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:
Jun. 18, 2019

Filed:

Dec. 22, 2016
Applicant:

Lockheed Martin Corporation, Bethesda, MD (US);

Inventors:

James C. Copp, Arlington, TX (US);

Steven J. Ellzey, Grand Prairie, TX (US);

Assignee:

LOCKHEED MARTIN CORPORATION, Bethesda, MD (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 5/12 (2006.01); B64C 39/02 (2006.01); B64C 3/56 (2006.01); B64C 5/02 (2006.01);
U.S. Cl.
CPC ...
B64C 5/12 (2013.01); B64C 3/56 (2013.01); B64C 5/02 (2013.01); B64C 39/024 (2013.01); B64C 2201/021 (2013.01); B64C 2201/102 (2013.01); B64C 2201/20 (2013.01);
Abstract

An aircraft is provided comprising: a fuselage, a first tail fin rotatably mounted to a first lateral side and a second tail fin rotatably mounted to the second lateral side. A wing body is rotatably mounted to the underside of the fuselage. A pair of independent tail fin latch and release devices are provided to independently latch the first tail fin and the second tail fin when the wing body having a first angle is in a stowed position with respect to the fuselage, to independently unlatch the first tail fin in response to a second angle of the wing body with respect to the fuselage, and to independently unlatch the second tail fin in response to a third angle of the wing body with respect to the fuselage. The first angle, second angle and third angle are different angles with respect to the longitudinal axis of the fuselage.


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