JP7401221B2 - 構造荷重を支持するための伸長構造物、伸長構造物を伴う構造アセンブリ、及び方法 - Google Patents

構造荷重を支持するための伸長構造物、伸長構造物を伴う構造アセンブリ、及び方法 Download PDF

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JP7401221B2
JP7401221B2 JP2019145894A JP2019145894A JP7401221B2 JP 7401221 B2 JP7401221 B2 JP 7401221B2 JP 2019145894 A JP2019145894 A JP 2019145894A JP 2019145894 A JP2019145894 A JP 2019145894A JP 7401221 B2 JP7401221 B2 JP 7401221B2
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web
elongated
height
elongated structure
examples
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JP2020050332A (ja
JP2020050332A5 (enExample
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ケネス エイチ． グリース，
カレン ディー． マッケンジー，
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Boeing Co
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Boeing Co
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Supports For Pipes And Cables (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Laminated Bodies (AREA)
JP2019145894A 2018-08-08 2019-08-08 構造荷重を支持するための伸長構造物、伸長構造物を伴う構造アセンブリ、及び方法 Active JP7401221B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US16/058,230 2018-08-08
US16/058,230 US11312468B2 (en) 2018-08-08 2018-08-08 Elongate structures, structural assemblies with elongate structures, and methods for supporting a structural load

Publications (3)

Publication Number Publication Date
JP2020050332A JP2020050332A (ja) 2020-04-02
JP2020050332A5 JP2020050332A5 (enExample) 2023-08-18
JP7401221B2 true JP7401221B2 (ja) 2023-12-19

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JP2019145894A Active JP7401221B2 (ja) 2018-08-08 2019-08-08 構造荷重を支持するための伸長構造物、伸長構造物を伴う構造アセンブリ、及び方法

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Country Link
US (1) US11312468B2 (enExample)
EP (1) EP3608218B1 (enExample)
JP (1) JP7401221B2 (enExample)
CN (1) CN110816807B (enExample)
CA (1) CA3042655C (enExample)

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* Cited by examiner, † Cited by third party
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US11447228B2 (en) * 2020-04-23 2022-09-20 The Boeing Company Methods of manufacture for aircraft substructure
CN112548569B (zh) * 2020-12-02 2023-07-07 南京航空航天大学 一种飞行器蒙皮-桁条结构复合增材减材制造系统与方法
CN112765695B (zh) * 2021-01-21 2023-12-05 深圳市创想三维科技股份有限公司 支撑体生成方法、3d打印机、计算机装置及存储介质
US11981460B2 (en) * 2022-05-13 2024-05-14 Firestorm Labs, Inc. Mission-adaptable aerial vehicle and methods for in-field assembly and use
CA3160533A1 (en) * 2022-05-26 2023-11-26 Airbus Canada Limited Partnership Stiffener integration in an isogrid structure
US12479644B1 (en) * 2023-01-26 2025-11-25 United States Of America, Department Of The Navy Sealed ortho-grid laser and imaging director with an ortho/iso-grid pressure vessel
US12486017B2 (en) 2024-03-13 2025-12-02 Firestorm Labs, Inc. Additive manufactured integral fastening system for mission adaptable unmanned aerial vehicles
EP4656512A1 (en) * 2024-05-29 2025-12-03 AIRBUS Operations GmbH Aircraft fuselage and aircraft or spacecraft

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US20080067289A1 (en) 2006-09-15 2008-03-20 Airbus France Splice plate for stringers and orbital joining device
DE102008057247B3 (de) 2008-11-13 2010-01-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Paneel in einer Semimonocoque-Bauweise und Herstellungsverfahren dafür
JP2014534924A (ja) 2011-10-10 2014-12-25 ザ・ボーイング・カンパニーＴｈｅＢｏｅｉｎｇ Ｃｏｍｐａｎｙ 高さが先細になる湾曲複合ストリンガーおよび対応するパネル
JP2016537249A (ja) 2013-11-15 2016-12-01 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ ＰＩ（π）結合された構造体内の低応力の補強材のランアウト

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US2617179A (en) * 1950-05-10 1952-11-11 Mcdonnell Aircraft Corp Method of manufacturing tapered beams
US6648273B2 (en) * 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
US7818945B2 (en) * 2005-03-31 2010-10-26 The Boeing Company Composite structural member having an undulating web and method for forming same
GB0712552D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Elongate composite structural members and improvements therein
GB0712549D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Improvements in elongate composite structural members
DE102007044389A1 (de) * 2007-09-18 2009-04-02 Airbus Deutschland Gmbh Strukturbauteil und Rumpf eines Luft- oder Raumfahrzeugs
DE102007054053A1 (de) * 2007-11-13 2009-05-20 Airbus Deutschland Gmbh Kupplungselement zur Verbindung von zwei Längsversteifungselementen
US8776375B2 (en) * 2011-05-19 2014-07-15 The Boeing Company Aircraft structure for high capacity pull off
FR2984844B1 (fr) * 2011-12-21 2014-02-28 Airbus Operations Sas Element de structure de fuselage d'aeronef anti deversement
US8703269B2 (en) * 2012-02-14 2014-04-22 Gulfstream Aerospace Corporation Reinforced composite structures for aircrafts and methods for making the same
US9096324B2 (en) * 2013-03-19 2015-08-04 The Boeing Company Joint assembly to form a sealed flow conduit
EP2781450B1 (en) * 2013-03-19 2018-05-02 Airbus Operations GmbH System and method for interconnecting composite structures
ES2819076T3 (es) * 2013-04-30 2021-04-14 Airbus Operations Sl Estructura compuesta para una aeronave y procedimiento de fabricación de la misma
GB2517954B (en) * 2013-09-05 2018-07-04 Airbus Operations Ltd Repair of a damaged composite aircraft wing
WO2015094059A1 (en) * 2013-12-20 2015-06-25 Saab Ab Stiffening element and reinforced structure
CL2014000880A1 (es) 2014-04-08 2014-10-03 Guillermo Moyano Fondo de contenedor para productos hortofruticolas que optimiza el uso del material para distribuir los esfuerzos a los cuales es sometido, dicho fondo conformado por un marco de fondo unido a una base de fondo porque dicha base de fondo comprende nervios de altura variable; contenedor para productos hortofruticolas y procedimiento de fabricacion.
US9527572B2 (en) * 2014-06-26 2016-12-27 The Boeing Company Elongated structures and related assemblies

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080067289A1 (en) 2006-09-15 2008-03-20 Airbus France Splice plate for stringers and orbital joining device
DE102008057247B3 (de) 2008-11-13 2010-01-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Paneel in einer Semimonocoque-Bauweise und Herstellungsverfahren dafür
JP2014534924A (ja) 2011-10-10 2014-12-25 ザ・ボーイング・カンパニーＴｈｅＢｏｅｉｎｇ Ｃｏｍｐａｎｙ 高さが先細になる湾曲複合ストリンガーおよび対応するパネル
JP2016537249A (ja) 2013-11-15 2016-12-01 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ ＰＩ（π）結合された構造体内の低応力の補強材のランアウト

Also Published As

Publication number Publication date
US11312468B2 (en) 2022-04-26
CN110816807A (zh) 2020-02-21
CN110816807B (zh) 2024-03-29
EP3608218A1 (en) 2020-02-12
EP3608218B1 (en) 2022-08-17
CA3042655A1 (en) 2020-02-08
CA3042655C (en) 2023-08-15
JP2020050332A (ja) 2020-04-02
US20200047867A1 (en) 2020-02-13

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