BRPI1006796A2 - estrutura de aerofólio com membro de reforço corrugado - Google Patents

estrutura de aerofólio com membro de reforço corrugado

Info

Publication number
BRPI1006796A2
BRPI1006796A2 BRPI1006796A BRPI1006796A BRPI1006796A2 BR PI1006796 A2 BRPI1006796 A2 BR PI1006796A2 BR PI1006796 A BRPI1006796 A BR PI1006796A BR PI1006796 A BRPI1006796 A BR PI1006796A BR PI1006796 A2 BRPI1006796 A2 BR PI1006796A2
Authority
BR
Brazil
Prior art keywords
reinforcement member
airfoil structure
corrugated reinforcement
corrugated
airfoil
Prior art date
Application number
BRPI1006796A
Other languages
English (en)
Inventor
Christopher Payne
David Groves
Original Assignee
Airbus Operations Ltd
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 Airbus Operations Ltd filed Critical Airbus Operations Ltd
Publication of BRPI1006796A2 publication Critical patent/BRPI1006796A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/22—Geodetic or other open-frame structures
    • 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
    • Y10T29/49616—Structural member making
    • Y10T29/49622—Vehicular structural member making
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Wind Motors (AREA)
  • Body Structure For Vehicles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BRPI1006796A 2009-01-14 2010-01-14 estrutura de aerofólio com membro de reforço corrugado BRPI1006796A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0900494.6A GB0900494D0 (en) 2009-01-14 2009-01-14 Aerofoil Structure
PCT/GB2010/050040 WO2010082047A1 (en) 2009-01-14 2010-01-14 Aerofoil structure with corrugated reinforcing member

Publications (1)

Publication Number Publication Date
BRPI1006796A2 true BRPI1006796A2 (pt) 2016-03-15

Family

ID=40379496

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1006796A BRPI1006796A2 (pt) 2009-01-14 2010-01-14 estrutura de aerofólio com membro de reforço corrugado

Country Status (9)

Country Link
US (1) US8800924B2 (pt)
EP (1) EP2376328B1 (pt)
JP (1) JP5600120B2 (pt)
CN (1) CN102282069B (pt)
BR (1) BRPI1006796A2 (pt)
CA (1) CA2744799C (pt)
GB (1) GB0900494D0 (pt)
RU (1) RU2523726C2 (pt)
WO (1) WO2010082047A1 (pt)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL2007438C2 (en) * 2011-09-16 2013-03-19 Suzlon Blade Technology B V Blade for a wind turbine and wind turbine including such blades.
FR2981880B1 (fr) * 2011-10-28 2014-09-19 Daher Aerospace Procede pour etancher un reservoir de carburant
WO2013078646A1 (en) * 2011-11-30 2013-06-06 Airbus S.A.S. Airplane component having a box structure
RU2521882C1 (ru) * 2013-01-31 2014-07-10 Общество с ограниченной ответственностью "Научно-технологический испытательный центр АпАТэК-Дубна" Стрингерная панель из композиционного слоистого материала
US9187168B2 (en) * 2013-07-30 2015-11-17 The Boeing Company Natural-path tearstraps and stiffeners for spherical composite pressure bulkheads
DK2875937T3 (da) * 2013-11-22 2021-05-03 Vitrulan Composites Oy Ensrettet forstærkning, en fremgangsmåde til fremstilling af en ensrettet forstærkning og anvendelsen deraf
ES2902069T3 (es) 2014-10-16 2022-03-24 Airbus Operations Gmbh Deflector para aeronave y método asociado
US10358821B2 (en) * 2015-03-02 2019-07-23 The Boeing Company Thermoplastic truss structure for use in wing and rotor blade structures and methods for manufacture
US10295438B2 (en) * 2016-06-24 2019-05-21 The Boeing Company Modeling and analysis of leading edge ribs of an aircraft wing
FR3069481B1 (fr) * 2017-07-28 2021-05-28 Airbus Helicopters Procede de fabrication d'un corps de remplissage d'une pale d'un rotor et corps de remplissage d'une pale de rotor comportant au moins un ensemble alveolaire a cellules fermees
US10167076B1 (en) * 2017-12-12 2019-01-01 Kitty Hawk Corporation Corrugated lift fan rotor
US11273899B2 (en) * 2018-01-25 2022-03-15 The Boeing Company Wing rib, wing having wing rib, and method for manufacturing the same
FR3091263A1 (fr) * 2018-12-28 2020-07-03 Daher Aerospace Bec de bord d’attaque à structure optimisée
CN112012877A (zh) * 2019-05-31 2020-12-01 江苏金风科技有限公司 加强部件、腹板、叶片、成型方法及风力发电机组
CN111486049A (zh) * 2020-04-29 2020-08-04 中材科技风电叶片股份有限公司 复合结构体、叶片
GB2606009A (en) * 2021-04-22 2022-10-26 Airbus Operations Ltd Aerofoil structures
CN114132483B (zh) * 2021-11-10 2024-06-07 大连海事大学 基于指数衰减曲线前缘变形的仿生机翼参数化变形方法

