Multicopter with wide span rotor configuration and protective fuselage
First Claim
1. An aircraft, comprising:
- a fuselage which includes an unenclosed cockpit;
a left arm, wherein a proximal end of the left arm is attached to the fuselage;
a right arm, wherein a proximal end of the right arm is attached to the fuselage;
a left float, wherein the left float is attached to the left arm between the proximal end of the left arm and the distal end of the left arm;
a right float, wherein the right float is attached to the right arm between the proximal end of the right arm and the distal end of the right arm; and
a plurality of rotors, wherein;
the plurality of rotors includes a left inner rotor that is attached at a fixed angle to a top surface of the left float;
the plurality of rotors includes a right inner rotor that is attached at a fixed angle to a top surface of the right float;
the plurality of rotors includes a left outer rotor that is attached at a fixed angle to a top surface of the distal end of the left arm; and
the plurality of rotors includes a right outer rotor that is attached at a fixed angle to a top surface of the distal end of the right arm.
6 Assignments
0 Petitions
Accused Products
Abstract
An aircraft includes a fuselage which includes an unenclosed cockpit, a left arm where the proximal end is attached to the fuselage, a right arm where the proximal end is attached to the fuselage, a left float which is attached to the left arm between the proximal and distal ends, a right float which is attached to the right arm between the proximal and distal ends, and a plurality of rotors which includes a left inner rotor that is attached at a fixed angle to a top surface of the left float, a right inner rotor that is attached at a fixed angle to a top surface of the right float, a left outer rotor that is attached at a fixed angle to a top surface of the distal end of the left arm, and a right outer rotor that is attached at a fixed angle to a top surface of the distal end of the right arm.
64 Citations
13 Claims
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1. An aircraft, comprising:
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a fuselage which includes an unenclosed cockpit; a left arm, wherein a proximal end of the left arm is attached to the fuselage; a right arm, wherein a proximal end of the right arm is attached to the fuselage; a left float, wherein the left float is attached to the left arm between the proximal end of the left arm and the distal end of the left arm; a right float, wherein the right float is attached to the right arm between the proximal end of the right arm and the distal end of the right arm; and a plurality of rotors, wherein; the plurality of rotors includes a left inner rotor that is attached at a fixed angle to a top surface of the left float; the plurality of rotors includes a right inner rotor that is attached at a fixed angle to a top surface of the right float; the plurality of rotors includes a left outer rotor that is attached at a fixed angle to a top surface of the distal end of the left arm; and the plurality of rotors includes a right outer rotor that is attached at a fixed angle to a top surface of the distal end of the right arm. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
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Specification