SE517133C2 - Anordning för att stödja en skalyta i ett flygplansskrov - Google Patents

Anordning för att stödja en skalyta i ett flygplansskrov

Info

Publication number
SE517133C2
SE517133C2 SE0102009A SE0102009A SE517133C2 SE 517133 C2 SE517133 C2 SE 517133C2 SE 0102009 A SE0102009 A SE 0102009A SE 0102009 A SE0102009 A SE 0102009A SE 517133 C2 SE517133 C2 SE 517133C2
Authority
SE
Sweden
Prior art keywords
profile
shell surface
stringer
base surface
shell
Prior art date
Application number
SE0102009A
Other languages
English (en)
Swedish (sv)
Other versions
SE0102009L (sv
SE0102009D0 (sv
Inventor
Paer Brofeldt
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Priority to SE0102009A priority Critical patent/SE517133C2/sv
Publication of SE0102009D0 publication Critical patent/SE0102009D0/xx
Publication of SE0102009L publication Critical patent/SE0102009L/
Publication of SE517133C2 publication Critical patent/SE517133C2/sv
Priority to ES02776541T priority patent/ES2281546T3/es
Priority to US10/479,663 priority patent/US7124982B2/en
Priority to AT02776541T priority patent/ATE356020T1/de
Priority to EP02776541A priority patent/EP1397289B1/fr
Priority to DE60218664T priority patent/DE60218664T2/de
Priority to PCT/SE2002/000787 priority patent/WO2002098733A1/fr

Links

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
    • B64C1/12—Construction or attachment of skin panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Tires In General (AREA)
  • Connection Of Plates (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Reciprocating Pumps (AREA)
  • Catching Or Destruction (AREA)
  • Laminated Bodies (AREA)
  • Fuses (AREA)
  • Body Structure For Vehicles (AREA)
SE0102009A 2001-06-05 2001-06-05 Anordning för att stödja en skalyta i ett flygplansskrov SE517133C2 (sv)

Priority Applications (7)

Application Number Priority Date Filing Date Title
SE0102009A SE517133C2 (sv) 2001-06-05 2001-06-05 Anordning för att stödja en skalyta i ett flygplansskrov
ES02776541T ES2281546T3 (es) 2001-06-05 2002-04-23 Dispositivo de arriostramiento de un revestimiento en un fuselaje de avion.
US10/479,663 US7124982B2 (en) 2001-06-05 2002-04-23 Device for bracing a shell in an aircraft fuselage
AT02776541T ATE356020T1 (de) 2001-06-05 2002-04-23 Vorrichtung zur verstrebung einer schale in einem flugzeugrumpf
EP02776541A EP1397289B1 (fr) 2001-06-05 2002-04-23 Dispositif d'entretoisement d'une coque dans un fuselage d'avion
DE60218664T DE60218664T2 (de) 2001-06-05 2002-04-23 Vorrichtung zur verstrebung einer schale in einem flugzeugrumpf
PCT/SE2002/000787 WO2002098733A1 (fr) 2001-06-05 2002-04-23 Dispositif d'entretoisement d'une coque dans un fuselage d'avion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0102009A SE517133C2 (sv) 2001-06-05 2001-06-05 Anordning för att stödja en skalyta i ett flygplansskrov

Publications (3)

Publication Number Publication Date
SE0102009D0 SE0102009D0 (sv) 2001-06-05
SE0102009L SE0102009L (sv) 2002-04-16
SE517133C2 true SE517133C2 (sv) 2002-04-16

Family

ID=20284386

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0102009A SE517133C2 (sv) 2001-06-05 2001-06-05 Anordning för att stödja en skalyta i ett flygplansskrov

Country Status (7)

Country Link
US (1) US7124982B2 (fr)
EP (1) EP1397289B1 (fr)
AT (1) ATE356020T1 (fr)
DE (1) DE60218664T2 (fr)
ES (1) ES2281546T3 (fr)
SE (1) SE517133C2 (fr)
WO (1) WO2002098733A1 (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10301445B4 (de) * 2003-01-16 2005-11-17 Airbus Deutschland Gmbh Leichtbau-Strukturbauteil insbesondere für Flugzeuge und Verfahren zu seiner Herstellung
US8276847B2 (en) 2004-04-16 2012-10-02 Airbus Operations Gmbh Cover for an aircraft structure
DE102004018579A1 (de) * 2004-04-16 2005-11-03 Airbus Deutschland Gmbh Verkleidung für eine Struktur eines Flugzeugs
EP1666354B1 (fr) * 2004-12-01 2010-09-29 Airbus Operations GmbH Composant structurel, procédé de fabrication d'un composant structurel et utilisation d'un composant structurel dans le revêtement d'un aéronef
US8869673B2 (en) 2006-01-31 2014-10-28 Sikorsky Aircraft Corporation Structural panel with ballistic protection
US8709584B2 (en) * 2006-01-31 2014-04-29 Sikorsky Aircraft Corporation Composite aircraft floor system
US9097496B2 (en) 2006-04-20 2015-08-04 Sikorsky Aircraft Corporation Lightweight projectile resistant armor system with surface enhancement
DE102006026170B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026169B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026168A1 (de) 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
FR2906218B1 (fr) * 2006-09-21 2009-05-15 Airbus France Sas Raidisseur autostabilise autorisant une reprise d'elements
US7993479B2 (en) * 2006-09-27 2011-08-09 Airbus Deutschland Gmbh Method for joining precured or cured stringers to at least one structural component of an aircraft or spacecraft
US8091950B2 (en) * 2006-11-02 2012-01-10 University Of Notre Dame Du Lac Methods and apparatus for reducing drag via a plasma actuator
US8043458B2 (en) * 2007-06-21 2011-10-25 Sikorsky Aircraft Corporation Method of forming panels using an in-situ tape placement process and panels formed therefrom
US7867928B2 (en) * 2007-12-14 2011-01-11 Sikorsky Aircraft Corporation Fluid resistant composite sandwich panel
US7857191B2 (en) * 2008-06-16 2010-12-28 Embraer-Empresa Brasileira De Aeronautica S.A. Friction stir welding (FSW) methods and systems and friction stir welded components made thereby
US9545757B1 (en) * 2012-02-08 2017-01-17 Textron Innovations, Inc. Composite lay up and method of forming
US9016628B2 (en) * 2012-06-12 2015-04-28 The Boeing Company Methods and apparatus for reducing noise in reinforced skin structures
US10392132B2 (en) * 2016-07-29 2019-08-27 The Boeing Company Curved aircraft substructure repair systems and methods
CN206528613U (zh) * 2017-02-24 2017-09-29 深圳市大疆创新科技有限公司 无人机的机身及无人机