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU15693A1 (ru) * 1927-05-02 1930-06-30 Рорбах А. Балка дл крыльев металлических аэропланов
GB447459A (en) 1934-08-30 1936-05-19 Dornier Metallbauten Gmbh Improvements in or relating to aircraft wings
US2157042A (en) * 1937-04-21 1939-05-02 Vickers Armstrongs Ltd Wing, fuselage, or other aircraft body
US2311683A (en) 1939-12-23 1943-02-23 Richard G Naugle Airplane wing construction
GB609313A (en) 1945-09-24 1948-09-29 Nigel Edward Broadsmith Improvements in or relating to aerofoil structures
SE305596B (pt) 1963-06-21 1968-10-28 Boelkow Gmbh
GB1082352A (en) 1964-10-02 1967-09-06 Parsons Corp Improved airfoil construction
US4083656A (en) 1975-03-21 1978-04-11 Textron, Inc. Composite rotor blade
GB2041861B (en) 1979-02-09 1983-04-13 Boeing Co Composite honeycomb core structures and single stage hot bonding method of producing such structures
US4657615A (en) 1984-08-20 1987-04-14 The Boeing Company Composite leading edge/spar member for an aircraft control surface
US5457884A (en) 1992-08-14 1995-10-17 Rolls-Royce Plc Method of manufacturing an article by superplastic forming and diffusion bonding
GB9603476D0 (en) 1996-02-19 1996-04-17 Holden Laurence Honeycomb frame construction
US6889937B2 (en) 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
JP4545339B2 (ja) * 2001-04-05 2010-09-15 富士重工業株式会社 複合材翼およびその製造方法
DE102004018579A1 (de) * 2004-04-16 2005-11-03 Airbus Deutschland Gmbh Verkleidung für eine Struktur eines Flugzeugs
FI119726B (fi) * 2006-09-26 2009-02-27 Patria Aerostructures Oy Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja
FR2977304B1 (fr) 2011-06-28 2013-07-19 Valeo Systemes Thermiques Echangeur de chaleur, boitier et circuit de climatisation comprenant un tel echangeur

Also Published As

Publication number Publication date
EP2376328B1 (en) 2013-03-20
WO2010082047A1 (en) 2010-07-22
JP2012515103A (ja) 2012-07-05
CA2744799C (en) 2015-09-08
US20120132751A1 (en) 2012-05-31
JP5600120B2 (ja) 2014-10-01
CA2744799A1 (en) 2010-07-22
US8800924B2 (en) 2014-08-12
CN102282069B (zh) 2013-12-18
GB0900494D0 (en) 2009-02-11
EP2376328A1 (en) 2011-10-19
RU2523726C2 (ru) 2014-07-20
RU2011130705A (ru) 2013-02-20
CN102282069A (zh) 2011-12-14

Similar Documents

Publication Publication Date Title
BRPI1006796A2 (pt) estrutura de aerofólio com membro de reforço corrugado
NO2020008I1 (no) nusinersen eller salter derav
BR112012003612A2 (pt) conversão de força com pseudofase acrescentada
FR2948598B1 (fr) Renfort composite
BRPI0921447A2 (pt) estrutrura de reforço híbrido
BRPI0921153A2 (pt) reforço de armadura
DK2406492T3 (da) Vingemontering
FR2943269B1 (fr) Renfort composite auto-adherent
FR2945826B1 (fr) Renfort composite auto-adherent
BRPI1006760A2 (pt) montagem
BRPI0915524A2 (pt) conjunto de aerofólio
BRPI1011310A2 (pt) aeronave
BRPI0906171A2 (pt) Nacela de aeronave
BR112012002585A2 (pt) reforço revestido
FR2942453B1 (fr) Aeronef a structure de plancher renforcee.
DE112010001215A5 (de) Gurtaufrollersystem mit einsteuerglied
BRPI1007026A2 (pt) estrutura de sustentação de carga reforçada
DOP2011000348A (es) Construcciones casb7439
BRPI0908341A2 (pt) Estrutura aerodinâmica com ondulações de choque assimétricas
BRPI1011196A2 (pt) aperfeiçoamentos em flutuadores de aeronave
FR2953810B1 (fr) Nacelle de turboreacteur
BRPI0907670A2 (pt) conjunto de estrutura de aeronave
DK3495068T3 (da) Armeringsforbindelsesanordning
FI20095607A0 (fi) Työkoneohjaamo
FI8515U1 (fi) Rakennelma

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 7A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]