公开(公告)号：EP3178966B1

公开(公告)日：2018-12-12

申请号：EP16192107.7

申请日：2016-10-03

申请人： The Boeing Company ,  General Nano, LLC

发明人： Braley, Daniel J. ,  Belk, John H. ,  Battat, Jacob I. ,  Truscello, Justine M. ,  Ferriell, Daniel R. ,  Sprengard, Joseph ,  Christy, Larry

IPC分类号： C23C28/00 ,  C23C24/08 ,  C01B32/168 ,  B64C3/20

CPC分类号： B05D3/12 ,  B05D1/02 ,  B05D1/30 ,  B05D3/0254 ,  B32B3/266 ,  B32B5/022 ,  B32B5/024 ,  B32B5/026 ,  B32B5/16 ,  B32B5/24 ,  B32B5/26 ,  B32B9/007 ,  B32B9/041 ,  B32B9/047 ,  B32B15/02 ,  B32B15/14 ,  B32B15/20 ,  B32B2250/05 ,  B32B2255/02 ,  B32B2255/06 ,  B32B2255/205 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/02 ,  B32B2262/0261 ,  B32B2262/0269 ,  B32B2262/0276 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2262/14 ,  B32B2307/202 ,  B32B2307/204 ,  B32B2307/206 ,  B32B2307/212 ,  B32B2307/584 ,  B32B2307/712 ,  B32B2307/718 ,  B32B2605/18 ,  B64C3/20 ,  C01B32/168 ,  C23C24/08 ,  C23C28/00 ,  C23C28/322 ,  C23C28/34 ,  C23C28/42

摘要： A carbon nanomaterial composite sheet 202 and a method for making a carbon nanomaterial composite sheet 202 may include a layer of a carbon nanomaterial structure 242 being bonded to a carrier layer 204, the carrier layer 204 being fabricated from a porous metalized nonwoven material.

公开(公告)号：EP3967426A1

公开(公告)日：2022-03-16

申请号：EP21195474.8

申请日：2021-09-08

申请人： The Boeing Company

发明人： MacDonald, Elaine ,  Cochran, Russell W. ,  Braley, Daniel J.

IPC分类号： B22F3/02 ,  B22F3/093 ,  B22F10/14 ,  B22F10/50 ,  B22F12/60 ,  B33Y10/00 ,  B33Y30/00

摘要： A method of additively manufacturing an object (130) includes successively forming a plurality of powder layers (114) by depositing powder (104) over a build platform (112) using a powder-deposition apparatus (102). The method also includes successively forming a binder shell (116) by bonding select regions of each one of the plurality of powder layers (114) before forming each successive one of the plurality of powder layers (114) using a binder-delivery apparatus (106). The binder shell (116) encloses a portion of the powder (104). The method further includes densifying the portion of the powder (104) bound by the binder shell (116) using a consolidation apparatus (118).

公开(公告)号：EP3909749A1

公开(公告)日：2021-11-17

申请号：EP21161858.2

申请日：2021-03-10

申请人： The Boeing Company

发明人： MacDonald, Elaine ,  Braley, Daniel J.

IPC分类号： B29C64/153 ,  B29C64/165 ,  B29C64/209 ,  B29C64/218 ,  B29C64/40 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y70/10 ,  B29C64/336 ,  B22F10/00 ,  B22F12/00

摘要： A method (1000) of additively manufacturing an object (100) includes steps of: 1) selectively depositing build powder (102) inside of a build contour (112) of the object (100) to form a build-powder section (108) of a powder layer (106); and 2) selectively depositing support powder (104) outside of the build contour (112) to form a support-powder section (110) of the powder layer (106). According to the method (1000), the build powder (102) includes a build-powder composition, the support powder (104) includes a support-powder composition, and the build-powder composition and the support-powder composition are different.

公开(公告)号：EP3486081A1

公开(公告)日：2019-05-22

申请号：EP18195539.4

申请日：2018-09-19

申请人： The Boeing Company

发明人： Braley, Daniel J. ,  Karty, Janice L.

IPC分类号： B32B5/02 ,  B32B7/08 ,  B32B37/00 ,  F16J15/08 ,  H05K9/00

摘要： A carbon nanomaterial composite sheet and a method for making a carbon nanomaterial composite sheet may include a layer of a carbon nanomaterial structure (504) being bonded to a carrier layer (502), the carrier layer (502) being fabricated from a porous metalized nonwoven material. (Fig. 13)

公开(公告)号：EP3892411A1

公开(公告)日：2021-10-13

申请号：EP21156232.7

申请日：2021-02-10

申请人： The Boeing Company

发明人： Braley, Daniel J. ,  Wegge, Brandon Heath ,  MacDonald, Elaine

IPC分类号： B23K11/00 ,  B23K11/30 ,  B23K11/34 ,  B23K13/01 ,  B33Y80/00

摘要： An article comprising additively manufactured metal portions is described. The article comprises a first additively manufactured metal portion, and a second additively manufactured metal portion coupled to the first additively manufactured metal portion at a welded joint. The article further comprises a resistive heating material disposed within an interior of the welded joint, the resistive heating material comprising a different material than the first additively manufactured metal portion and the second additively manufactured metal portion.

