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:
Apr. 17, 2018

Filed:

Oct. 21, 2011
Applicants:

Robert Gilchrist, Iii, Cook, WA (US);

John Stafford, Lyle, WA (US);

Brian D. Dennis, White Salmon, WA (US);

Allen Smith, Hood River, OR (US);

Jaime Mack, White Salmon, WA (US);

Steven M. Sliwa, White Salmon, WA (US);

Bradley Schrick, Bingen, WA (US);

Robert Hughes, Springfield, VA (US);

Inventors:

Robert Gilchrist, III, Cook, WA (US);

John Stafford, Lyle, WA (US);

Brian D. Dennis, White Salmon, WA (US);

Allen Smith, Hood River, OR (US);

Jaime Mack, White Salmon, WA (US);

Steven M. Sliwa, White Salmon, WA (US);

Bradley Schrick, Bingen, WA (US);

Robert Hughes, Springfield, VA (US);

Assignee:

Insitu, Inc., Bingen, WA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64F 1/02 (2006.01);
U.S. Cl.
CPC ...
B64F 1/02 (2013.01); B64C 2201/182 (2013.01);
Abstract

Systems and methods for recovering unmanned aircraft and controlling post-recovery motion of the aircraft are disclosed herein. An aircraft recovery system for handling an unmanned aircraft in accordance with one embodiment of the disclosure includes a base portion and an elongated aircraft capture member having a first end movably coupled to the base portion and a second, free end opposite the first end. The aircraft capture member includes a first portion and a second portion at a distal end of the first portion and positioned to intercept an unmanned aircraft in flight. The first and/or second portions are generally flexible. The system further includes an energy capture and dissipation assembly operably coupled to the aircraft capture member and positioned to receive at least a portion of the landing forces from the aircraft.


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