BR0212086A - Estrutura de rede de antenas de fenda de cavidade de radiação longitudinal e método de formação - Google Patents

Estrutura de rede de antenas de fenda de cavidade de radiação longitudinal e método de formação

Info

Publication number
BR0212086A
BR0212086A BR0212086-0A BR0212086A BR0212086A BR 0212086 A BR0212086 A BR 0212086A BR 0212086 A BR0212086 A BR 0212086A BR 0212086 A BR0212086 A BR 0212086A
Authority
BR
Brazil
Prior art keywords
electrically conductive
network structure
composite material
radiation cavity
longitudinal radiation
Prior art date
Application number
BR0212086-0A
Other languages
English (en)
Inventor
Arnold L Ferreri
Dominic Anton
Leonard Poveromo
Original Assignee
Northrop Grumman Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Northrop Grumman Corp filed Critical Northrop Grumman Corp
Publication of BR0212086A publication Critical patent/BR0212086A/pt

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H01Q1/286—Adaptation for use in or on aircraft, missiles, satellites, or balloons substantially flush mounted with the skin of the craft
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H01Q1/286—Adaptation for use in or on aircraft, missiles, satellites, or balloons substantially flush mounted with the skin of the craft
    • H01Q1/287—Adaptation for use in or on aircraft, missiles, satellites, or balloons substantially flush mounted with the skin of the craft integrated in a wing or a stabiliser
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • H01Q13/10—Resonant slot antennas
    • H01Q13/18—Resonant slot antennas the slot being backed by, or formed in boundary wall of, a resonant cavity ; Open cavity antennas
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/0087—Apparatus or processes specially adapted for manufacturing antenna arrays

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Manufacturing & Machinery (AREA)
  • Details Of Aerials (AREA)
  • Waveguide Aerials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

"ESTRUTURA DE REDE DE ANTENAS DE FENDA DE CAVIDADE DE RADIAçãO LONGITUDINAL E MéTODO DE FORMAçãO". De acordo com uma concretização da invenção, uma estrutura de rede de antenas de fenda de cavidade de radiação longitudinal inclui um revestimento superior formado de um material composto correspondendo a uma porção de uma superfície externa da asa do avião, um revestimento inferior formado de um material composto correspondendo a uma porção de uma superfície interna da asa do avião e uma pluralidade de elementos eletricamente condutores, posicionados proximamente, dispostos entre os revestimentos superior e inferior. Cada elemento eletricamente condutor é formado de pelo menos uma folha de material composto tendo uma superfície eletricamente condutora e a folha de material composto é configurada de modo que a superfície eletricamente condutora define uma superfície interna do elemento eletricamente condutor e quaisquer superfícies externas do elemento eletricamente condutor que estejam em contado com um elemento eletricamente condutor adjacente.
BR0212086-0A 2001-08-20 2002-08-15 Estrutura de rede de antenas de fenda de cavidade de radiação longitudinal e método de formação BR0212086A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/933,595 US6496151B1 (en) 2001-08-20 2001-08-20 End-fire cavity slot antenna array structure and method of forming
PCT/US2002/026046 WO2003017419A1 (en) 2001-08-20 2002-08-15 End-fire cavity slot antenna array structure and method of forming

Publications (1)

Publication Number Publication Date
BR0212086A true BR0212086A (pt) 2004-09-28

Family

ID=25464214

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0212086-0A BR0212086A (pt) 2001-08-20 2002-08-15 Estrutura de rede de antenas de fenda de cavidade de radiação longitudinal e método de formação

Country Status (7)

Country Link
US (1) US6496151B1 (pt)
EP (1) EP1419551A1 (pt)
JP (1) JP2005500774A (pt)
BR (1) BR0212086A (pt)
CA (1) CA2458109A1 (pt)
IL (1) IL160431A0 (pt)
WO (1) WO2003017419A1 (pt)

