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1. 发明授权

US11128039B2 Cavity antenna with radome 有权
公开(公告)号：US11128039B2
公开(公告)日：2021-09-21
申请号：US16837281
申请日：2020-04-01
申请人： The Boeing Company
发明人： Ronald O. Lavin , Dennis K. McCarthy , Andy H. Lee , Manny S. Urcia
IPC分类号： H01Q1/42 , H01Q7/00 , H01Q9/04
摘要： A method for designing an antenna including defining an operating frequency of an antenna radiating element located within an antenna cavity structure; determining a non-loaded depth of the antenna cavity structure; determining a reduced depth of the antenna cavity structure; determining a reduction factor to reduce the non-loaded depth to the reduced depth; and selecting a dielectric material, at least partially forming a radome structure covering the antenna radiating element, to achieve the reduction factor.

2. 发明申请

US20200067179A1 COMBINED STRUCTURAL AND ELECTRICAL REPAIR FOR MULTIFUNCTIONAL WIDEBAND ARRAYS 审中-公开
公开(公告)号：US20200067179A1
公开(公告)日：2020-02-27
申请号：US16672353
申请日：2019-11-01
申请人： The Boeing Company
发明人： Manny S. Urcia , Andrew S. Niederschulte , Alec Adams
IPC分类号： H01Q1/28
摘要： A system comprising a core, backskin, longitudinal repair core strip, splice clip, and a section of the backskin. The core comprises a plurality of longitudinal core strips and transverse core strips forming a plurality of core cells and the backskin comprises electronics connected to the core and providing electrical functionality enabling the plurality of core cells of the core to function as a phased array antenna aperture. The splice clip connected one of the plurality of longitudinal core strips to the longitudinal repair core strip and the section of the backskin is electrically connected and structurally bonded to the longitudinal repair core strip.

3. 发明授权

US10340584B2 Structural multilayer antenna design and fabrication 有权
公开(公告)号：US10340584B2
公开(公告)日：2019-07-02
申请号：US15671796
申请日：2017-08-08
申请人： The Boeing Company
发明人： Manny S. Urcia , Andrew S. Niederschulte , Alec Adams , Lixin Cai , Timothy J. Luchini , Justin J. Schell
IPC分类号： H01Q1/28 , B64C1/12 , B64C3/26 , H01Q1/12 , H01Q1/40 , H01Q3/26 , H01Q1/38
摘要： A structural panel of an aircraft is constructed with a multiphase antenna embedded inside the structural panel between multiple sheets of fiberglass.

4. 发明授权

US09190727B1 Structural wideband multifunctional aperture manufacturing 有权
标题翻译：结构宽带多功能孔径制造
公开(公告)号：US09190727B1
公开(公告)日：2015-11-17
申请号：US14043563
申请日：2013-10-01
申请人： The Boeing Company
发明人： Manny S. Urcia , Charles W. Manry, Jr. , Joseph A. Marshall, IV , Tai A. Lam , Otis F. Layton
IPC分类号： H01Q1/28 , H01Q5/00
CPC分类号： H01Q21/062 , H01Q1/286 , H01Q9/28
摘要： A structural wideband aperture assembly and methods are presented. A non-conductive structural backsheet comprises electrical vias. A structural egg-crate core comprises a grid of core strips coupled to the non-conductive structural backsheet and is configured substantially perpendicular to the non-conductive structural backsheet around open boxes. A non-structural grid of antenna feed cards is configured substantially perpendicular to the non-conductive structural backsheet and crosses the core strips. A non-structural grid of antenna feed cards comprises intersections configured within the open boxes, and electronic feed-lines aligned with the electrical vias. Antenna array unit cells comprising antenna cards coupled to the non-structural grid of antenna feed cards and configured to fit within the open boxes.
摘要翻译：提出了一种结构化的宽带孔径组件和方法。非导电结构底片包括电气通孔。结构蛋壳芯包括耦合到非导电结构底片的芯条的网格，并且被构造成基本上垂直于围绕打开框的非导电结构底片。天线馈电卡的非结构网格被配置为基本上垂直于非导电结构底片并且穿过芯条。天线馈电卡的非结构网格包括配置在开放框内的交叉点，以及与电气通孔对准的电子馈线。天线阵列单元，其包括耦合到天线馈线卡的非结构网格并且被配置为装配在开放框内的天线卡。

