RU97101352A - METHOD FOR ASSEMBLING AN AIRPLANE FUSELAGE - Google Patents

METHOD FOR ASSEMBLING AN AIRPLANE FUSELAGE

Info

Publication number
RU97101352A
RU97101352A RU97101352/28A RU97101352A RU97101352A RU 97101352 A RU97101352 A RU 97101352A RU 97101352/28 A RU97101352/28 A RU 97101352/28A RU 97101352 A RU97101352 A RU 97101352A RU 97101352 A RU97101352 A RU 97101352A
Authority
RU
Russia
Prior art keywords
assembling
passenger compartment
fuselage
airplane fuselage
riveting
Prior art date
Application number
RU97101352/28A
Other languages
Russian (ru)
Other versions
RU2121452C1 (en
Inventor
В.М. Тихонов
Original Assignee
Закрытое акционерное общество "Саратовский авиационный завод"
Filing date
Publication date
Application filed by Закрытое акционерное общество "Саратовский авиационный завод" filed Critical Закрытое акционерное общество "Саратовский авиационный завод"
Priority to RU97101352A priority Critical patent/RU2121452C1/en
Priority claimed from RU97101352A external-priority patent/RU2121452C1/en
Application granted granted Critical
Publication of RU2121452C1 publication Critical patent/RU2121452C1/en
Publication of RU97101352A publication Critical patent/RU97101352A/en

Links

Claims (2)

1. Способ сборки фюзеляжа самолета, включающий сборку и клепку верхней части пассажирского салона, отличающийся тем, что сборку верхних панелей между собой производят в отдельном комплектовочном стапеле, после чего крупногабаритную верхнюю часть пассажирского салона устанавливают в поддерживающее устройство и клепают на клепальном автомате с ЧПУ, а затем верхнюю часть пассажирского салона устанавливают на фюзеляж.1. A method of assembling an aircraft fuselage, including assembling and riveting the upper part of the passenger compartment, characterized in that the upper panels are assembled together in a separate stocking frame, after which the large upper part of the passenger compartment is installed in a support device and riveted on a CNC riveting machine, and then the upper part of the passenger compartment is mounted on the fuselage. 2. Способ по п.1, отличающийся тем, что выем крупногабаритной верхней части пассажирского салона из комплектовочного стапеля, транспортировку и установку в поддерживающее устройство и на фюзеляж осуществляют при помощи траверсы, снабженной пружинными подвесками. 2. The method according to claim 1, characterized in that the removal of the large upper part of the passenger compartment from the pickup slip, transportation and installation in the supporting device and on the fuselage is carried out using a traverse equipped with spring suspensions.
RU97101352A 1997-01-24 1997-01-24 Method of assembly of aircraft fuselage RU2121452C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97101352A RU2121452C1 (en) 1997-01-24 1997-01-24 Method of assembly of aircraft fuselage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97101352A RU2121452C1 (en) 1997-01-24 1997-01-24 Method of assembly of aircraft fuselage

Publications (2)

Publication Number Publication Date
RU2121452C1 RU2121452C1 (en) 1998-11-10
RU97101352A true RU97101352A (en) 1999-01-27

Family

ID=20189442

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97101352A RU2121452C1 (en) 1997-01-24 1997-01-24 Method of assembly of aircraft fuselage

Country Status (1)

Country Link
RU (1) RU2121452C1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005054869A1 (en) 2005-11-17 2007-05-31 Airbus Deutschland Gmbh Method for producing a fuselage cell of an aircraft
FR2896767B1 (en) * 2006-01-30 2009-10-02 Airbus France Sas PILOTAGE STATION AND AEROPLANE HAVING SUCH A PILOTAGE STATION
DE102007028918A1 (en) * 2007-06-22 2009-01-02 Airbus Deutschland Gmbh Method for producing a fuselage cell of an aircraft and device
RU2452596C2 (en) * 2007-11-29 2012-06-10 Эйрбас Оперейшнс Сас Method of preparing joint of aircraft fuselage two sections
WO2009068107A1 (en) 2007-11-29 2009-06-04 Airbus France Sas Method of preparing the connection between two fuselage sections of an aircraft
CN105905313B (en) * 2016-04-01 2018-07-06 中航飞机股份有限公司西安飞机分公司 A kind of large transport airplane Integral floor mounting platform and installation method
CN105905312B (en) * 2016-04-01 2018-07-06 中航飞机股份有限公司西安飞机分公司 A kind of large transport airplane Integral floor mounting platform and its method for dismounting
US9817402B1 (en) * 2016-07-12 2017-11-14 The Boeing Company Application of factory automation for an airline assembly and build process
US10344906B2 (en) * 2017-01-27 2019-07-09 The Boeing Company Isolated human work platform for stabilized positioning of collaborative robotics
US10745251B2 (en) 2017-01-27 2020-08-18 The Boeing Company Belt drive dual robot gantry
RU2759013C1 (en) 2020-11-18 2021-11-08 Общество с ограниченной ответственностью «Нью Лайн Инжиниринг» Method for positioning elements of prefabricated structures in space

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