Docking station of the wing with the center section
- Added: 23.03.2024
- Size: 82 KB
- Downloads: 0
Find out how to download this material
Subscribe to receive an information about new materials:
Description
To transfer forces from the wing panel, which operates on normal and shear stresses from bending, shear and torsion, to the center section , a flange (contour) joint is used, carried out with the help of a butt fitting made of a pressed profile (alloy B95). Usually, these fittings are made in one piece with the side rib belt. For the top panel, butt bolts are inserted into the fittings through vertical slots; For tightening the bolted connection, cutouts (sockets) are provided for the size of the wrench. Bolt loss during shaking and loosening is prevented by washers "recessed" into the body of the eyelet.
Project's Content
KR.frw
|
Similar materials
Free downloading for today
Update after: 23 hours 11 minutes