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2233969A (en) * 1938-12-30 1941-03-04 Bell Aircraft Corp Pressed wing rib
US2389767A (en) * 1943-09-01 1945-11-27 Budd Edward G Mfg Co Structural frame
US2427853A (en) * 1944-02-23 1947-09-23 Curtiss Wright Corp Aircraft construction
US4310132A (en) * 1978-02-16 1982-01-12 Nasa Fuselage structure using advanced technology fiber reinforced composites
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
JPH10258463A (ja) * 1997-03-19 1998-09-29 Fuji Heavy Ind Ltd 複合材の小骨およびその成形方法
DE19844035C1 (de) * 1998-09-25 1999-11-25 Daimler Chrysler Aerospace Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung
DE19922295C1 (de) * 1999-05-14 2000-07-27 Eurocopter Deutschland Unterbodenstruktur einer Rumpfzelle eines Luftfahrzeuges

Also Published As

Publication number Publication date
WO2002098733A1 (fr) 2002-12-12
DE60218664T2 (de) 2007-11-22
US20040195452A1 (en) 2004-10-07
ATE356020T1 (de) 2007-03-15
DE60218664D1 (de) 2007-04-19
EP1397289B1 (fr) 2007-03-07
SE0102009L (sv) 2002-04-16
SE0102009D0 (sv) 2001-06-05
EP1397289A1 (fr) 2004-03-17
ES2281546T3 (es) 2007-10-01
US7124982B2 (en) 2006-10-24

Similar Documents

Publication Publication Date Title
SE517133C2 (sv) Anordning för att stödja en skalyta i ett flygplansskrov
JP5055280B2 (ja) 翼用の支持構造
EP2955108B1 (fr) Structure de bec de bord d'attaque sur le stabilisateur vertical d'un aéronef
BR0102605A (pt) Componentes estrutural para um avião
ES2711074T3 (es) Estructuras alargadas y conjuntos relacionados
US7896402B2 (en) Spacer for coaxially sheathed fuel pipes
EP3334650B1 (fr) Ensemble porte d'aéronef muni d'espace creux à bruit réduit pouvant être recouvert par une porte d'aéronef
US7686249B2 (en) Integral frame member for an aircraft
US7931234B2 (en) Continuous fuselage connection
JP2011510859A (ja) 航空機や宇宙船における２つの異なる断面形状を有する２つの補強要素を連結するための連結構造体及び骨組み構造体
JP2017516703A (ja) 航空機胴体用の耐圧隔壁
EP0956915A3 (fr) Procédé et installation pour la fabrication d'ailes ou stabilisateurs pour avions
US20130328241A1 (en) Arrangement and method for manufacturing a wind turbine blade
KR200484346Y1 (ko) 창틀 고정용 브라켓
EP3112307A1 (fr) Carénage aérodynamique virtuel d'ascenseur
CN109263860A (zh) 一种机翼翼梁及机翼
FI120655B (fi) Kaidetolppa, kaide ja kuiturainakoneen hoitotasojärjestely
ES2912379T3 (es) Anclaje para unir el estabilizador de cola horizontal de una aeronave
ITTO960924A1 (it) Sistema di sopporto di una plancia di un autoveicolo
EP3498592B1 (fr) Avion
EP2796373A1 (fr) Gabarit de montage pour le montage des éléments de structure de panneau sur une surface en plastique renforcé par fibres de carbone (CFRP)
US11345098B2 (en) Continuous molded carbon fiber reinforced polymer slender curved component
JP6606336B2 (ja) 装備品懸架部材の設計方法
CN214427602U (zh) 激光雷达支架、激光雷达装置及车辆
JP2020074086A (ja) 装備品懸架部材の設計方法

Legal Events

Date Code Title Description
NUG Patent has lapsed