The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 03, 2019

Filed:

Feb. 01, 2017
Applicant:

Aerovel Corporation, Bingen, WA (US);

Inventor:

Brian T. McGeer, Underwood, WA (US);

Assignee:

Aerovel Corporation, Bingen, WA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64F 1/04 (2006.01); B64C 39/02 (2006.01); B64C 29/02 (2006.01);
U.S. Cl.
CPC ...
B64F 1/04 (2013.01); B64C 39/024 (2013.01); B64C 29/02 (2013.01); B64C 2201/08 (2013.01); B64C 2201/182 (2013.01);
Abstract

Automated launch and retrieval of a 'tail-sitting' VTOL aircraft is accomplished by exploiting the natural stability of hover when restrained in tension by an upwind wing tip. For retrieval, a flexible rod is lifted into contact with the trailing edge of the upwind wing as the aircraft translates downwind overhead. Sliding between the rod and wing leads to interlocking of hooks at the rod end and wing tip, while the aircraft swings into a stable tethered hover downwind of the rod. The rod is then used to pull the aircraft upwind into a fixture for secure parking and servicing. After servicing, the aircraft lifts-off into tethered hover, and power margin for climb is assessed. If the aircraft is judged to have sufficient power safely to proceed, then the interlocking hooks are disengaged, leaving the aircraft to climb away in free flight.


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