ES2112711A1 - Estructura para aviones. - Google Patents

Estructura para aviones.

Info

Publication number
ES2112711A1
ES2112711A1 ES09401145A ES9401145A ES2112711A1 ES 2112711 A1 ES2112711 A1 ES 2112711A1 ES 09401145 A ES09401145 A ES 09401145A ES 9401145 A ES9401145 A ES 9401145A ES 2112711 A1 ES2112711 A1 ES 2112711A1
Authority
ES
Spain
Prior art keywords
frames
tube
aircraft
ribs
correlation
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
ES09401145A
Other languages
English (en)
Other versions
ES2112711B1 (es
Inventor
Martinez Manuel Torres
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to ES09401145A priority Critical patent/ES2112711B1/es
Publication of ES2112711A1 publication Critical patent/ES2112711A1/es
Application granted granted Critical
Publication of ES2112711B1 publication Critical patent/ES2112711B1/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64C1/061—Frames
    • 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
    • B64C1/065—Spars

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Tires In General (AREA)
  • Laminated Bodies (AREA)

Abstract

ESTRUCTURA PARA AVIONES, QUE SE DETERMINA POR UNA CORRELACION DE CUADERNAS (1) MUY PROXIMAS ENTRE SI E INTERRELACIONADAS, POR, AL MENOS UN TUBO (6) QUE SE EXTIENDE A TODO LO LARGO DE LA PARTE INFERIOR DEL FUSELAJE RECUBIERTO POR UNOS GRANDES PANELES QUE, AL IGUAL QUE LAS CUADERNAS (1) Y EL TUBO (6) SE CONSTITUYEN EN FIBRA DE CARBONO.
ES09401145A 1994-05-25 1994-05-25 Estructura para aviones. Expired - Lifetime ES2112711B1 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES09401145A ES2112711B1 (es) 1994-05-25 1994-05-25 Estructura para aviones.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES09401145A ES2112711B1 (es) 1994-05-25 1994-05-25 Estructura para aviones.

Publications (2)

Publication Number Publication Date
ES2112711A1 true ES2112711A1 (es) 1998-04-01
ES2112711B1 ES2112711B1 (es) 1998-12-01

Family

ID=8286381

Family Applications (1)

Application Number Title Priority Date Filing Date
ES09401145A Expired - Lifetime ES2112711B1 (es) 1994-05-25 1994-05-25 Estructura para aviones.

Country Status (1)

Country Link
ES (1) ES2112711B1 (es)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007141291A1 (en) * 2006-06-06 2007-12-13 Airbus Deutschland Gmbh Aircraft fuselage structure and method for its production
US8534605B2 (en) 2006-06-06 2013-09-17 Airbus Operations Gmbh Aircraft fuselage structure and method for producing it
EP3040265A1 (en) * 2015-01-02 2016-07-06 Airbus Operations GmbH Method for joining two fuselage sections and mounting device
FR3043646A1 (fr) * 2015-11-17 2017-05-19 Airbus Operations Sas Ensemble structurel pour fuselage d'aeronef a double courbure comprenant des cadres a orientation optimisee

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006026170B4 (de) 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
FR2980766B1 (fr) * 2011-09-30 2013-10-25 Airbus Operations Sas Structure de pointe avant d'aeronef et aeronef correspondant

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR880181A (fr) * 1941-02-10 1943-03-16 Messerschmitt Ag Fuselage d'avion en coque
US2387219A (en) * 1941-08-08 1945-10-16 Vickers Armstrongs Ltd Aircraft structure
US4531695A (en) * 1983-01-25 1985-07-30 Westland Plc Composite helicopter fuselage
EP0273466A2 (en) * 1986-12-31 1988-07-06 The Boeing Company Aircraft
FR2629045A1 (fr) * 1988-03-22 1989-09-29 Mounier Poulat Francois Architecture d'avion leger a moteur central
US5171510A (en) * 1988-06-08 1992-12-15 Aerospatiale Societe Nationale Industrielle Method of producing a frame made of a composite material, especially for the fuselage of an aircraft
US5435504A (en) * 1993-03-09 1995-07-25 Honda Giken Kogyo Kabushiki Kaisha Aircraft

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR880181A (fr) * 1941-02-10 1943-03-16 Messerschmitt Ag Fuselage d'avion en coque
US2387219A (en) * 1941-08-08 1945-10-16 Vickers Armstrongs Ltd Aircraft structure
US4531695A (en) * 1983-01-25 1985-07-30 Westland Plc Composite helicopter fuselage
EP0273466A2 (en) * 1986-12-31 1988-07-06 The Boeing Company Aircraft
FR2629045A1 (fr) * 1988-03-22 1989-09-29 Mounier Poulat Francois Architecture d'avion leger a moteur central
US5171510A (en) * 1988-06-08 1992-12-15 Aerospatiale Societe Nationale Industrielle Method of producing a frame made of a composite material, especially for the fuselage of an aircraft
US5435504A (en) * 1993-03-09 1995-07-25 Honda Giken Kogyo Kabushiki Kaisha Aircraft

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007141291A1 (en) * 2006-06-06 2007-12-13 Airbus Deutschland Gmbh Aircraft fuselage structure and method for its production
US8534605B2 (en) 2006-06-06 2013-09-17 Airbus Operations Gmbh Aircraft fuselage structure and method for producing it
US8695922B2 (en) 2006-06-06 2014-04-15 Airbus Operations Gmbh Aircraft fuselage structure and method for its production
EP3040265A1 (en) * 2015-01-02 2016-07-06 Airbus Operations GmbH Method for joining two fuselage sections and mounting device
FR3043646A1 (fr) * 2015-11-17 2017-05-19 Airbus Operations Sas Ensemble structurel pour fuselage d'aeronef a double courbure comprenant des cadres a orientation optimisee
US10427773B2 (en) 2015-11-17 2019-10-01 Airbus Operations (S.A.S.) Structural assembly for an aircraft fuselage with double curvature including frames with an optimized orientation

Also Published As

Publication number Publication date
ES2112711B1 (es) 1998-12-01

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