FIELD: aircraft manufacture. SUBSTANCE: permanent construction joint has upper and lower joint profiles of center section connected respectively with upper and lower panels of wing by their weds. Joint includes also spars with vertical struts, bands, walls and ribs with their connecting members. Upper panel of wing is provided with cutouts for connecting members. Walls of spars have detachable sections extending from plane of joint as far as rib which is parallel to plane of joint. Web of upper joint profile of center section is located above upper panel of wing overlapping it. EFFECT: ease of assembly of aircraft due to sectional assembly of center section and wing in separate jigs followed by rejoining in general jig.
Title | Year | Author | Number |
---|---|---|---|
OUTER WING JOINT WITH AIRCRAFT CENTER SECTION | 2016 |
|
RU2621925C1 |
AIRFRAME OF MULTIMODE MONOPLANE | 1997 |
|
RU2173654C2 |
AIRCRAFT WING | 2014 |
|
RU2557638C1 |
AIRCRAFT WING, AIRCRAFT WINGS CAISSON, CENTER WING, SPAR (VERSIONS) | 2019 |
|
RU2709976C1 |
METHOD OF MODULAR ASSEMBLY OF A SPLICE RIB OF AN AIRCRAFT FOR CONNECTING WING CONSOLES WITH THE CENTER WING AND APPARATUS FOR IMPLEMENTATION OF THE METHOD | 2020 |
|
RU2749432C1 |
AIRCRAFT WING AND OUTER WING JOINT ASSEMBLY | 2012 |
|
RU2481243C1 |
JOINT BETWEEN AIRCRAFT CENTRE WING SECTION AND OUTER WING | 2014 |
|
RU2556268C1 |
AIRCRAFT WING | 1997 |
|
RU2140375C1 |
METHOD FOR MODULAR ASSEMBLY OF THE BOX OF AN AIRCRAFT WING CONSOLE WITH PARTS MADE OF CARBON POLYMER COMPOSITE MATERIALS AND METALS AND AN ASSEMBLY LINE WITH DEVICES FOR IMPLEMENTING THE METHOD | 2021 |
|
RU2774870C1 |
METHOD FOR ASSEMBLING WING OF FLYING APPARATUS | 2016 |
|
RU2657816C1 |
Authors
Dates
1996-09-20—Published
1981-12-11—Filed