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US 11,453,495 B1Granted
Double wing aircraft and method of use
OwnerKhaled Abdullah Alhussaninventor
Life of this patent
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Abstract
A dual-wing aircraft includes a body extending from a front end to a rear end; a front wing, having: a first section secured to the body; and a second section secured to an opposing side of the body; a rear wing, having: a third section secured to the body; and a fourth section secured to the opposing side of the body; a tail wing rigidly attached to the body and positioned between the front wing and the rear wing.
Claims6
A dual-wing aircraft, comprising:
- a front wing;
- a rear wing;
- a body extending from a front end to a rear end, the body having a narrow section between the front wing and the rear wing and near a center line of the body, the narrow section being formed by tapering of the body before and after the narrow section;
- the front wing having:
- a first section secured to the body;
- and
- a second section secured to an opposing side of the body;
- the rear wing having:
- a first section secured to the body;
- and
- a second section secured to an opposing side of the body;
- a propulsion system attached to the narrow section of the body and at a top surface of the body;
- and
- a vertical stabilizer attached to the propulsion system and positioned between the front wing and the rear wing, the vertical stabilizer extending vertically away from the propulsion system and the body.
11 more elements
Dependencies are inferred from the claim text.