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AIRCRAFT STRUCTURE LAB EQUIPMENT

We proudly presents its latest project, the Aircraft Structure Lab equipment, designed to provide cutting-edge, precise tools for advanced aerospace research and education. Reflecting our commitment to innovation and quality, this equipment enhances structural analysis and testing capabilities, supporting the future progress of the aviation industry.

BEAM TEST SETUP

HINGED BAR SUSPENDED BY TWO WIRES OF DIFFERENT MATERIALS (BIFILAR SUSPENSION SYSTEM)

SETUP FOR TRANSVERSE VIBRATION OF BEAMS WITH DIFFERENT END CONDITIONS

SETUP FOR LOGARITHMIC DECREMENT OF A DAMPED SYSTEM

SETUP FOR MEASUREMENT OF DISPLACEMENT, VELOCITY, ACCELERATION AND PHASE LAG IN FORCED VIBRATION SYSTEM

UNSYMMETRICAL BENDING OF BEAMS –Z’ SECTION

SHEAR CENTRE LOCATION FOR OPEN SECTION – CHANNEL

DROP WEIGHT IMPACT TEST RIG

Constant Strength beam

FLEXIBILITY MATRIX FOR CANTILEVER BEAM

BEAM WITH COMBINED LOADING

PHOTOELASTIC APPARATUS

VIBRATION OF BEAMS – FREE, FORCED AND TORSIONAL

WAGNER BEAM – TENSION FIELD BEAM

IMPACT DROP WEIGHT TESTING MACHIN.png

AUTOCLAVE FURNACE 500L

SHEAR CENTER OF CLOSED SECTION

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