ES2169620A1 - Util para el montaje de secciones dek fuselaje de aeronaves. - Google Patents

Util para el montaje de secciones dek fuselaje de aeronaves.

Info

Publication number
ES2169620A1
ES2169620A1 ES009900124A ES9900124A ES2169620A1 ES 2169620 A1 ES2169620 A1 ES 2169620A1 ES 009900124 A ES009900124 A ES 009900124A ES 9900124 A ES9900124 A ES 9900124A ES 2169620 A1 ES2169620 A1 ES 2169620A1
Authority
ES
Spain
Prior art keywords
assembly
frame
mountings
components
fuselage
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
ES009900124A
Other languages
English (en)
Other versions
ES2169620B1 (es
Inventor
Martinez Manuel Torres
Albaladejo Francisco Vidal
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.)
M Torres Ingenieria de Procesos SL
Original Assignee
M Torres Ingenieria de Procesos SL
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 M Torres Ingenieria de Procesos SL filed Critical M Torres Ingenieria de Procesos SL
Priority to ES009900124A priority Critical patent/ES2169620B1/es
Priority to FR0000500A priority patent/FR2788743A1/fr
Publication of ES2169620A1 publication Critical patent/ES2169620A1/es
Application granted granted Critical
Publication of ES2169620B1 publication Critical patent/ES2169620B1/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • B23P19/04—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
    • 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
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/01—Aircraft parts

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automatic Assembly (AREA)
  • Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)

Abstract

Util para el montaje de secciones del fuselaje de aeronaves, formado por una estructura en donde previamente se realizan los laterales de las secciones de fuselaje, mediante la unión de dos respectivas semicarcasas en cada caso, y por una estructura (2) destinada para el montaje del conjunto de todas las partes componentes de las secciones de fuselaje, disponiendo cada una de las mencionadas estructuras de soportes adaptables para la sujeción de las piezas; en tanto que mediante unos útiles de transferencia (3), también adaptables, es realizable el traslado de los laterales formados, hasta la estructura (2) de montaje del conjunto.
ES009900124A 1999-01-22 1999-01-22 Util para el montaje de secciones del fuselaje de aeronaves. Expired - Fee Related ES2169620B1 (es)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ES009900124A ES2169620B1 (es) 1999-01-22 1999-01-22 Util para el montaje de secciones del fuselaje de aeronaves.
FR0000500A FR2788743A1 (fr) 1999-01-22 2000-01-17 Dispositif pour le montage de troncons du fuselage d'aeronefs

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES009900124A ES2169620B1 (es) 1999-01-22 1999-01-22 Util para el montaje de secciones del fuselaje de aeronaves.

Publications (2)

Publication Number Publication Date
ES2169620A1 true ES2169620A1 (es) 2002-07-01
ES2169620B1 ES2169620B1 (es) 2003-11-01

Family

ID=8307019

Family Applications (1)

Application Number Title Priority Date Filing Date
ES009900124A Expired - Fee Related ES2169620B1 (es) 1999-01-22 1999-01-22 Util para el montaje de secciones del fuselaje de aeronaves.

Country Status (2)

Country Link
ES (1) ES2169620B1 (es)
FR (1) FR2788743A1 (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2370324A1 (es) * 2009-08-17 2011-12-14 Aritex Cading, S.A. Equipo de gradas flexibles reconfigurables, aplicables para el montaje de alas de avion.

