Aurora win patent for UAV skyhook.
Aurora Flight Sciences, Manassas, Va., has been assigned a patent (8,038,090) developed by Richard Wilson, Beverly, Mass., and Adam Woodworth, Melrose, Mass., for a “system and method for the retrieval of a smaller unmanned aerial vehicle by a larger unmanned aerial vehicle.”
The abstract of the patent published by the U.S. Patent and Trademark Office states: “A system and method are provided for using a first aircraft to retrieve a second aircraft. The first aircraft is typically larger than the second aircraft. A minimum airspeed of the first aircraft is typically greater than a maximum airspeed of the second aircraft. The first aircraft flies in a substantially circular pattern and extends a tow line, such that the tow line forms a substantially helical shape behind and below the first aircraft. Due to the helical shape, there is at least one point along the extended tow line at which the speed of the tow line is substantially equal to the speed of the second aircraft. The second aircraft can readily latch onto the tow line at that point, thereby minimizing potential damage otherwise caused by differential airspeeds.”
The patent application was filed on March 19, 2009 (12/407,231). The full-text of the patent can be found at http://patft.uspto.gov/netacgi/nph-Parser?Sect1=PTO2&Sect2=HITOFF&p=1&u=%2Fnetahtml%2FPTO%2Fsearch-bool.html&r=1&f=G&l=50&co1=AND&d=PTXT&s1=8,038,090&OS=8,038,090&RS=8,038,090
What is claimed is:
1. A method of using a first aircraft to retrieve at least one second aircraft onto the first aircraft, comprising the steps of: flying the first aircraft along a first path; extending a tow line from the first aircraft such that the flying of the first aircraft along the first path causes a helical shape to be formed by the extended tow line behind and below the first aircraft; determining a point on the extended tow line at which a tow line speed is substantially equal to a second aircraft speed for each of the at least one second aircraft; adjusting an altitude of the first aircraft or the at least one second aircraft such that an altitude of the point on the extended tow line at which the tow line speed is substantially equal to the at least one second aircraft speed is substantially equal to an altitude of the at least one second aircraft for each of the at least one second aircraft; and securing each of the at least one second aircraft to the extended tow line.
2. The method of claim 1, further comprising the step of retracting the extended tow line and the secured at least one second aircraft into the first aircraft.
3. The method of claim 1, wherein a ratio of a length of the first aircraft to a length of the at least one second aircraft is greater than or equal to 4:1.
4. The method of claim 1, wherein a minimum first aircraft speed is greater than a maximum second aircraft speed.
5. The method of claim 1, wherein the first path is substantially circular.
6. The method of claim 1, wherein the tow line comprises a catch basket positioned at or near a bottom portion of the extended tow line, and the method further comprising the steps of: after securing the at least one second aircraft to the extended tow line, flying the first aircraft along a substantially straight path, such that the extended tow line is configured to form a substantially straight line behind and below the first aircraft; causing the at least one second aircraft to slide down the extended tow line into the catch basket; and retracting the extended tow line, the catch basket, and the secured at least one second aircraft into the first aircraft.
