View source for 20250153841. Aircraft Wing-to-fuselage Inte (BOMBARDIER INC.)

= AIRCRAFT WING-TO-FUSELAGE INTERFACE PERMITTING POSITIONAL ADJUSTMENT =

'''Abstract''':
assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. in some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially defined by the fuselage portion. in some embodiments, the aircraft assemblies disclosed herein comprise one or more first structural interfaces that permit positional adjustment between the wing unit and the fuselage portion so that one or more second structural interfaces may be finished only after such positional adjustment. in some embodiments, the aircraft assemblies disclosed herein comprise one or more structural interfaces that are disposed outside of the wing unit in order to eliminate or reduce the need for assembly personnel to access the interior of the wing unit to carry out the structural assembly of the wing unit to the fuselage portion.

'''Inventor(s)''': [[:Category:Michael MURPHY of Whitby  CA|Michael MURPHY]], [[:Category:Jack ARAUJO of Ajax  CA|Jack ARAUJO]], [[:Category:Gary SHUM of Mississauga  CA|Gary SHUM]], [[:Category:George BRADLEY of Montreal  CA|George BRADLEY]]

'''CPC Classification''': [[:Category:CPC_B64C1/26|B64C1/26]] (AEROPLANES; HELICOPTERS)


[[Category:Patent Applications]]
[[Category:BOMBARDIER INC.]]
[[Category:CPC_B64C1/26]]
[[Category:Michael MURPHY of Whitby  CA]]
[[Category:Jack ARAUJO of Ajax  CA]]
[[Category:Gary SHUM of Mississauga  CA]]
[[Category:George BRADLEY of Montreal  CA]]

[https://wikipatents.org/index.php?search=20250153841+rejection&title=Special%3ASearch&wprov=acrw1_-1 Search for rejections for patent application number 20250153841]


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