JP5809249B2 - 複合材ストリンガ端部トリム - Google Patents

複合材ストリンガ端部トリム Download PDF

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Publication number
JP5809249B2
JP5809249B2 JP2013511168A JP2013511168A JP5809249B2 JP 5809249 B2 JP5809249 B2 JP 5809249B2 JP 2013511168 A JP2013511168 A JP 2013511168A JP 2013511168 A JP2013511168 A JP 2013511168A JP 5809249 B2 JP5809249 B2 JP 5809249B2
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JP
Japan
Prior art keywords
stringer
edge
radius
radial
wing
Prior art date
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Active
Application number
JP2013511168A
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English (en)
Japanese (ja)
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JP2013527075A5 (cg-RX-API-DMAC7.html
JP2013527075A (ja
Inventor
ジョシュア ディー． バーナード，
ジョシュア ディー． バーナード，
ブライアン ダブリュ． アレント，
ブライアン ダブリュ． アレント，
チュン−リャン リン，
チュン−リャン リン，
ハンギ リ，
ハンギ リ，
カルロス アルベルト パエツ，
カルロス アルベルト パエツ，
バーンハード ドプカー，
バーンハード ドプカー，
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 JP2013527075A publication Critical patent/JP2013527075A/ja
Publication of JP2013527075A5 publication Critical patent/JP2013527075A5/ja
Application granted granted Critical
Publication of JP5809249B2 publication Critical patent/JP5809249B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/182—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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24777—Edge feature

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Body Structure For Vehicles (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Connection Of Plates (AREA)
  • Casings For Electric Apparatus (AREA)
JP2013511168A 2010-05-19 2011-04-19 複合材ストリンガ端部トリム Active JP5809249B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/783,057 US8408493B2 (en) 2010-05-19 2010-05-19 Composite stringer end trim
US12/783,057 2010-05-19
PCT/US2011/033083 WO2011146194A1 (en) 2010-05-19 2011-04-19 Composite stringer end trim

Publications (3)

Publication Number Publication Date
JP2013527075A JP2013527075A (ja) 2013-06-27
JP2013527075A5 JP2013527075A5 (cg-RX-API-DMAC7.html) 2014-03-27
JP5809249B2 true JP5809249B2 (ja) 2015-11-10

Family

ID=44626060

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013511168A Active JP5809249B2 (ja) 2010-05-19 2011-04-19 複合材ストリンガ端部トリム

Country Status (6)

Country Link
US (1) US8408493B2 (cg-RX-API-DMAC7.html)
EP (1) EP2571757B1 (cg-RX-API-DMAC7.html)
JP (1) JP5809249B2 (cg-RX-API-DMAC7.html)
CN (1) CN102892670B (cg-RX-API-DMAC7.html)
ES (1) ES2614708T3 (cg-RX-API-DMAC7.html)
WO (1) WO2011146194A1 (cg-RX-API-DMAC7.html)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5455541B2 (ja) * 2009-10-14 2014-03-26 三菱重工業株式会社 ストリンガーの製造方法
US8408493B2 (en) 2010-05-19 2013-04-02 The Boeing Company Composite stringer end trim
FR2970463B1 (fr) * 2011-01-17 2013-02-15 Airbus Operations Sas Dispositif d'eclissage a tenue mecanique amelioree.
US8703269B2 (en) 2012-02-14 2014-04-22 Gulfstream Aerospace Corporation Reinforced composite structures for aircrafts and methods for making the same
US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
US8974886B2 (en) * 2012-04-25 2015-03-10 The Boeing Company Disbond resistant composite stiffener runout
EP2687436B1 (en) * 2012-07-17 2016-08-31 Airbus Operations, S.L. Highly integrated leading edge of an aircraft lifting surface
US9272769B2 (en) 2012-11-13 2016-03-01 The Boeing Company Joint for composite wings
WO2014150553A1 (en) * 2013-03-15 2014-09-25 Boston Scientific Scimed, Inc. Methods and apparatuses for remodeling tissue of or adjacent to a body passage
US9096324B2 (en) * 2013-03-19 2015-08-04 The Boeing Company Joint assembly to form a sealed flow conduit
US9926067B1 (en) * 2013-06-10 2018-03-27 The Boeing Company Stringer flange extending to composite skin edge
US10029780B2 (en) 2013-08-09 2018-07-24 The Boeing Company Stiffened composite panels
US10479475B2 (en) 2013-08-09 2019-11-19 The Boeing Company Composite stringer beam joint structure of an aircraft
US9475569B2 (en) 2013-10-29 2016-10-25 Gulfstream Aerospace Corporation Methods for manufacturing an i-stringer of an aircraft and devices for use in such methods
FR3015433B1 (fr) 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
US9527572B2 (en) 2014-06-26 2016-12-27 The Boeing Company Elongated structures and related assemblies
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
US9399510B2 (en) * 2014-08-20 2016-07-26 The Boeing Company Hat stringer closeout fitting and method of making same
US9586667B2 (en) * 2014-12-02 2017-03-07 The Boeing Company Splice assembly for joining structural components
US10745104B2 (en) * 2018-03-02 2020-08-18 The Boeing Company Stringer transition through a common base charge
GB2575280A (en) * 2018-07-04 2020-01-08 Airbus Operations Ltd A Connector
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
US11724791B2 (en) * 2019-10-08 2023-08-15 The Boeing Company Enhanced design for stringer runout terminations on composite panels
CN112591073B (zh) * 2020-12-23 2021-09-24 北京北航天宇长鹰无人机科技有限公司 一种翼身结合接头及无人机
KR20240148479A (ko) * 2023-04-04 2024-10-11 현대자동차주식회사 동체의 날개 하중 지지구조

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2383634A (en) 1943-02-20 1945-08-28 Budd Edward G Mfg Co Main frame structure for airfoils or the like
GB0122050D0 (en) * 2001-09-13 2001-10-31 Bae Systems Plc Composite material structure
US7159822B2 (en) 2004-04-06 2007-01-09 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7546979B1 (en) * 2006-09-15 2009-06-16 The Boeing Company Trapezoidal panel pin joint allowing free deflection between fuselage and wing
US7635106B2 (en) * 2006-11-30 2009-12-22 The Boeing Company Composite shear tie
US7721995B2 (en) * 2006-12-13 2010-05-25 The Boeing Company Rib support for wing panels
US7861969B2 (en) * 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
DE102007029500B4 (de) 2007-06-25 2013-02-14 Airbus Operations Gmbh Verfahren zum Koppeln von Versteifungsprofilelementen sowie Strukturbauteil
DE202009012605U1 (de) 2009-09-18 2011-02-03 Evac Gmbh Mobile Wasserverbrauchseinrichtung mit Kondenswassernutzung
US8408493B2 (en) 2010-05-19 2013-04-02 The Boeing Company Composite stringer end trim

Also Published As

Publication number Publication date
CN102892670B (zh) 2015-10-21
US8408493B2 (en) 2013-04-02
ES2614708T3 (es) 2017-06-01
EP2571757B1 (en) 2016-11-09
US20110284693A1 (en) 2011-11-24
CN102892670A (zh) 2013-01-23
EP2571757A1 (en) 2013-03-27
JP2013527075A (ja) 2013-06-27
WO2011146194A1 (en) 2011-11-24

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