Design And Analysis Of UAV Wing Landing Gear Interface
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Date
2015-12-28T14:19:34Z
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Abstract
Unmanned Ariel Vehicle (UAV) is becoming an essential part of airpower as well as air
surveillance of every nation. Previously they were mainly used for air surveillance in high
security regions as well as in disaster struck region. Recently they are being deployed for
traffic surveillance and monitoring and even used for combat purposes in hostile regions.
This helps in reducing loss of lives and cost during mishaps. They are also used as flying
targets for testing Surface to Air Missiles (SAMs). The UAVs are piloted remotely through
ground stations or through other in flight controls. Some UAVs are developed to be selfguided.
The project deals with design and analysis of wing-engine frame-landing gear interface for
UAV. The landing gear interface is used for joining the engine frame with landing gear to
the center section of the wings through metallic ribs. The project deals with designing the
mounting interfaces and solid mapping the interfaces (3D mesh) and detailed local static
analysis of the interface for design load.
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Design And Analysis Of UAV Wing Landing Gear Interface, Prasanna Venkatesan S, Rajesh T, Abhishek Reddy