公开(公告)号：EP3739082A1

公开(公告)日：2020-11-18

申请号：EP20161456.7

申请日：2020-03-06

申请人： The Boeing Company

发明人： Braley, Daniel J. ,  Wilson, Peter A.

IPC分类号： C23C24/00 ,  B05B7/00 ,  C23C24/08 ,  C23C30/00

摘要： A method (100) for fabricating an electrical conductor (304) on a substrate (302) by cold spraying includes propelling (102) a solid powder composition that includes copper and highly oriented pyrolytic graphite using a gas propellant, and directing (106) the solid powder composition towards the substrate (302) at a velocity sufficient to cause the solid powder composition to undergo plastic deformation and to adhere to the substrate (302) to deposit the electrical conductor (304) thereon.

公开(公告)号：EP3498593A1

公开(公告)日：2019-06-19

申请号：EP18200756.7

申请日：2018-10-16

申请人： The Boeing Company

发明人： Braley, Daniel J. ,  LYONS, Brett Ian ,  Gonze, Thomas J. ,  Tucker, Trevor E. ,  Wick, Janet M. ,  Deck, Eric E. ,  Peters, Garrett B. ,  Williams, Nicole R. ,  Bauer, Andrew L.

IPC分类号： B64C1/36 ,  B64C3/26 ,  B64C5/06 ,  B33Y80/00 ,  B33Y10/00

摘要： Core structures (120) for composite panels (75) of an aircraft (10), composite panels (75) and aircraft (10) including the core structures (120), and methods (200) of manufacturing the composite panels (75) are disclosed herein. The core structures (120) include a first side (140), a second side (150), and a connecting region (160) that interconnects an upper portion (142) of the first side (140) with an upper portion (152) of the second side (150). The first side (140), the second side (150), and the connecting region (160) at least partially define an antenna housing (62), which defines a housing volume (64) configured to contain an aircraft antenna (60) of the aircraft (10), and an electromagnetic wave transmission region (66) configured to permit electromagnetic waves to pass therethrough. The electromagnetic wave transmission region (66) defines a plurality of kite-shaped voids (130) arranged in a repeating pattern and bounded by a corresponding plurality of walls (170), at least 10% of which extends at least substantially perpendicular to a surface (122/124) that bounds the electromagnetic wave transmission region (66).

公开(公告)号：EP3178966A1

公开(公告)日：2017-06-14

申请号：EP16192107.7

申请日：2016-10-03

申请人： The Boeing Company

发明人： Braley, Daniel J. ,  Belk, John H. ,  Battat, Jacob I. ,  Truscello, Justine M. ,  Ferriell, Daniel R. ,  Sprengard, Joseph ,  Christy, Larry

IPC分类号： C23C24/08 ,  C23C28/00

CPC分类号： B05D3/12 ,  B05D1/02 ,  B05D1/30 ,  B05D3/0254 ,  B32B3/266 ,  B32B5/022 ,  B32B5/024 ,  B32B5/026 ,  B32B5/16 ,  B32B5/24 ,  B32B5/26 ,  B32B9/007 ,  B32B9/041 ,  B32B9/047 ,  B32B15/02 ,  B32B15/14 ,  B32B15/20 ,  B32B2250/05 ,  B32B2255/02 ,  B32B2255/06 ,  B32B2255/205 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/02 ,  B32B2262/0261 ,  B32B2262/0269 ,  B32B2262/0276 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2262/14 ,  B32B2307/202 ,  B32B2307/204 ,  B32B2307/206 ,  B32B2307/212 ,  B32B2307/584 ,  B32B2307/712 ,  B32B2307/718 ,  B32B2605/18 ,  B64C3/20 ,  C01B32/168 ,  C23C24/08 ,  C23C28/00 ,  C23C28/322 ,  C23C28/34 ,  C23C28/42

摘要： A carbon nanomaterial composite sheet 202 and a method for making a carbon nanomaterial composite sheet 202 may include a layer of a carbon nanomaterial structure 242 being bonded to a carrier layer 204, the carrier layer 204 being fabricated from a porous metalized nonwoven material.

摘要翻译： 碳纳米材料复合片202和用于制造碳纳米材料复合片202的方法可以包括结合到载体层204的碳纳米材料结构层242，载体层204由多孔金属化非织造材料制成。