RU2661411C2 - Симметричная крыльевая нервюра со срезными поперечинами, прикрепленными по центральной плоскости - Google Patents

Симметричная крыльевая нервюра со срезными поперечинами, прикрепленными по центральной плоскости Download PDF

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Publication number
RU2661411C2
RU2661411C2 RU2014124529A RU2014124529A RU2661411C2 RU 2661411 C2 RU2661411 C2 RU 2661411C2 RU 2014124529 A RU2014124529 A RU 2014124529A RU 2014124529 A RU2014124529 A RU 2014124529A RU 2661411 C2 RU2661411 C2 RU 2661411C2
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RU
Russia
Prior art keywords
symmetrical
rib
design
specified
central plane
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RU2014124529A
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English (en)
Russian (ru)
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RU2014124529A (ru
Inventor
Джон Дэвид ВАНДЕРХОУК
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Зе Боинг Компани
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Application filed by Зе Боинг Компани filed Critical Зе Боинг Компани
Publication of RU2014124529A publication Critical patent/RU2014124529A/ru
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs
    • 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

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Connection Of Plates (AREA)
RU2014124529A 2013-06-21 2014-06-17 Симметричная крыльевая нервюра со срезными поперечинами, прикрепленными по центральной плоскости RU2661411C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/923,841 US9296466B2 (en) 2013-06-21 2013-06-21 Symmetric wing rib with center plane fastened shear ties
US13/923,841 2013-06-21

Publications (2)

Publication Number Publication Date
RU2014124529A RU2014124529A (ru) 2015-12-27
RU2661411C2 true RU2661411C2 (ru) 2018-07-16

Family

ID=50980176

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014124529A RU2661411C2 (ru) 2013-06-21 2014-06-17 Симметричная крыльевая нервюра со срезными поперечинами, прикрепленными по центральной плоскости

Country Status (9)

Country Link
US (1) US9296466B2 (enExample)
EP (1) EP2815961B1 (enExample)
JP (1) JP6494186B2 (enExample)
KR (1) KR102153756B1 (enExample)
CN (1) CN104229121B (enExample)
AU (1) AU2014201864B2 (enExample)
CA (1) CA2847635C (enExample)
ES (1) ES2616729T3 (enExample)
RU (1) RU2661411C2 (enExample)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2910365B1 (en) * 2014-02-21 2017-04-26 Airbus Operations GmbH Composite structural element and torsion box
US10479474B2 (en) 2016-07-14 2019-11-19 The Boeing Company Friction stir welded wingtip torque box
US10745103B2 (en) * 2017-05-31 2020-08-18 The Boeing Company Aircraft, aircraft wings and associated shear ties
CN108082474B (zh) * 2017-10-31 2022-11-18 中航通飞华南飞机工业有限公司 一种水上飞机断阶框结构
US11319051B2 (en) * 2020-01-03 2022-05-03 The Boeing Company Stiffened composite ribs

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2336021A2 (en) * 2009-12-15 2011-06-22 The Boeing Company High pull-off capability hat stringer
US8001690B2 (en) * 2003-12-23 2011-08-23 Airbus Uk Limited Rib for aircraft wing and methods for the manufacture thereof
RU2428353C2 (ru) * 2006-03-27 2011-09-10 ЭЙРБАС ЮКей ЛИМИТЕД Конструктивный элемент воздушного судна

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB157310A (en) 1919-02-27 1922-06-08 John William Rapp Improvements in airplane ribs
FR1396979A (fr) 1964-06-01 1965-04-23 Kirk Wing Company Structure de profil d'aile et son procédé de fabrication
US4557440A (en) 1983-08-18 1985-12-10 The Boeing Company Movable panel with compound curvature and method of making same
FR2901243B1 (fr) * 2006-05-16 2008-06-27 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef
GB0619512D0 (en) * 2006-10-03 2006-11-15 Airbus Uk Ltd Fitting
US7721995B2 (en) * 2006-12-13 2010-05-25 The Boeing Company Rib support for wing panels
US7686251B2 (en) * 2006-12-13 2010-03-30 The Boeing Company Rib support for wing panels
FR2948099B1 (fr) * 2009-07-16 2012-05-11 Airbus Operations Sas Procede de fabrication d'un aeronef a voilure fixe
EP2463291B1 (en) * 2010-12-09 2016-05-04 Shin-Etsu Chemical Co., Ltd. Hydrosilylation method, method for producing organosilicon compound, and organosilicon compound.
US8679616B2 (en) 2010-12-14 2014-03-25 The Boeing Company Skew-angle radius filler
JP6093192B2 (ja) * 2013-01-25 2017-03-08 三菱航空機株式会社 航空機の機体用パネル、航空機の翼

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8001690B2 (en) * 2003-12-23 2011-08-23 Airbus Uk Limited Rib for aircraft wing and methods for the manufacture thereof
RU2428353C2 (ru) * 2006-03-27 2011-09-10 ЭЙРБАС ЮКей ЛИМИТЕД Конструктивный элемент воздушного судна
EP2336021A2 (en) * 2009-12-15 2011-06-22 The Boeing Company High pull-off capability hat stringer

Also Published As

Publication number Publication date
KR102153756B1 (ko) 2020-09-09
JP6494186B2 (ja) 2019-04-03
AU2014201864A1 (en) 2015-01-22
JP2015227151A (ja) 2015-12-17
RU2014124529A (ru) 2015-12-27
US9296466B2 (en) 2016-03-29
KR20150035362A (ko) 2015-04-06
CA2847635A1 (en) 2014-12-21
EP2815961B1 (en) 2016-11-30
AU2014201864B2 (en) 2016-05-19
CN104229121B (zh) 2018-05-22
CA2847635C (en) 2018-06-19
CN104229121A (zh) 2014-12-24
ES2616729T3 (es) 2017-06-14
US20150298790A1 (en) 2015-10-22
EP2815961A1 (en) 2014-12-24

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