Multicopter with wide span rotor configuration and protective fuselage
An inner middle rotor is rotated while an inner front rotor, an inner back rotor, and an outer rotor are not rotated. The inner middle rotor is surrounded by the inner front rotor, the inner back rotor, the outer rotor, and a fuselage. After rotating the inner middle rotor while not rotating the inner front rotor, the inner back rotor, and the outer rotor, the inner middle rotor, the inner front rotor, the inner back rotor, and the outer rotor are simultaneously rotated.
1. A method, comprising:
rotating an inner middle rotor while not rotating an inner front rotor, an inner back rotor, and an outer rotor, wherein the inner middle rotor is surrounded by the inner front rotor, the inner back rotor, the outer rotor, and a fuselage; and
after rotating the inner middle rotor while not rotating the inner front rotor, the inner back rotor, and the outer rotor, simultaneously rotating the inner middle rotor, the inner front rotor, the inner back rotor, and the outer rotor.
2. The method recited in claim 1 , wherein:
the method further includes: prior to rotating an inner middle rotor while not rotating an inner front rotor, an inner back rotor, and an outer rotor, rotating the inner front rotor, the inner back rotor, and the outer rotor to be positioned tip-to-tip; and
the inner front rotor, the inner back rotor, and the outer rotor are positioned tip-to-tip while not rotating and while the inner middle rotor rotates.
3. The method recited in claim 1 , wherein:
the method further includes: prior to rotating the inner middle rotor while not rotating the inner front rotor, the inner back rotor, and the outer rotor, rotating the inner front rotor, the inner back rotor, and the outer rotor to be positioned tip-to-tip at an end of a first flight; and
the inner front rotor, the inner back rotor, and the outer rotor are positioned tip-to-tip while not rotating and while the inner middle rotor rotates during a second flight, wherein the second flight occurs after the first flight.
4. The method recited in claim 1 , wherein:
the method further includes: prior to rotating the inner middle rotor while not rotating the inner front rotor, the inner back rotor, and the outer rotor, rotating the inner front rotor, the inner back rotor, and the outer rotor to be positioned tip-to-tip; and
the inner front rotor, the inner back rotor, and the outer rotor are positioned tip-to-tip while not rotating and while the inner middle rotor rotates during a same flight as when the inner front rotor, the inner back rotor, and the outer rotor are rotated to be positioned tip-to-tip.
5. A computer program product, the computer program product being embodied in a non-transitory computer readable storage medium and comprising computer instructions for:
rotating an inner middle rotor while not rotating an inner front rotor, an inner back rotor, and an outer rotor, wherein the inner middle rotor is surrounded by the inner front rotor, the inner back rotor, the outer rotor, and a fuselage; and
after rotating the inner middle rotor while not rotating the inner front rotor, the inner back rotor, and the outer rotor, simultaneously rotating the inner middle rotor, the inner front rotor, the inner back rotor, and the outer rotor.
6. The computer program product recited in claim 5 , wherein:
the computer program product further includes computer instructions for: prior to rotating an inner middle rotor while not rotating an inner front rotor, an inner back rotor, and an outer rotor, rotating the inner front rotor, the inner back rotor, and the outer rotor to be positioned tip-to-tip; and
the inner front rotor, the inner back rotor, and the outer rotor are positioned tip-to-tip while not rotating and while the inner middle rotor rotates.
7. The computer program product recited in claim 5 , wherein:
the computer program product further includes computer instructions for: prior to rotating the inner middle rotor while not rotating the inner front rotor, the inner back rotor, and the outer rotor, rotating the inner front rotor, the inner back rotor, and the outer rotor to be positioned tip-to-tip at an end of a first flight; and
the inner front rotor, the inner back rotor, and the outer rotor are positioned tip-to-tip while not rotating and while the inner middle rotor rotates during a second flight, wherein the second flight occurs after the first flight.
8. The computer program product recited in claim 5 , wherein:
the computer program product further includes computer instructions for: prior to rotating the inner middle rotor while not rotating the inner front rotor, the inner back rotor, and the outer rotor, rotating the inner front rotor, the inner back rotor, and the outer rotor to be positioned tip-to-tip; and
the inner front rotor, the inner back rotor, and the outer rotor are positioned tip-to-tip while not rotating and while the inner middle rotor rotates during a same flight as when the inner front rotor, the inner back rotor, and the outer rotor are rotated to be positioned tip-to-tip.