External load mass rope of a rotorcraft
US-2015360779-A1 · Dec 17, 2015 · US
US9751627B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9751627-B2 |
| Application number | US-201514631025-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 25, 2015 |
| Priority date | May 29, 2012 |
| Publication date | Sep 5, 2017 |
| Grant date | Sep 5, 2017 |
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A system of transporting micro-cargo incorporates an unmanned aerial vehicle (UAV) having a tether capture device. A tether is connected to and suspends a micro cargo container with a suspension system to vertically extend the tether. The system having a first pickup state and a second flight state with a transition between the first and second states. The first state provides the micro-container unsuspended via the tether from the suspension system. The transition state provides engagement of the tether by the UAV, the tether positioning the micro-cargo container with respect to the capture device which secures the tether. The second state is then entered with the micro-cargo towed by the UAV in cruising flight to its destination.
Opening claim text (preview).
What is claimed is: 1. A method for transport of micro cargo comprising: loading a micro cargo into a micro cargo container; suspending the micro cargo container on a tether in a vertical state; constraining the micro cargo container with a securing line to position the micro cargo container with respect to a surface in a first system state; directing a UAV having a tether capture device to the tether for engagement; in a transition state, contacting the tether with a leading edge of at least one main wing of the UAV; sliding the tether to the capture device attached to the main wing; engaging the tether with the tether capture device; and towing the micro cargo container with the UAV in a second system state. 2. The method of claim 1 further comprising rupturing a suspension link and a lower link freeing the tether and securing line. 3. The method of claim 1 wherein the step of suspending the micro cargo container comprises suspending the micro cargo container from a balloon. 4. The method of claim 1 wherein the step of suspending the micro cargo container comprises suspending the micro cargo container from suspension arm. 5. The method of claim 1 wherein the step of suspending the micro cargo container comprises suspending the micro cargo container from natural object. 6. The method of claim 3 wherein the tether remains attached to the balloon which is aerodynamically streamlined for tow. 7. The method of claim 3 wherein the balloon is punctured for flagging during tow. 8. The method of claim 1 wherein the step of contacting the tether is achieved by flying a nose of the UAV into an open loop in the tether for a symmetric flight configuration. 9. The method of claim 1 further comprising reeling the tether in to closely hold the micro-cargo near or in the UAV for more efficient flight.
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