Aerial vehicle with deployable components
First Claim
1. An unmanned aerial vehicle (UAV) comprising:
- a fuselage;
at least one stabilizer; and
wherein the base of the at least one stabilizer is configured to pivot about a first axis and a second axis,wherein the at least one stabilizer is configurable in at least the following arrangements;
a compact arrangement comprising;
the at least one stabilizer stowed against the fuselage, and a deployed arrangement comprising;
the least one stabilizer deployed from the fuselage about the first axis such that the deployment about the first axis places the at least one stabilizer in position to stabilize the UAV flight through a rotation of the at least one stabilizer about the second axis.
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Accused Products
Abstract
An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.
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Citations
20 Claims
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1. An unmanned aerial vehicle (UAV) comprising:
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a fuselage; at least one stabilizer; and wherein the base of the at least one stabilizer is configured to pivot about a first axis and a second axis, wherein the at least one stabilizer is configurable in at least the following arrangements; a compact arrangement comprising; the at least one stabilizer stowed against the fuselage, and a deployed arrangement comprising; the least one stabilizer deployed from the fuselage about the first axis such that the deployment about the first axis places the at least one stabilizer in position to stabilize the UAV flight through a rotation of the at least one stabilizer about the second axis. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. An unmanned aerial vehicle (UAV) comprising:
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at least one deployable stabilizer, wherein the at least one stabilizer is configurable in at least the following configurations; a stowed configuration positioned at a first angle relative to a first axis, and a deployed configuration pivoted at a second angle relative to the first axis, wherein the at least one stabilizer is in position, at the second angle relative to the first axis, to stabilize the UAV into a controlled flight through a pivot of the at least one stabilizer about the second axis. - View Dependent Claims (10, 11, 12, 13, 14)
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15. A method for operating a stabilizer on a unmanned aerial vehicle (UAV) comprising:
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arranging the stabilizer in a stowed position against a fuselage of the UAV; deploying the stabilizer from the stowed position to a deployed position, wherein deploying the stabilizer from the stowed position to the deployed position comprises pivoting the stabilizer about a first axis such that the deployment about the first axis places the stabilizer into the deployed position, and wherein the stabilizer is operable to stabilize the UAV into a controlled flight from the deployed position; and operating the stabilizer by enabling the stabilizer to pivot about a second axis in order to stabilize the UAV into the controlled flight. - View Dependent Claims (16, 17, 18, 19, 20)
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Specification