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Optimized bolted joint
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hart-Smith, L. J. Bunin, B. L. |
| Copyright Year | 1986 |
| Description | A method is disclosed for joining segments of the skin of an aircraft. The ends of the skin are positioned in close proximity or abutt each other. The skin is of constant thickness throughout the joint and is sandwiched between splice plates, which taper in thickness from the last to the first bolt rows in order to reduce the stiffness of the splice plate and thereby reduce the load transfer at the location where bypass loads are the highest. |
| File Size | 569220 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860018158 |
| Archival Resource Key | ark:/13960/t08w89b0g |
| Language | English |
| Publisher Date | 1986-04-01 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Thickness Joints Junctions Splicing Plates Structural Members Bolted Joints Bolts Skin Structural Member Composite Structures Aircraft Structures Load Distribution Forces Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
