Aircraft
AssigneeMitsubishi Aircraft Corporation
InventorsYoshinori OKABE, Kenya ISHIHARA, Zenta SUGAWARA
Life of this patent
Estimating the term…
Abstract
The present invention provides an aircraft including: a main wing; and a flight control surface that is deployed from the main wing in a first direction and in a second direction different from the first direction. In the aircraft, an end surface of the flight control surface facing the main wing when the flight control surface is not deployed is inclined with respect to the first direction or the second direction on at least one side of a longitudinal direction of the flight control surface, and a portion of the main wing facing the end surface is also inclined with respect to the first direction or the second direction in accordance with the end surface.
Claims19
An aircraft comprising:
- a main wing;
- and
- a flight control surface that is deployed from the main wing in a first direction and in a second direction different from the first direction,
- wherein an end surface of the flight control surface facing the main wing when the flight control surface is not deployed is inclined with respect to the first direction or the second direction on at least one side of a longitudinal direction of the flight control surface, and
- a portion of the main wing facing the end surface is also inclined with respect to the first direction or the second direction in accordance with the end surface.
An aircraft comprising:
- a main wing;
- and
- a flight control surface that is deployed from the main wing in a first direction and in a second direction different from the first direction,
- wherein only one of an end surface of the flight control surface facing the main wing when the flight control surface is not deployed and a portion of the main wing facing the end surface is inclined with respect to the first direction or the second direction on at least one side of a longitudinal direction of the flight control surface.
Dependencies are inferred from the claim text.