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A rotational arm connection point design for a C-130 aircraft standardized sensor platform

Posted on:2007-11-22Degree:M.S.M.EType:Thesis
University:West Virginia UniversityCandidate:Williams, Kenneth AFull Text:PDF
GTID:2442390005979620Subject:Engineering
Abstract/Summary:PDF Full Text Request
West Virginia University's Center for Industrial Research Applications (CIRA) was sponsored by the United States Army National Guard (USANG) and the Department of Defense (DOD) to design a standardized, articulating sensor platform for the C-130 Hercules military aircraft. This sensor platform was to be capable of in-flight deployment and capable of facilitating a diverse spectrum of sensor configurations in order to aid in surveillance and reconnaissance for counter narco-terrorism efforts. Two complete sensor pallet prototypes have been developed. The current platform configuration consists of four aluminum arms that are connected to a rotational shaft via a cylindrical hub. For the construction of the third prototype of the sensor platform, an optimization of the rotational arm-hub connection was performed. The goal of the new design was to allow for easier system assembly, maintenance, and the ability to carry a larger sensor payload. The following work describes the complete design and development of the new arm-hub connection through the use of both analytical and finite element analysis (FEA) using Pro-Engineer and Pro-Mechanica solid modeling software.
Keywords/Search Tags:Sensor, Connection, Rotational
PDF Full Text Request
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