Structural joint developed for attachment of hypersonic control surface to aircraft wing structure. Transmits large torque loads from composite control surface and torque tube to wing structure through metallic attachment lug and collar. Torque load transmitted from tube to collar by series of radially oriented cleats. Bearing surfaces of cleats plane passing through center-line of torque tube. Such joints accommodate differential thermal growth between parts of dissimilar materials. Potential for application to high-temperature structural joints associated with hypervelocity vehicles.
Low-Thermal-Stress Structural Joints For Dissimilar Materials
NASA Tech Briefs ; 14 , 11
1990-11-01
Sonstige
Keine Angabe
Englisch
Comparative Study of Dissimilar Materials Joints
SAE Technical Papers | 2019
|Joints between dissimilar metallic and ceramic materials
British Library Online Contents | 1992
|Finite Element Analyses of Structural Stresses near Dissimilar Spot Joints in Lap-Shear Specimens
SAE Technical Papers | 2019
|Joining technologies to realize dissimilar joints for automotive applications
Kraftfahrwesen | 2001
|