JP2013527075A5 - - Google Patents

Download PDF

Info

Publication number
JP2013527075A5
JP2013527075A5 JP2013511168A JP2013511168A JP2013527075A5 JP 2013527075 A5 JP2013527075 A5 JP 2013527075A5 JP 2013511168 A JP2013511168 A JP 2013511168A JP 2013511168 A JP2013511168 A JP 2013511168A JP 2013527075 A5 JP2013527075 A5 JP 2013527075A5
Authority
JP
Japan
Prior art keywords
stringer
radius
edge
free end
providing
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.)
Granted
Application number
JP2013511168A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013527075A (ja
JP5809249B2 (ja
Filing date
Publication date
Priority claimed from US12/783,057 external-priority patent/US8408493B2/en
Application filed filed Critical
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

Links

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 2010-05-19
US12/783,057 US8408493B2 (en) 2010-05-19 2010-05-19 Composite stringer end trim
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 true JP2013527075A5 (cg-RX-API-DMAC7.html) 2014-03-27
JP5809249B2 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
ES2606245T3 (es) * 2012-07-17 2017-03-23 Airbus Operations, S.L. Borde de ataque altamente integrado de una superficie sustentadora de una aeronave
US9272769B2 (en) 2012-11-13 2016-03-01 The Boeing Company Joint for composite wings
JP6220044B2 (ja) * 2013-03-15 2017-10-25 ボストン サイエンティフィック サイムド，インコーポレイテッドＢｏｓｔｏｎ Ｓｃｉｅｎｔｉｆｉｃ Ｓｃｉｍｅｄ，Ｉｎｃ． 腎神経アブレーションのための医療用デバイス
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
CA2911447C (en) 2013-08-09 2020-03-10 The Boeing Company Stiffened composite panels and method of their manufacture
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

Similar Documents

Publication Publication Date Title
JP2013527075A5 (cg-RX-API-DMAC7.html)
JP5809249B2 (ja) 複合材ストリンガ端部トリム
EP2032432B1 (en) Composite wing-body joint
JP2010523397A5 (cg-RX-API-DMAC7.html)
RU2424155C2 (ru) Стрингер для крыла летательного аппарата и способ изготовления стрингера для крыла летательного аппарата
EP2835310B1 (en) Aircraft side of body joint
US8684311B2 (en) Bonded splice joint
CN103874629B (zh) 高度渐缩的弯曲复合纵梁及相应面板
CA2768957C (en) Composite-material structure and aircraft main wing and aircraft fuselage provided with the same
WO2010070181A3 (es) Costilla-herraje
JP5600120B2 (ja) 波状補強部材を備えたエアロフォイル構造体
US9470205B2 (en) Wind turbine blades with layered, multi-component spars, and associated systems and methods
EP3276162A3 (en) Efficient wind turbine blades, wind turbine blade structures, and associated systems and methods of manufacture, assembly and use
JP2015147412A (ja) 積層ｉ字ブレードストリンガー
US20120234978A1 (en) Load transfer devices at a stringer run-out
WO2011157849A3 (en) Rotor blade for a wind turbine
WO2012028467A8 (en) Air sucking vehicle fuselage component, method for producing an air sucking vehicle fuselage component and a vehicle, especially an aircraft, with an air sucking vehicle fuselage component
WO2012001207A3 (es) Fuselaje de aeronave en material compuesto y procedimientos para su fabricacion
WO2011071939A3 (en) Wing spar splice joint
US9533481B2 (en) Method for manufacturing a composite material part comprising a web and at least one flange
US20170240299A1 (en) Process for assembling aircraft control surfaces
CN203889055U (zh) 一种直升机平尾结构
WO2011106733A3 (en) Advanced aerodynamic and structural blade and wing design
JP2019151321A (ja) 共通の基礎支持部を通るストリンガ移行部
EP3126125A2 (en) Structural arrangement and method of fabricating a composite trailing edge control surface