RU97101352A - METHOD FOR ASSEMBLING AN AIRPLANE FUSELAGE - Google Patents
METHOD FOR ASSEMBLING AN AIRPLANE FUSELAGEInfo
- 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
Links
- 238000009434 installation Methods 0.000 claims 1
- 239000000725 suspension Substances 0.000 claims 1
- 238000004642 transportation engineering Methods 0.000 claims 1
Claims (2)
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)
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 |
-
1997
- 1997-01-24 RU RU97101352A patent/RU2121452C1/en active
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