08-14
申请人： Raytheon Company
发明人： Daniel F. Sievenpiper , Michael Wechsberg , Fangchou Yang
IPC分类号： H01L31/0224 , H01L31/18 , H01L31/042
CPC分类号： H01L31/022441 , H01L31/0224 , H01L31/022425 , H01L31/042 , H01L31/18 , H01Q1/1292 , H01Q1/44 , H01Q15/0013 , Y02E10/50
摘要： A radio frequency transparent photovoltaic cell includes a back contact layer formed of an electrically conductive material, at least one aperture formed in the back contact layer, and at least one photovoltaic cell section disposed on the back contact layer. An airship includes one or more radio frequency antennas disposed in an interior of the airship. One or more radio frequency transparent photovoltaic cells are disposed on an outer surface of the airship.
摘要翻译：射频透明光伏电池包括由导电材料形成的背接触层，形成在背接触层中的至少一个孔和设置在背接触层上的至少一个光伏电池部分。飞艇包括设置在飞艇内部的一个或多个射频天线。一个或多个射频透明光伏电池设置在飞艇的外表面上。

4. 发明授权

US08274446B2 Lightweight antenna attachment structure 有权
标题翻译：轻便天线附件结构
公开(公告)号：US08274446B2
公开(公告)日：2012-09-25
申请号：US12793448
申请日：2010-06-03
申请人： Kyle W. Maxhimer , David T. Winslow , Larry L. Lai , Derek Pruden
发明人： Kyle W. Maxhimer , David T. Winslow , Larry L. Lai , Derek Pruden
IPC分类号： H01Q1/12 , H01Q21/00
CPC分类号： H01Q1/1292 , Y10T156/10
摘要： The present invention relates to lightweight antenna arrays and more particularly to an attachment mechanism for attaching a lightweight antenna array to a structure. In one embodiment, an antenna structure includes a platform having a first coefficient of thermal expansion; an antenna panel having a second coefficient of thermal expansion different from the first coefficient, and having first and second opposite ends; and a support structure mounting the panel to the platform. The support structure includes a first spacer element with a first height at the first end of the panel, and a second spacer element with a second height less than the first height between the first and second ends of the panel; a first adhesive layer adhering each spacer element to the platform; and a second adhesive layer adhering each spacer element to the antenna panel. A yield strength of the adhesive layers is less than a yield strength of the spacer elements.
摘要翻译：本发明涉及轻质天线阵列，更具体地说，涉及一种用于将轻型天线阵列附接到结构的附接机构。在一个实施例中，天线结构包括具有第一热膨胀系数的平台; 天线面板，其具有与所述第一系数不同的第二热膨胀系数，并且具有第一和第二相对端; 以及将面板安装到平台的支撑结构。支撑结构包括在面板的第一端处具有第一高度的第一间隔元件和具有小于面板的第一和第二端之间的第一高度的第二高度的第二间隔元件; 将每个间隔元件粘附到平台上的第一粘合剂层; 以及将每个间隔元件粘附到天线面板上的第二粘合剂层。粘合剂层的屈服强度小于间隔元件的屈服强度。

5. 发明申请

US20100097277A1 Airship mounted array 有权
标题翻译：飞艇安装阵列
公开(公告)号：US20100097277A1
公开(公告)日：2010-04-22
申请号：US12462709
申请日：2009-08-07
申请人： Jar J. Lee , Clifton Quan , Stanley W. Livingston
发明人： Jar J. Lee , Clifton Quan , Stanley W. Livingston
IPC分类号： H01Q1/28
CPC分类号： H01Q1/1292 , H01Q1/286 , H01Q3/46 , H01Q5/42 , H01Q21/0018
摘要： A space-fed conformal array for a high altitude airship includes a primary array lens assembly adapted for conformal mounting to a non-planar airship surface. The lens assembly includes a first set of radiator elements and a second set of radiator elements, the first set and the second set spaced apart by a spacing distance. The first set of radiators faces outwardly from the airship surface to provide a radiating aperture. The second set of radiators faces inwardly toward an inner space of the airship, for illumination by a feed array spaced from the second set of radiators.
摘要翻译：用于高空飞艇的空间馈电保形阵列包括适于安装到非平面飞艇表面的主阵列透镜组件。透镜组件包括第一组散热器元件和第二组散热器元件，第一组和第二组间隔开间隔距离。第一组散热器从飞艇表面向外面向外提供辐射孔。第二组散热器向内朝向飞艇的内部空间，用于通过与第二组散热器间隔开的进给阵列进行照明。

6. 发明授权

US3171128A Emergency antenna having balloon means to erect antenna automatically in response to impact or immersion 失效
标题翻译：具有气球装置的紧急天线响应于冲击或浸没自动竖立天线
公开(公告)号：US3171128A
公开(公告)日：1965-02-23
申请号：US23625362
申请日：1962-11-08
申请人： MYRON W NIXON , FRANK HOWARD JR , FRANK S HERTZIG
发明人： SHATTUCK OWEN M
IPC分类号： H01Q1/12 , H01Q1/34
CPC分类号： H01Q1/1292 , H01Q1/34 , Y10S116/09

7. 发明授权

US3045952A Antenna support structure 失效
标题翻译：天线支撑结构
公开(公告)号：US3045952A
公开(公告)日：1962-07-24
申请号：US80116859
申请日：1959-03-23
申请人： UNDERWOOD LAWRENCE E
发明人： UNDERWOOD LAWRENCE E
IPC分类号： H01Q1/12
CPC分类号： H01Q1/1292

