FUSELAGE STRUCTURE FOR ACCOMMODATING TAILS AND CANARDS OF DIFFERENT SIZES AND SHAPES

An aircraft includes a fuselage with structural interfaces for connection to any one or more of a variety of vertical tails, horizontal tails and canards. Vertical tails, horizontal tails and/or canards of different sizes, shapes, sweep angles, box chords, and/or root chords may connect to the fusel...

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Bibliographic Details
Main Authors Schmidt Gregory M, Walton Samuel Thomas
Format Patent
LanguageEnglish
Published 22.06.2017
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:An aircraft includes a fuselage with structural interfaces for connection to any one or more of a variety of vertical tails, horizontal tails and canards. Vertical tails, horizontal tails and/or canards of different sizes, shapes, sweep angles, box chords, and/or root chords may connect to the fuselage without changing the structural layout or configuration of the fuselage structural interfaces.
Bibliography:Application Number: US201514975115