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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
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.
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公开(公告)号：US20170264007A1
公开(公告)日：2017-09-14
申请号：US15069818
申请日：2016-03-14
申请人： The Boeing Company
IPC分类号： H01Q1/28
CPC分类号： H01Q1/286 , H01Q21/0006 , H01Q21/0087 , H01Q21/061
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.
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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
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.
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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
摘要： A structural panel of an aircraft is constructed with a multiphase antenna embedded inside the structural panel between multiple sheets of fiberglass.
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5.发明申请公开(公告)号：US20200094471A1
公开(公告)日：2020-03-26
申请号：US16139320
申请日：2018-09-24
申请人： THE BOEING COMPANY
IPC分类号： B29C64/135 , B29C64/268 , B22F3/105 , B29C64/393
摘要： An additively-manufactured component includes a main body, and at least one stiffening member. Each of the main body and the stiffening member(s) is additively manufactured layer-by-layer in a common build direction. A method of forming an additively-manufactured component includes forming a main body and at least one stiffening member of the additively-manufactured component layer-by-layer in a common build direction.
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公开(公告)号：US20190051976A1
公开(公告)日：2019-02-14
申请号：US15671796
申请日：2017-08-08
申请人： The Boeing Company
发明人： Manny S. Urcia, JR. , Andrew S. Niederschulte , Alec Adams , Lixin Cai , Timothy J. Luchini , Justin J. Schell
摘要： A structural panel of an aircraft is constructed with a multiphase antenna embedded inside the structural panel between multiple sheets of fiberglass.
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