Full scale Structural Testing facility
Full scale structural tests are essential to qualify the structure for flight. ACD- NAL has state-of-the-art test facility to conduct static and fatigue testing for full-scale aircraft composite structures and major components. The facility is managed by technical personnel having experience in structural testing of variety of aircraft structures in a cost-effective and timely manner.
The facility consists of equipment and systems capable of carrying out tests towards
- Performance of static & fatigue load tests on primary airframes, subsystems and components
- Investigations into damage tolerance characteristics, crack propagation and residual strength
- Determination of deformations, stiffness, fracture strength and fracture characteristics
- Development of test concepts, test fixtures, load frames and post-test documentation
Specifications
This facility consists of
- MTS hydraulic power supply unit of up to 100 lpm at 3000 psi
- 10 channel Servo Control system and extendable up to 32 channels (capacity of 53 ton servo controlled hydraulic jacks)
- Capacity of 50 ton manual control hydraulic loading cylinders
- 24 channels Universal Data acquisition system for static and fatigue measurement of strain, displacement, pressure and temperature
- 10 non contact,18 draw–wire sensors for displacement measurements
- High capacity (100 ton) dynamic axial test system
Major clients of this facility:
Government, public sector, PSU private sectors, R&D establishments, DRDO and Educational Institutes