8. 发明授权

US09153854B1 Integration of antenna structures into balloon envelopes 有权
标题翻译：将天线结构集成到气球信封中
公开(公告)号：US09153854B1
公开(公告)日：2015-10-06
申请号：US13712618
申请日：2012-12-12
申请人： Google Inc.
发明人： Cliff L. Biffle , Richard Wayne DeVaul , Joshua Weaver , Anton Valdemar Staaf , Eric Teller , Michael Cassidy
IPC分类号： B64B1/40 , H01Q1/12 , H04B1/06 , H04B1/38
CPC分类号： H01Q1/286 , H01Q1/1292 , H01Q9/04 , H01Q9/0407 , H01Q9/30 , H04B1/06 , H04B1/44 , H04B7/18502
摘要： Methods and apparatus are disclosed for receiving and transmitting signals at a balloon. Received signals can be received at the balloon, which can include a payload and an envelope. The envelope can include at least a first antenna section and a second antenna section. Both the first and second antenna sections are configured at least to receive the received signals and convey at least the received signals to the payload. The first antenna section can include a first metallization pattern to receive a first type of signal. The second antenna section can include a second metallization pattern to receive a second type of signal, with the first metallization pattern being different from the second metallization pattern.
摘要翻译：公开了用于在气球处接收和发送信号的方法和装置。可以在气球处接收接收的信号，其可以包括有效载荷和信封。信封可以包括至少第一天线部分和第二天线部分。第一和第二天线部分都被配置为至少接收接收到的信号并且将至少接收到的信号传送到有效载荷。第一天线部分可以包括用于接收第一类型的信号的第一金属化图案。第二天线部分可以包括第二金属化图案以接收第二类型的信号，其中第一金属化图案不同于第二金属化图案。

9. 发明授权

US07605767B2 Space-fed array operable in a reflective mode and in a feed-through mode 有权
标题翻译：空间馈送阵列可在反射模式和馈通模式下操作
公开(公告)号：US07605767B2
公开(公告)日：2009-10-20
申请号：US11499591
申请日：2006-08-04
申请人： Jar J. Lee , Clifton Quan , Stanley W. Livingston
发明人： Jar J. Lee , Clifton Quan , Stanley W. Livingston
IPC分类号： H01Q19/06
CPC分类号： H01Q21/0018 , H01Q1/1292 , H01Q1/28 , H01Q1/286 , H01Q3/46 , H01Q5/42
摘要： A space-fed array is selectively operable in a reflective mode or in a feed-through mode. The array includes, in an exemplary embodiment, a primary array; and a feed array. The primary array includes a first side set of radiating elements, a first set of phase shifters, a set of switches, a second set of phase shifters and a second side set of radiating elements. Each of the switches is connected between corresponding ones of the first set and the second set of phase shifters and ground, selectively settable at an open position or at a closed position. The open position corresponds to the feed through mode, and the closed position corresponds to the reflective mode.
摘要翻译：空间馈送阵列可选择性地以反射模式或馈通模式操作。在示例性实施例中，阵列包括主阵列; 和馈送数组。主阵列包括第一组辐射元件，第一组移相器，一组开关，第二组移相器和第二侧辐射元件组。每个开关连接在第一组和第二组移相器的对应的开关和地之间，可选择地设置在打开位置或关闭位置。打开位置对应于进给模式，关闭位置对应于反射模式。

10. 发明授权

US06816114B1 System for polarization tilting and main beam steering of airship antenna using GPS 失效
标题翻译：使用GPS的飞艇天线的偏振倾斜和主波束转向系统
公开(公告)号：US06816114B1
公开(公告)日：2004-11-09
申请号：US10743410
申请日：2003-12-23
申请人： Sangman Moon , Hyounkyoung Kim , Inkyu Kim , Sangjong Lee , Taesik Kim , Haechang Lee , Chanhong Yeom
发明人： Sangman Moon , Hyounkyoung Kim , Inkyu Kim , Sangjong Lee , Taesik Kim , Haechang Lee , Chanhong Yeom
IPC分类号： H01Q300
CPC分类号： H04B7/10 , G01S19/14 , G01S19/51 , H01Q1/1292 , H01Q1/28
摘要： The present invention relates to a system for tilting polarization and steering main beam of airship antenna comprises: a 1st GPS receiver, which is located in the airship; a 2nd GPS receiver, which is located in the ground station; an airship antenna database for extracting the radiation pattern information of airship antenna and polarization information according to the posture of the antenna based on the position information of the airship; a ground station antenna database for extracting the radiation pattern information of ground station antenna and polarization information according to the posture of the antenna based on the position information of the ground station; a polarization and main beam direction correction operating device for computing the correction value of polarization and main beam direction of the airship antenna and the ground station antenna based on the position information of the airship and the ground station received from the 1st GPS receiver and the 2nd GPS receiver; and an airship antenna controller for correcting the posture of the airship antenna by controlling tilting the polarization and steering the main beam direction of the airship antenna based on the corrected value received from the polarization and main beam direction correction operating device.
摘要翻译：本发明涉及一种用于倾斜偏航的飞行器天线的转向主梁的系统，包括：位于飞艇中的第一GPS接收器; GPS接收器位于地面站; 飞艇天线数据库，用于根据飞艇的位置信息，根据天线的姿势提取飞艇天线的辐射图案信息和偏振信息; 地面站天线数据库，用于根据地面站的位置信息，根据天线的姿势提取地面站天线的辐射图案信息和偏振信息; 基于从第1台GPS接收机接收的飞艇和地面站的位置信息，计算飞艇天线和地面站天线的偏振和主波束方向的校正值的偏振和主波束方向校正操作装置和2号GPS接收机; 以及飞艇天线控制器，用于通过基于从偏振光束方向校正操作装置接收到的校正值控制飞越天线的偏振和主飞轮方向的倾斜来校正飞艇天线的姿势。

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