Honeycomb panel construction methods
The aluminum Honeycomb panel is structured of the interlining of honeycomb type. It is a sort of a high strength external building material, which was just employed in the aeronautic industry in the past. honeycomb aluminum can hold an external load such as strong gust wind, typhoon and artificial load by spreading uniformly the external concentrated load into the internal hexagonal core column. The strength of dynamic aluminum honeycomb panel is as strong as iron material of the same thickness. Aluminum thin marble panel has the same function as fiberglass thin granite panel. Light weight: 3.70 pounds/sq.
Cores, in comparison to the supplemental structural value they add, are highly cost effective. With a sandwich floor panels, less material is necessary than with a solid structure. Core material is rock wool with density at 100kg/m3, the rock wool is upright against the surfaces. There are high strength vesicant between rock wools and surfaces. Core in a sandwich panel is comparable to the web of an I-beam, which supports the flanges and allows them to act as a unit. The web of the I-beam and the core of the sandwich panels hold the beam shear stresses. With a sandwich, less material is needed than with a solid structure.
Typically, an adhesive is used to bond the face sheets to the core for cleanroom panels. The adhesive must rigidly attach the facings or skins to the core in order for loads to be carried from one facing to the other and to permit the structure to fulfill all the assumptions implied in the acceptance of the commonly used stress calculation methods. Typically, two honeycomb core layers 2 and 3 will be provided, separated by a center septum 5. Facing skins 4 and 6 are provided on the front and rear surfaces, respectively, of the sandwich panel 1.
This entry was posted on Friday, July 31st, 2009 at 7:44 am and is filed under General. You can follow any responses to this entry through the RSS 2.0 feed. Both comments and pings are currently closed.