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19929471C1 (de) 1999-06-26 2001-01-18 Eads Airbus Gmbh Verfahren und Vorrichtung zur Herstellung eines dreidimensionalen Großbauteiles
US7624488B2 (en) * 2004-12-07 2009-12-01 The Boeing Company One-piece barrel assembly cart
DE102006062794B4 (de) * 2006-03-29 2010-04-22 Ima Materialforschung Und Anwendungstechnik Gmbh Prüfvorrichtung für spantverstärkte Rumpfschalen
DE102008044262B4 (de) 2008-12-02 2019-12-12 Airbus Operations Gmbh Vorrichtung und Verfahren zum Eintakten von Strukturbauteilen in einen Bauplatz
US8468674B2 (en) 2008-12-02 2013-06-25 Airbus Operations Gmbh Device and method for supplying structural components to an assembly zone
DE102011076841B4 (de) 2011-05-31 2016-02-18 Airbus Operations Gmbh Vorrichtungen zur Abbildung zumindest eines Abschnittes eines Flugzeugrumpfes
FR3002518B1 (fr) * 2013-02-28 2016-10-14 Dassault Aviat Dispositif d'aide au montage d'un element d'aeronef, poste de montage et procede associes
US10025288B2 (en) 2014-04-24 2018-07-17 Bae Systems Plc Machining fixture production
WO2015162403A1 (en) * 2014-04-24 2015-10-29 Bae Systems Plc Aircraft airframe assembly
WO2015162400A2 (en) 2014-04-24 2015-10-29 Bae Systems Plc Object production
US10364046B2 (en) 2014-04-24 2019-07-30 Bae Systems Plc Airframe production
ES2898091T3 (es) 2014-04-24 2022-03-03 Bae Systems Plc Producción de componentes de un armazón de aeronave
AU2015250687B2 (en) 2014-04-24 2018-10-04 Bae Systems Plc Assembly tool production
CN104309816B (zh) * 2014-10-29 2017-01-11 中航成飞民用飞机有限责任公司 飞机货舱门处壁板组件下架的方法及工具
GB2532451B (en) 2014-11-19 2018-12-26 Bae Systems Plc Object production
JP6513584B2 (ja) * 2016-02-02 2019-05-15 三菱重工業株式会社 保持治具固定装置
US10919746B2 (en) 2016-10-31 2021-02-16 The Boeing Company Flexible hydrostatically normalized cradle to support fuselage sections for assembly
FR3086268A1 (fr) * 2018-09-25 2020-03-27 Airbus Operations Procede d’assemblage d’un troncon de fuselage d’aeronef a partir de deux parties superieure et inferieure superposees, support de montage polyvalent, outillage et unite de production de troncons de fuselage pour la mise en œuvre dudit procede
FR3100232B1 (fr) 2019-08-30 2022-01-14 Airbus Ensemble comportant une tour support et au moins deux systemes de support pour des panneaux d’un troncon de fuselage d’un aeronef
US11427351B2 (en) * 2019-12-06 2022-08-30 The Boeing Company Carrier and operational frame system and methods of assembling a structure
EP4011784B1 (en) * 2020-12-14 2024-05-01 The Boeing Company Methods and apparatuses for decoupling a fuselage from a mandrel
US11772822B2 (en) 2021-01-26 2023-10-03 The Boeing Company Object lifting system and method
CN114291288A (zh) * 2022-01-05 2022-04-08 中国航空制造技术研究院 一种适用于机身装配的生产线系统
FR3138121A1 (fr) * 2022-07-25 2024-01-26 Airbus Operations Plateforme d’assemblage destinée à manipuler au moins une coque inférieure d’aéronef sans la déformer en vue d’un assemblage d’un corps de fuselage d’aéronef.
FR3138122A1 (fr) * 2022-07-25 2024-01-26 Airbus Operations Système de transport de grille de plancher de cabine d’aéronef en vue d’un assemblage d’un corps de fuselage d’aéronef et procédé de calibration dudit système de transport.
EP4311780A1 (fr) * 2022-07-25 2024-01-31 Airbus Operations SAS Dispositif référentiel de positionnement destiné à positionner l'un par rapport à l'autre au moins une grille de plancher de cabine et une coque latérale d'un aéronef en vue d'un assemblage d'un corps de fuselage de l'aéronef

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2374894A (en) * 1943-06-16 1945-05-01 Ford Motor Co Method and apparatus for assembling aircraft fuselages
US2486378A (en) * 1939-02-21 1949-11-01 Amiot Felix Construction of fuselages
EP0507033A1 (en) * 1991-04-05 1992-10-07 Manuel Torres Martinez Machine tool installation for supporting and machining workpieces
US5341556A (en) * 1991-06-28 1994-08-30 The United States Of America As Represented By The Secretary Of The Air Force Method and apparatus for manufacture of reinforced panels
US5649888A (en) * 1992-10-13 1997-07-22 The Boeing Company System for making a panel

