The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Jan. 10, 2023
Filed:
Sep. 06, 2019
Applicant:
The Boeing Company, Chicago, IL (US);
Inventors:
Harinder S. Oberoi, Snohomish, WA (US);
Richard Griffith Reese, IV, Seattle, WA (US);
Kevin Marion Barrick, Kingston, WA (US);
Quang T. Do, Mukilteo, WA (US);
Alan S. Draper, Everett, WA (US);
Yuanxin Charles Hu, Newcastle, WA (US);
Alfredo Jose Gerosa, Snohomish, WA (US);
Michael J. Kozak, Snohomish, WA (US);
Jeffrey Lawrence Miller, Mukilteo, WA (US);
Assignee:
The Boeing Company, Chicago, IL (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64F 5/10 (2017.01); B21J 15/14 (2006.01); B23P 19/10 (2006.01); B21J 15/28 (2006.01); B21J 15/02 (2006.01); B21J 15/10 (2006.01); B60G 3/14 (2006.01); B25J 5/00 (2006.01); B29C 65/70 (2006.01); B25J 9/16 (2006.01); B25J 11/00 (2006.01); F16B 19/06 (2006.01); B60G 7/00 (2006.01); B21J 15/32 (2006.01); B21J 15/40 (2006.01); G05B 19/418 (2006.01); B25B 5/16 (2006.01); B29C 39/12 (2006.01); B29C 39/22 (2006.01); B64C 1/06 (2006.01); G05D 1/00 (2006.01); G05D 3/12 (2006.01); B29C 45/14 (2006.01); B29C 39/02 (2006.01); B29C 39/10 (2006.01); B64F 5/50 (2017.01); B23P 21/00 (2006.01); B29L 31/00 (2006.01); B60P 3/025 (2006.01);
U.S. Cl.
CPC ...
B21J 15/28 (2013.01); B21J 15/02 (2013.01); B21J 15/10 (2013.01); B21J 15/142 (2013.01); B21J 15/32 (2013.01); B21J 15/40 (2013.01); B23P 19/10 (2013.01); B25B 5/163 (2013.01); B25J 5/007 (2013.01); B25J 9/1682 (2013.01); B25J 9/1687 (2013.01); B25J 9/1697 (2013.01); B25J 11/005 (2013.01); B25J 11/007 (2013.01); B29C 39/026 (2013.01); B29C 39/10 (2013.01); B29C 39/123 (2013.01); B29C 39/22 (2013.01); B29C 45/14336 (2013.01); B29C 65/70 (2013.01); B60G 3/145 (2013.01); B60G 7/001 (2013.01); B60G 7/008 (2013.01); B64C 1/06 (2013.01); B64F 5/10 (2017.01); B64F 5/50 (2017.01); F16B 19/06 (2013.01); G05B 19/41805 (2013.01); G05D 1/0088 (2013.01); G05D 3/12 (2013.01); B23P 21/002 (2013.01); B23P 2700/00 (2013.01); B23P 2700/01 (2013.01); B29C 2045/14368 (2013.01); B29C 2793/0081 (2013.01); B29K 2715/00 (2013.01); B29L 2031/748 (2013.01); B60G 2204/143 (2013.01); B60G 2204/418 (2013.01); B60G 2206/8207 (2013.01); B60G 2300/60 (2013.01); B60P 3/025 (2013.01); G05B 2219/45071 (2013.01); Y02P 90/80 (2015.11); Y10S 901/01 (2013.01); Y10S 901/02 (2013.01); Y10S 901/41 (2013.01);
Abstract
An apparatus for accessing an interior of a fuselage assembly. A tower having a number of platform levels may be driven into a selected tower position within an assembly area. The interior of the fuselage assembly may be accessed using the number of platform levels.