W Oltoria Di Un Uo Non Man at Taman Antonio La D
W OLTORIA DI UN USUO NON20180134382A1 MAN AT TAMAN ANTONIOLA D ( 19) United States (12 ) Patent Application Publication ( 10) Pub . No. : US 2018 /0134382 A1 Scholl et al. (43 ) Pub . Date : May 17 , 2018 ( 54 ) COMMERCIAL SUPERSONIC AIRCRAFT Publication Classification AND ASSOCIATED SYSTEMS AND (51 ) Int. Cl. METHODS B64C 30 / 00 (2006 .01 ) B64D 13 /08 ( 2006 . 01) ( 71) Applicant: Boom Technology, Inc. , Englewood , B64D 43 / 00 (2006 . 01 ) CO (US ) B64D 11 /06 ( 2006 .01 ) (72 ) Inventors : Nathaniel Blake Scholl, Englewood , (52 ) U . S . CI. CO (US ) ; Joe Wilding, Englewood , CO CPC . .. .. B64C 30 / 00 ( 2013 .01 ) ; B64D 13 / 08 (US ) ; Josh Krall, Englewood , CO (2013 .01 ) ; B64D 2013 /0618 (2013 .01 ) ; B64D (US ) ; Andy Berryann , Englewood , CO 11 / 064 (2014 . 12 ); B64D 43 / 00 ( 2013 .01 ) (US ) ; Michael Reid , Englewood , CO (US ) (57 ) ABSTRACT Commercial supersonic aircraft and associated systems and ( 21 ) Appl. No. : 15 /811 ,327 methods . A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between ( 22 ) Filed : Nov . 13 , 2017 20 and 60 passengers, a delta wing mounted to the fuselage , and a propulsion system carried by at least one of the wing Related U . S . Application Data and the fuselage , the propulsion system including a plurality (60 ) Provisional application No . 62 /421 , 870 , filed on Nov . of engines , at least one variable - geometry inlet , and at least 14 , 2016 . one variable - geometry nozzle . 101 103 100 102 51216 Chen 110 - - - - 000000 - -
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