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公开(公告)号:US09899732B2
公开(公告)日:2018-02-20
申请号:US15342094
申请日:2016-11-02
申请人: The Boeing Company
发明人: Manny S. Urcia, Jr. , Alec Adams , Edward V. White
摘要: A reconfigurable antenna is provided having a liquid metal in contact with an electrolyte with the liquid metal being in a first configuration. A plurality of electrodes includes a first electrode in contact with the liquid metal and a second electrode in contact with the electrolyte. A voltage source connected across the first and second electrodes applies a voltage of a predetermined magnitude and a predetermined polarity in order to move the liquid metal from the first configuration to a second configuration and to measure resultant current flow and modify the applied voltage based on the resultant current flow. Cessation of the applied voltage locks the liquid metal in this second configuration.
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公开(公告)号:US10686254B2
公开(公告)日:2020-06-16
申请号:US15609851
申请日:2017-05-31
申请人: The Boeing Company
发明人: Lixin Cai , Alec Adams , Manny S. Urcia, Jr.
摘要: A system, method, and apparatus for an antenna system. The antenna system comprises an aperture structure, a primary radiating slot, a tuning slot, and a stripline feed. The primary radiating slot and the tuning slot are both located in the aperture structure. The stripline feed is located between the primary radiating slot and the tuning slot in the aperture structure.
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公开(公告)号:US20180366831A1
公开(公告)日:2018-12-20
申请号:US15609851
申请日:2017-05-31
申请人: The Boeing Company
发明人: Lixin Cai , Alec Adams , Manny S. Urcia, Jr.
摘要: A system, method, and apparatus for an antenna system. The antenna system comprises an aperture structure, a primary radiating slot, a tuning slot, and a stripline feed. The primary radiating slot and the tuning slot are both located in the aperture structure. The stripline feed is located between the primary radiating slot and the tuning slot in the aperture structure.
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公开(公告)号:US11260957B2
公开(公告)日:2022-03-01
申请号:US16265443
申请日:2019-02-01
申请人: The Boeing Company
发明人: John Cleveland Waldrop, III , Manny S. Urcia, Jr. , Robert Ray Johnson , Samuel Jerome Huhman , Xue Liu , William A. Lamey, III , Anthony Roberts , Lucian Woods
IPC分类号: B64C7/00
摘要: Rupture fairings are disclosed. A disclosed example fairing for use with an aircraft includes a surface to at least partially define an exterior surface of the aircraft when the fairing is installed onto the aircraft, and a membrane to rupture during flight of the aircraft, where the membrane defines at least a portion of the exterior surface.
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