Design of an instrumented workpart for robotic aircraft wing-box assembly
Thesis (S.B.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2006.
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| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2011
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| Online Access: | http://hdl.handle.net/1721.1/62992 |
| _version_ | 1811078625926053888 |
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| author | Kaina, Leighton |
| author2 | Harry Asada. |
| author_facet | Harry Asada. Kaina, Leighton |
| author_sort | Kaina, Leighton |
| collection | MIT |
| description | Thesis (S.B.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2006. |
| first_indexed | 2024-09-23T11:03:11Z |
| format | Thesis |
| id | mit-1721.1/62992 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T11:03:11Z |
| publishDate | 2011 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/629922019-04-11T01:43:08Z Design of an instrumented workpart for robotic aircraft wing-box assembly Kaina, Leighton Harry Asada. Massachusetts Institute of Technology. Dept. of Mechanical Engineering. Massachusetts Institute of Technology. Dept. of Mechanical Engineering. Mechanical Engineering. Thesis (S.B.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2006. Cataloged from PDF version of thesis. Includes bibliographical references (p. 15). The 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. by Leighton Kaina. S.B. 2011-05-23T17:58:31Z 2011-05-23T17:58:31Z 2006 2006 Thesis http://hdl.handle.net/1721.1/62992 720657266 eng M.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. http://dspace.mit.edu/handle/1721.1/7582 15 p. application/pdf Massachusetts Institute of Technology |
| spellingShingle | Mechanical Engineering. Kaina, Leighton Design of an instrumented workpart for robotic aircraft wing-box assembly |
| title | Design of an instrumented workpart for robotic aircraft wing-box assembly |
| title_full | Design of an instrumented workpart for robotic aircraft wing-box assembly |
| title_fullStr | Design of an instrumented workpart for robotic aircraft wing-box assembly |
| title_full_unstemmed | Design of an instrumented workpart for robotic aircraft wing-box assembly |
| title_short | Design of an instrumented workpart for robotic aircraft wing-box assembly |
| title_sort | design of an instrumented workpart for robotic aircraft wing box assembly |
| topic | Mechanical Engineering. |
| url | http://hdl.handle.net/1721.1/62992 |
| work_keys_str_mv | AT kainaleighton designofaninstrumentedworkpartforroboticaircraftwingboxassembly |