[특허]Amphibious aircraft

Leader Industries, Inc.

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Amphibious aircraft

국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-025/54 B64C-035/00
미국특허분류(USC)	244/101; 244/105; 244/108
출원번호	US-0667874 (2012-11-02)
등록번호	US-8807478 (2014-08-19)
발명자 / 주소	Meekins, John A. Husa, William
출원인 / 주소	Leader Industries, Inc.
대리인 / 주소	Kilpatrick Townsend & Stockton LLP
인용정보	피인용 횟수 : 0 인용 특허 : 24

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Described are aircraft with at least one fuselage, a wing, and at least one float coupled to the wing. As examples, each float may include a step that is located forward of or at an intersection of a bottom surface and a line that extends from an aircraft aft-most center of gravity at an angle of less than ten degrees rearward from a vertical direction. As further examples, each float may include a forward portion located forward of the step, the forward portion including a ski surface that is planar in a left to right horizontal direction, and an aft po...

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1. An aircraft configured to take off and land on water, the aircraft including at least one fuselage and at least one wing connected to the fuselage, the aircraft including an aft-most center of gravity and at least one float, the float comprising: a float body that includes a bottom surface;a bottom surface forward portion located on the float body bottom surface, the bottom surface forward portion including a ski surface that is planar in a left-to-right horizontal direction;a bottom surface rearward portion located on the float body bottom surface, the bottom surface rearward portion including a rudder; anda bottom surface step located on the float body bottom surface and interposed between the bottom surface forward portion and the bottom surface rearward portion, the step including a point that is located forward of or at an intersection of the bottom surface and a line that extends from the aircraft aft-most center of gravity at an angle of less than ten degrees rearward from a vertical direction. 2. An aircraft according to claim 1, wherein the step includes a point that is located forward of or at the intersection of the bottom surface and a line that extends from the aircraft aft-most center of gravity at an angle greater than six and less than ten degrees rearward from the vertical direction. 3. An aircraft according to claim 1, wherein the step includes a point that is located forward of or at the intersection of the bottom surface and a line that extends from the aircraft aft-most center of gravity at an angle of five degrees rearward from the vertical direction. 4. An aircraft according to claim 1, wherein the at least one float includes a center of buoyancy on a line extending vertically from the aircraft aft-most center of gravity and rearward of the bottom surface step when the aircraft is at rest on the water. 5. An aircraft according to claim 1, wherein the at least one float includes a center of buoyancy that is located forward of the bottom surface step during takeoff of the aircraft. 6. An aircraft according to claim 1, wherein the at least one float is connected to the at least one wing. 7. An aircraft according to claim 1, wherein the aircraft includes two floats. 8. An aircraft according to claim 1, wherein the at least one float includes at least one landing gear. 9. An aircraft according to claim 8, wherein the at least one landing gear includes at least one wheel. 10. An aircraft according to claim 1, wherein the float body includes a nose and the ski surface includes a convergent portion wherein a pair of edges of the ski surface converge toward the nose of the float body. 11. An aircraft according to claim 10, wherein at least part of the bottom surface forward portion is concave in cross section. 12. An aircraft according to claim 11, wherein at least part of the bottom surface forward portion includes a pair of streamline surfaces that are concave in cross section adjacent the ski surface convergent portion. 13. An aircraft configured to take off and land on water, the aircraft including at least one fuselage and at least one wing connected to the fuselage, the aircraft including an aft-most center of gravity and at least one float, the float comprising: a float body that includes a bottom surface and a nose;a bottom surface forward portion located on the float body bottom surface, the bottom surface forward portion including: a ski surface that is planar in a left-to-right horizontal direction, wherein the ski surface includes a convergent portion toward the nose of the float body; anda pair of streamline surfaces that are concave in cross section adjacent the convergent portion of the ski surface;a bottom surface rearward portion located on the float body bottom surface, the bottom surface rearward portion including a rudder; anda bottom surface step located on the float body bottom surface and interposed between the bottom surface forward portion and the bottom surface rearward portion, the step including a point that is located forward of or at an intersection of the bottom surface and a line that extends from the aircraft aft-most center of gravity at an angle of less than ten degrees rearward from a vertical direction. 14. An aircraft according to claim 13, wherein the step includes a point that is located forward of or at the intersection of the bottom surface and a line that extends from the aircraft aft-most center of gravity at an angle greater than six and less than ten degrees rearward from the vertical direction. 15. An aircraft according to claim 13, wherein the step includes a point that is located forward of or at the intersection of the bottom surface and a line that extends from the aircraft aft-most center of gravity at an angle of five degrees rearward from the vertical direction. 16. An aircraft according to claim 13, wherein the at least one float includes a center of buoyancy on a line extending vertically from the aircraft aft-most center of gravity and rearward of the bottom surface step when the aircraft is at rest on the water. 17. An aircraft according to claim 13, wherein the at least one float includes a center of buoyancy that is located forward of the bottom surface step during takeoff of the aircraft. 18. An aircraft according to claim 13, wherein the at least one float is connected to the at least one wing. 19. An aircraft according to claim 13, wherein the aircraft includes two floats. 20. An aircraft according to claim 13, wherein the at least one float includes at least one landing gear. 21. An aircraft according to claim 20, wherein the at least one landing gear includes at least one wheel.

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Amphibious aircraft

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Amphibious aircraft

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