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE713281C (de) 1938-06-14 1941-11-05 Messerschmitt Boelkow Blohm Verfahren zum Herstellen von Fluzeugbauteilen
DE712525C (de) 1939-03-14 1941-10-21 Messerschmitt Boelkow Blohm Spannvorrichtung zum Aufbau von aus Aussenhaut und Versteifungen bestehenden schussartigen Flugzeugschalenteilen
DE1010836B (de) 1939-08-30 1957-06-19 Messerschmitt Boelkow Blohm Baugeruest zur Herstellung halbschalenfoermiger Flugzeugzellenteile, insbesondere Rumpfteile
DE3341564A1 (de) 1983-11-17 1985-05-30 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2486378A (en) * 1939-02-21 1949-11-01 Amiot Felix Construction of fuselages
US2374894A (en) * 1943-06-16 1945-05-01 Ford Motor Co Method and apparatus for assembling aircraft fuselages
EP0507033A1 (en) * 1991-04-05 1992-10-07 Manuel Torres Martinez Machine tool installation for supporting and machining workpieces
US5341556A (en) * 1991-06-28 1994-08-30 The United States Of America As Represented By The Secretary Of The Air Force Method and apparatus for manufacture of reinforced panels
US5649888A (en) * 1992-10-13 1997-07-22 The Boeing Company System for making a panel

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2370324A1 (es) * 2009-08-17 2011-12-14 Aritex Cading, S.A. Equipo de gradas flexibles reconfigurables, aplicables para el montaje de alas de avion.

Also Published As

Publication number Publication date
FR2788743A1 (fr) 2000-07-28
ES2169620B1 (es) 2003-11-01

Similar Documents

Publication Publication Date Title
ES2169620A1 (es) Util para el montaje de secciones dek fuselaje de aeronaves.
FI933824A0 (fi) Matkustajien kuljetuslaite ja sitä varten tarkoitettu vaihtoaskelma sekä kuljetuslaitteen askelmaan liittyvät muunto- ja valmistusmenetelmät
ES2154498T3 (es) Dispositivo para el acoplamiento y desacoplamiento de una herramienta con respecto a un porta-herramientas.
GB2245241B (en) Airship with a supporting structure comprising frames and longitudinals
DE69906746D1 (de) Fliegend auf der matrize montierte nockeneinheit
SG79227A1 (en) Fiber-reinforced composite product with graded stiffness
PT1092172E (pt) Proteccao de fixacao para oculos e combinacao de uma proteccao amovivel e um par de oculos
HK1044877B (zh) 帶鏈節的錶帶及其組裝方法
IL107812A0 (en) Tag axle with rearwardly extending support framework
EP0455204A3 (en) Power source for dot matrix lcd
EP0920935A3 (de) Traggerüst für eine oszillierende Kokille
GB9006349D0 (en) Picture frame with quick changeable ornamentation assembly
DE29714217U1 (de) Verbindungsrahmen für standarisierte Solarmodule
KR950032338U (ko) 익형이 서로 다른 주날개를 호환할 수 있는 고정익 모형항공기용 받침대
Burkhardt et al. Demonstration centres for fibre composite materials--an aid for medium-sized businesses
DE29705863U1 (de) Verfahrbare Transportgestell, insbesondere für Möbel und Möbelteile
SI0948441T1 (en) Aircraft with a fuselage substantially designed as an aerostatic lifting body
GB9915950D0 (en) Air-craft aerofoil
GB2250710B (en) Fibre-reinforced elastomeric sheet
KR920009107U (ko) 셀프씨일커플링(self seal coupling) 착탈용 지그(Jig)
ITMI922066A0 (it) Profilato fermavetro in due parti accoppiate,per serramenti metallici in generale
ES1023965Y (es) Marco perfeccionado para marcos y similares.
ES1029324Y (es) Marco perfeccionado para sujecion de paneles publicitarios.
IT8720410V0 (it) Banco di esposizione con raffredamento ad aria ricircolata e, rispettivamente, con raffreddamento inerte.
PL101819U1 (en) Bogie frame for tank-cars, especially those with autocouplers

Legal Events

Date Code Title Description
EC2A Search report published

Date of ref document: 20020701

Kind code of ref document: A1

Effective date: 20020701

FG2A Definitive protection

Ref document number: 2169620B1

Country of ref document: ES

FD1A Patent lapsed

Effective date: 20040916