Aerial vehicle such as high speed drone
By providing propellers for vertical ascent and descent and for horizontal flight, and a blade for horizontal flight, it is possible to obtain an aerial vehicle capable of high-speed horizontal flight and capable of flying a long distance.
1. An aerial vehicle comprising:
a first horizontal flight wing having two first propellers fixed on the first horizontal flight wing, each of the first propellers located at a center portion of a side of the first horizontal flight wing for ascending, descending, and advancing, the first horizontal flight wing configured to rotate vertically for the ascending and the descending using the first propellers, and configured to rotate horizontally with an angle of attack for the advancing and horizontal flight using the first propellers;
a second horizontal flight wing having two second propellers fixed on the second horizontal flight wing, each of the second propellers located at a center portion of a side of second horizontal flight wing for ascending, descending, and advancing, the second horizontal flight wing configured to rotate vertically for the ascending and the descending using the second propellers, and configured to rotate horizontally with an angle of attack for the advancing and horizontal flight using the second propellers; and
a combined landing gear and cargo carrier section adjacent to a center of gravity of the aerial vehicle, which serves as both a landing gear and a cargo carrier,
wherein the first horizontal flight wing and the second horizontal flight wing are located on a same horizontal plane on a fuselage of the aerial vehicle,
the first horizontal flight wing while positioned for horizontal flight has a first angle of attack and the second horizontal flight wing while positioned for horizontal flight has a second angle of attack, and
the first angle of attack is a different angle of attack from the second angle of attack.
2. An aerial vehicle comprising:
a first rotatable horizontal flight wing with first propellers for ascending and descending for vertical flight, and advancing for horizontal flight fixed on the first rotatable horizontal flight wing;
a second rotatable horizontal flight wing with second propellers for ascending and descending for vertical flight, and advancing for horizontal flight fixed on the second rotatable horizontal flight wing; and
a combined landing gear and cargo carrier section forming a shape having a base portion larger than a top portion and adjacent to a center of gravity of the aerial vehicle, which serves as both a landing gear and a cargo carrier,
wherein the first rotatable horizontal flight wing and the second rotatable horizontal flight wing are located on a same horizontal plane on a fuselage of the aerial vehicle,
the first rotatable horizontal flight wing while positioned for horizontal flight has a first angle of attack and the second rotatable horizontal flight wing while positioned for horizontal flight has a second angle of attack, and
the first angle of attack is a different angle of attack from the second angle of attack.
3. The aerial vehicle of claim 2 , having the horizontal flight wing for flying horizontally and a plurality of ascending, descending, and advancing propellers located on either side of the fuselage.
4. The aerial vehicle of claim 2 , comprising a plurality of propellers for ascent, descent and forward disposed on left, right, front and rear of the fuselage, and the horizontal flight wings for obtaining lift during horizontal flight are provided not to interfere with a slipstream of the ascending, descending and advancing propeller.
5. The aerial vehicle of claim 2 , wherein at least a portion of a plurality of ascent, descent and forward propellers are provided between the horizontal flight wings, so that the horizontal flight wings serve as guards for the plurality of ascent, descent and forward propellers.
6. The aerial vehicle of claim 2 , wherein the aircraft including a main wing forward tail wing rearward type, a tailless type, a tail wing forward main wing to rearward type, a same main wing forward and rearward type.
7. The aerial vehicle of claim 2 , further comprising a solar battery on a wing surface.
8. The aerial vehicle of claim 2 , wherein the combined landing gear and cargo carrier section forms a shape having a base portion larger than a top portion.