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US7397429B2 (en) * 2004-03-09 2008-07-08 Northrop Grumman Corporation Aircraft window plug antenna assembly
US7737898B2 (en) * 2007-03-01 2010-06-15 L-3 Communications Integrated Systems, L.P. Very high frequency line of sight winglet antenna
US8201773B1 (en) 2008-07-02 2012-06-19 The United States Of America As Represented By Secretary Of The Navy Flexible self-erecting substructures for sensor networks
US8025752B2 (en) * 2009-02-18 2011-09-27 Raytheon Company Method of fabricating conductive composites
KR20120113210A (ko) 2009-09-09 2012-10-12 에어로바이론먼트, 인크. 휴대용 ｒｆ 투명 발사관을 구비한 원격 조종 무인 항공기 포성 억제 발사장치를 위한 시스템 및 장치
US9270016B2 (en) * 2011-07-15 2016-02-23 The Boeing Company Integrated antenna system
US9705185B2 (en) * 2013-04-11 2017-07-11 Raytheon Company Integrated antenna and antenna component
KR101677984B1 (ko) * 2015-04-22 2016-11-21 국방과학연구소 비행체 날개를 이용한 슬롯 안테나
US10046666B2 (en) * 2015-11-05 2018-08-14 Ningbo Wise Digital Technology Co., Ltd Vehicle comprising a bifunctional structural part
US10020590B2 (en) 2016-07-19 2018-07-10 Toyota Motor Engineering & Manufacturing North America, Inc. Grid bracket structure for mm-wave end-fire antenna array
US10333209B2 (en) 2016-07-19 2019-06-25 Toyota Motor Engineering & Manufacturing North America, Inc. Compact volume scan end-fire radar for vehicle applications
CN106428522A (zh) * 2016-09-26 2017-02-22 华东电子工程研究所（中国电子科技集团公司第三十八研究所） 传感器飞行器、基于所述传感器飞行器的扫描系统与方法
US10141636B2 (en) 2016-09-28 2018-11-27 Toyota Motor Engineering & Manufacturing North America, Inc. Volumetric scan automotive radar with end-fire antenna on partially laminated multi-layer PCB
US9917355B1 (en) 2016-10-06 2018-03-13 Toyota Motor Engineering & Manufacturing North America, Inc. Wide field of view volumetric scan automotive radar with end-fire antenna
US10401491B2 (en) 2016-11-15 2019-09-03 Toyota Motor Engineering & Manufacturing North America, Inc. Compact multi range automotive radar assembly with end-fire antennas on both sides of a printed circuit board
US10585187B2 (en) 2017-02-24 2020-03-10 Toyota Motor Engineering & Manufacturing North America, Inc. Automotive radar with end-fire antenna fed by an optically generated signal transmitted through a fiber splitter to enhance a field of view
KR102086388B1 (ko) * 2018-10-25 2020-03-09 주식회사 한화 안테나 일체형 날개 구조체 및 이를 구비한 유도무기
CN112928427A (zh) * 2019-12-06 2021-06-08 中国空空导弹研究院 翼面共形可调倒f型振子天线及其设计方法
CN112606992B (zh) * 2021-02-04 2022-04-29 中国电子科技集团公司第三十八研究所 一种具有蒙皮天线的一体化飞机机身
US11342687B1 (en) * 2021-04-20 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Endfire antenna structure on an aerodynamic system
CN113809534A (zh) * 2021-09-18 2021-12-17 中国电子科技集团公司第三十八研究所 一种超宽带宽波束嵌入式端射蒙皮天线
CN114267935B (zh) * 2021-12-14 2023-11-07 重庆交通大学绿色航空技术研究院 应用于无人飞行器的双向通信阵列天线以及通信方法

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Also Published As

Publication number Publication date
WO2003017419A1 (en) 2003-02-27
JP2005500774A (ja) 2005-01-06
US6496151B1 (en) 2002-12-17
EP1419551A1 (en) 2004-05-19
IL160431A0 (en) 2004-07-25
CA2458109A1 (en) 2003-02-27

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 6A,7A E 8A ANUIDADES.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2060 DE 29/06/2010.