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dc.contributor.advisorHarry Asada.en_US
dc.contributor.authorKaina, Leightonen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Mechanical Engineering.en_US
dc.date.accessioned2011-05-23T17:58:31Z
dc.date.available2011-05-23T17:58:31Z
dc.date.copyright2006en_US
dc.date.issued2006en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/62992
dc.descriptionThesis (S.B.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2006.en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (p. 15).en_US
dc.description.abstractThe idea of an underactuated robotic arm used in aircraft wing assembly and production was created to improve the wing-box assembly process. In order to display the robots capabilities and areas of improvement, a suitable testing device would be most helpful. This project attempts to achieve an appropriate environment by creating a wing-box assembly imitating what would be found at a manufacturing plant. Secondly, the use of beacons to allow for the robot's careful positioning will help it identify certain tasks needed to be fulfilled. The initial design of the wing-box underwent various changes in order to account for financial and physical disturbances. These changes could have compromised the strength of the entire structure however, after the completion of the wing-box, the durability of the assembly surpassed any expectation. The beacon was designed under different specifications which addressed the problem of overall size and ease of assembly. While two of the designs addressed only one of those requirements separately, the third balanced the assembly problems while minimizing the size of the beacon. The third prototype was determined to be most desirable for production. The use of these projects will hopefully lead to the development of innovative technology in aircraft manufacturing.en_US
dc.description.statementofresponsibilityby Leighton Kaina.en_US
dc.format.extent15 p.en_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectMechanical Engineering.en_US
dc.titleDesign of an instrumented workpart for robotic aircraft wing-box assemblyen_US
dc.typeThesisen_US
dc.description.degreeS.B.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineering
dc.identifier.oclc720657266en_US


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