5. 发明授权

US11463166B2 Conformal load bearing distributed sensing arrays 有权
公开(公告)号：US11463166B2
公开(公告)日：2022-10-04
申请号：US16936903
申请日：2020-07-23
申请人： The Boeing Company
发明人： Manny S. Urcia , Jonathan M. St. Clair , Christopher M. La Fata , John G. Castagno , Ordie D. Butterfield , Stephen T. Tyahla , Alec Adams , Lixin Cai
IPC分类号： H04B10/00 , H04B10/112 , H04B10/50 , H04B10/66 , G01S1/00 , H01Q5/22 , G01S17/42 , H04B7/185 , G01S13/42 , H04J14/00 , H01Q1/28
摘要： Systems, methods, and apparatus for an electromagnetic (EM) panel are disclosed. In one or more embodiments, a disclosed electromagnetic (EM) panel comprises an outer skin, an inner skin, a core disposed between the outer skin and the inner skin, and at least one receiver to receive at least one first signal. In at least one embodiment, at least one receiver is disposed within an opening on the outer skin of the EM panel. At least one receiver is an optical sensor(s) and/or a radio frequency (RF) antenna(s). In one or more embodiments, the EM panel further comprises at least one transmitter to transmit at least one second signal. In at least one embodiment, at least one transmitter is disposed within an opening on the outer skin of the EM panel. At least one transmitter is a laser(s) and/or a RF antenna(s).

6. 发明授权

US10756814B2 Conformal load bearing distributed sensing arrays 有权
公开(公告)号：US10756814B2
公开(公告)日：2020-08-25
申请号：US15156237
申请日：2016-05-16
申请人： THE BOEING COMPANY
发明人： Manny S. Urcia , Jonathan M. Saint Clair , Christopher M. La Fata , John G. Castagno , Ordie D. Butterfield , Stephen T. Tyahla , Alec Adams , Lixin Cai
IPC分类号： H04B10/112 , H04B10/50 , H04B10/66 , G01S1/00 , H01Q5/22 , G01S17/42 , H04B7/185 , G01S13/90 , G01S13/42 , H01Q1/28
摘要： Systems, methods, and apparatus for an electromagnetic (EM) panel are disclosed. In one or more embodiments, a disclosed electromagnetic (EM) panel comprises an outer skin, an inner skin, a core disposed between the outer skin and the inner skin, and at least one receiver to receive at least one first signal. In at least one embodiment, at least one receiver is disposed within an opening on the outer skin of the EM panel. At least one receiver is an optical sensor(s) and/or a radio frequency (RF) antenna(s). In one or more embodiments, the EM panel further comprises at least one transmitter to transmit at least one second signal. In at least one embodiment, at least one transmitter is disposed within an opening on the outer skin of the EM panel. At least one transmitter is a laser(s) and/or a RF antenna(s).

7. 发明授权

US10476140B2 Combined structural and electrical repair for multifunctional wideband arrays 有权
公开(公告)号：US10476140B2
公开(公告)日：2019-11-12
申请号：US15069818
申请日：2016-03-14
申请人： The Boeing Company
发明人： Manny S. Urcia , Andrew S. Niederschulte , Alec Adams
IPC分类号： H01Q1/28
摘要： A method for repair of a multifunctional wideband array includes processes and operations of assessing electrical and structural impairment to the multifunctional wideband array; cutting an opening in a superstrate of the multifunctional wideband array to expose an impaired backskin section of a lower electronics assembly of the multifunctional wideband array; replacing the impaired backskin section with a replacement backskin section; and repairing the opening in the superstrate. A system of multifunctional wideband array repair includes a core having longitudinal core strips and transverse core strips; a backskin having electronics connected to the core and providing electrical functionality enabling the core cells of the core to function as a phased array antenna aperture; a number of splice clips connecting longitudinal core strips to longitudinal repair core strips; and a section of the backskin electrically connected and structurally bonded to the repair core strips.

