Patent ID: 9656748
Date: 2017-05-23
CPC Classifications: B64C,B64D,Y02T

Claim:
1. An aircraft capable of vertical take-off/landing, comprising: ailerons ( 1 , 2 ); a turbofan engine ( 3 ) including a low-temp duct ( 6 ) with an openable and closable propelling nozzle ( 7 ) and a high-temp duct ( 4 ) with an openable and closable propelling nozzle ( 5 ); a low-temp bypass duct ( 15 ) including an openable and closable inlet ( 14 ) connected to the low-temp duct ( 6 ), an outer wall ( 16 ), an inner wall ( 17 ) and a thin slot outlet ( 19 ) set on the upper surface of the wing and in the direction of the wingspan; and a high-temp bypass duct ( 9 ) including an openable and closable inlet ( 8 ) connected to the high-temp duct ( 4 ), an outer wall ( 10 ) and a thin slot outlet ( 12 ) set above the thin slot outlet ( 19 ) of the low-temp bypass duct ( 15 ) in the direction of the wingspan.