JP7783717B2 - 一体化された犠牲表面を備えた複合スパー - Google Patents

一体化された犠牲表面を備えた複合スパー

Info

Publication number
JP7783717B2
JP7783717B2 JP2021174539A JP2021174539A JP7783717B2 JP 7783717 B2 JP7783717 B2 JP 7783717B2 JP 2021174539 A JP2021174539 A JP 2021174539A JP 2021174539 A JP2021174539 A JP 2021174539A JP 7783717 B2 JP7783717 B2 JP 7783717B2
Authority
JP
Japan
Prior art keywords
composite
sacrificial member
spar
layup
machining
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
JP2021174539A
Other languages
English (en)
Japanese (ja)
Other versions
JP2022105979A (ja
JP2022105979A5 (enExample
Inventor
エリック・ショーン・カミラ
ジョセフ・リー・スウィーティン・ザ・サード
ジョセフィン・ラコエ
チリプ・チャン
クリフォード・ディー・ボロヴィチ
ルーズベ・チャヴォシャン
イアン・エドワード・シュレーダー
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of JP2022105979A publication Critical patent/JP2022105979A/ja
Publication of JP2022105979A5 publication Critical patent/JP2022105979A5/ja
Application granted granted Critical
Publication of JP7783717B2 publication Critical patent/JP7783717B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/185—Spars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/20—Integral or sandwich constructions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Moulding By Coating Moulds (AREA)
JP2021174539A 2021-01-05 2021-10-26 一体化された犠牲表面を備えた複合スパー Active JP7783717B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US202163134071P 2021-01-05 2021-01-05
US63/134,071 2021-01-05

Publications (3)

Publication Number Publication Date
JP2022105979A JP2022105979A (ja) 2022-07-15
JP2022105979A5 JP2022105979A5 (enExample) 2025-10-20
JP7783717B2 true JP7783717B2 (ja) 2025-12-10

Family

ID=82219926

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2021174539A Active JP7783717B2 (ja) 2021-01-05 2021-10-26 一体化された犠牲表面を備えた複合スパー

Country Status (2)

Country Link
US (1) US11981426B2 (enExample)
JP (1) JP7783717B2 (enExample)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2617556A (en) * 2022-04-08 2023-10-18 Airbus Operations Ltd Wing-box structure

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000043796A (ja) 1998-07-30 2000-02-15 Japan Aircraft Development Corp 複合材の翼形構造およびその成形方法
JP2016172437A (ja) 2015-03-04 2016-09-29 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 複合材料構造体を接合するための共硬化プロセス
JP2017226206A (ja) 2016-03-24 2017-12-28 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 補強材を有する複合構造体及びその製造方法
CN107813920A (zh) 2016-09-13 2018-03-20 波音公司 开放通道加强筋
JP2019038517A (ja) 2017-08-23 2019-03-14 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 共硬化した桁および縦通材の中央ウイングボックス
US20190184648A1 (en) 2017-12-15 2019-06-20 MTU Aero Engines AG Faserverbund-Bauteilanordnung, Faserverbund-Bauteilsystem und Verfahren zum Herstellen eines Faserverbund-Bauteilsystems
JP2020511334A (ja) 2017-03-16 2020-04-16 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 第１の熱硬化性複合材と第２の熱硬化性複合材を共接合して硬化複合材部品を構成する方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9024387D0 (en) 1990-11-09 1991-01-02 British Aerospace Carbon fibre composite wing manufacture
JP5476916B2 (ja) 2009-10-16 2014-04-23 東レ株式会社 繊維強化プラスチックの製造方法
US10974465B2 (en) 2018-06-20 2021-04-13 The Boeing Company Method and system for generating a layup plan for forming a composite laminate
GB2575280A (en) 2018-07-04 2020-01-08 Airbus Operations Ltd A Connector
RU2749432C1 (ru) 2020-01-10 2021-06-10 Акционерное общество "АэроКомпозит" Способ модульной сборки стыковой нервюры самолета для соединения консолей крыла с центропланом и устройство для осуществления способа
US11673644B2 (en) * 2021-01-05 2023-06-13 The Boeing Company Composite spars with integrated sacrificial surfaces

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000043796A (ja) 1998-07-30 2000-02-15 Japan Aircraft Development Corp 複合材の翼形構造およびその成形方法
JP2016172437A (ja) 2015-03-04 2016-09-29 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 複合材料構造体を接合するための共硬化プロセス
JP2017226206A (ja) 2016-03-24 2017-12-28 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 補強材を有する複合構造体及びその製造方法
CN107813920A (zh) 2016-09-13 2018-03-20 波音公司 开放通道加强筋
JP2020511334A (ja) 2017-03-16 2020-04-16 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 第１の熱硬化性複合材と第２の熱硬化性複合材を共接合して硬化複合材部品を構成する方法
JP2019038517A (ja) 2017-08-23 2019-03-14 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 共硬化した桁および縦通材の中央ウイングボックス
US20190184648A1 (en) 2017-12-15 2019-06-20 MTU Aero Engines AG Faserverbund-Bauteilanordnung, Faserverbund-Bauteilsystem und Verfahren zum Herstellen eines Faserverbund-Bauteilsystems

Also Published As

Publication number Publication date
JP2022105979A (ja) 2022-07-15
US11981426B2 (en) 2024-05-14
US20220212777A1 (en) 2022-07-07

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