8. 发明申请

US20190190140A1 Cavity Antenna with Radome 审中-公开
公开(公告)号：US20190190140A1
公开(公告)日：2019-06-20
申请号：US15846307
申请日：2017-12-19
申请人： The Boeing Company
发明人： Ronald O. Lavin , Dennis K. McCarthy , Andy H. Lee , Manny S. Urcia
IPC分类号： H01Q1/42 , H01Q9/04 , H01Q7/00
CPC分类号： H01Q1/422 , H01Q7/00 , H01Q9/0485
摘要： An antenna includes an antenna cavity structure that defines an antenna cavity and that has a cavity opening. The antenna also includes an antenna radiating element located within the cavity opening and operable to emit electromagnetic radiation that has a frequency and a wavelength and a radome structure covering the cavity opening. The radome structure includes a dielectric material and defines an antenna window that is transparent to the electromagnetic radiation. Due to the dielectric material of the radome structure, the antenna cavity has a depth less than one-fourth of the wavelength of the electromagnetic radiation and the cavity is filled with a low-dielectric material.

9. 发明授权

US09515373B2 Integrated antenna transceiver for sensor and data transmission on rotating shafts 有权
标题翻译：用于旋转轴上传感器和数据传输的集成天线收发器
公开(公告)号：US09515373B2
公开(公告)日：2016-12-06
申请号：US14019348
申请日：2013-09-05
申请人： The Boeing Company
发明人： Charles W. Manry, Jr. , Manny S. Urcia
IPC分类号： H01Q1/36 , H01Q1/22 , H02J17/00 , H01Q11/08 , H01Q5/40 , H01P1/06
CPC分类号： H01Q1/22 , H01P1/068 , H01Q1/2208 , H01Q1/362 , H01Q5/40 , H01Q11/08 , H02J17/00 , H02J50/20 , H02J50/23 , H02J50/27 , H02J50/40
摘要： A method and system for communication with assemblies comprising shafts (e.g., drive shafts, or other rotating objects) comprising use of helical antenna based components. In this regard, a helical antenna based component may comprise one or more helical antennas surrounding or wound around a shaft, with the one or more helical antennas being electrically decoupled from the shaft, and with the helical antenna based component being configurable to communicate the signals when the shaft is stationary or rotating.
摘要翻译：一种用于与包括轴（例如，驱动轴或其它旋转物体）的组件通信的方法和系统，其包括使用基于螺旋天线的部件。在这方面，基于螺旋天线的部件可以包括围绕轴缠绕或围绕轴缠绕的一个或多个螺旋天线，其中一个或多个螺旋天线与轴电耦合，并且基于螺旋天线的部件可配置为传送信号当轴静止或旋转时。

10. 发明申请

US20150061947A1 INTEGRATED ANTENNA TRANSCEIVER FOR SENSOR AND DATA TRANSMISSION ON ROTATING SHAFTS 有权
标题翻译：用于传感器和数据传输的集成天线收发器
公开(公告)号：US20150061947A1
公开(公告)日：2015-03-05
申请号：US14019348
申请日：2013-09-05
申请人： The Boeing Company
发明人： Charles W. Manry, Jr. , Manny S. Urcia
IPC分类号： H01Q1/22 , H02J17/00 , H01Q1/36
CPC分类号： H01Q1/22 , H01P1/068 , H01Q1/2208 , H01Q1/362 , H01Q5/40 , H01Q11/08 , H02J17/00 , H02J50/20 , H02J50/23 , H02J50/27 , H02J50/40
摘要： A method and system for communication with assemblies comprising shafts (e.g., drive shafts, or other rotating objects) comprising use of helical antenna based components. In this regard, a helical antenna based component may comprise one or more helical antennas surrounding or wound around a shaft, with the one or more helical antennas being electrically decoupled from the shaft, and with the helical antenna based component being configurable to communicate the signals when the shaft is stationary or rotating.
摘要翻译：一种用于与包括轴（例如，驱动轴或其它旋转物体）的组件通信的方法和系统，其包括使用基于螺旋天线的部件。在这方面，基于螺旋天线的部件可以包括围绕轴缠绕或围绕轴缠绕的一个或多个螺旋天线，其中一个或多个螺旋天线与轴电耦合，并且基于螺旋天线的部件可配置为传送信号当轴静止或旋转时。

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