| 摘要 |
PURPOSE: A canard assembly and an aircraft including the same are provided to enable quick initial turning by using not only a pneumatic force but thrust generated in the lateral direction of the canard. CONSTITUTION: A first side thrust nozzle(610a) is extended from a first nozzle inlet to a first nozzle outlet, which is formed one side of a canard. A second side thrust nozzle(610b) is formed inside the canard as being extended from a second nozzle inlet to a second nozzle outlet, which is formed on the other side of the canard. The second side thrust nozzle has a flow path isolated from the first side thrust nozzle. The distance from the rotary axis of the canard to the first nozzle inlet is the same as the distance to the second nozzle inlet. The first and the second side thrust nozzle are selectively connected to a vent of a thruster, so that the thrust discharged from the vent is outputted through one of the first and the second nozzle outlet.
|
