Unmanned aerial vehicle
First Claim
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1. An unmanned aerial vehicle comprising:
- a fuselage; and
a wing comprising a single central wing section pivotably mounted to the fuselage and a pair of outer wing sections pivotably mounted to the central wing section;
wherein the wing has a folded configuration in which the central wing section and the outer wing sections are stacked on top of one another and are aligned with a longitudinal axis of the fuselage, and a deployed configuration in which the central wing section is substantially perpendicular to the fuselage and the outer wing sections extend from the central wing section away from the fuselage.
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Abstract
An unmanned aerial vehicle 2 comprising: a fuselage 4; and a wing 6 comprising a central wing section 12 pivotably mounted to the fuselage 4 and a pair of outer wing sections 14a, 14b pivotably mounted to the central wing section 12; wherein the wing 6 has a folded configuration in which the central wing section 12 and the outer wing sections 14a, 14b are stacked on top of one another and are aligned with a longitudinal axis of the fuselage 4; and a deployed configuration in which the central wing section 12 is substantially perpendicular to the fuselage 4 and the outer wing sections 14a, 14b extend from the central wing section 12 away from the fuselage 4.
32 Citations
10 Claims
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1. An unmanned aerial vehicle comprising:
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a fuselage; and a wing comprising a single central wing section pivotably mounted to the fuselage and a pair of outer wing sections pivotably mounted to the central wing section; wherein the wing has a folded configuration in which the central wing section and the outer wing sections are stacked on top of one another and are aligned with a longitudinal axis of the fuselage, and a deployed configuration in which the central wing section is substantially perpendicular to the fuselage and the outer wing sections extend from the central wing section away from the fuselage. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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Specification