IN2014CH00463AIN463CH2014AIN2014CH00463AIN 2014CH00463 AIN2014CH00463 AIN 2014CH00463AIN 463CH2014 AIN463CH2014 AIN 463CH2014AIN 2014CH00463 AIN2014CH00463 AIN 2014CH00463A
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IN
India
Prior art keywords
structure made
section
kevlar
aluminium
relations
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Application number
Inventor
Srikari S
Subbaramu S
Prashanth Manvi S
Original Assignee
M S Ramaiah School Of Advanced Studies Bangalore
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Application filed by M S Ramaiah School Of Advanced Studies BangalorefiledCriticalM S Ramaiah School Of Advanced Studies Bangalore
Priority to IN463CH2014priorityCriticalpatent/IN2014CH00463A/en
Publication of IN2014CH00463ApublicationCriticalpatent/IN2014CH00463A/en
According to an aspect of the present invention, a composite material based on honeycomb core structure made of Kevlar material which is sandwiched between stiffened aluminium panels is developed. A sample material is studied under various physical condition in relations to commonly used materials such as I section and HAT section. It is found that the honeycomb structure made with Kevlar material in between two aluminium sheets provided greater load bearing capacity while lowering the mass for an Aircraft construction.
Efficient production of composite components and semi-finished products in a wet pressing method using hydroxy-functionalised (meth) acrylates that are duroplastically crosslinked with the use of isocyanates or uretdiones are duroplasticly crosslinked with the use of isocyanates or uretdiones