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:
Mar. 19, 2024

Filed:

May. 22, 2020
Applicant:

The Texas A&m University System, College Station, TX (US);

Inventors:

Moble Benedict, College Station, TX (US);

Hunter J. Denton, Hawkins, TX (US);

Hao Kang, Abingdon, MD (US);

Vikram Hrishikeshavan, Arlington, VA (US);

Assignee:

The Texas A&M University System, College Station, TX (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64U 70/70 (2023.01); B64C 27/10 (2023.01); B64C 27/50 (2006.01); B64C 39/02 (2023.01); B64U 10/10 (2023.01); F42B 10/14 (2006.01); B64U 80/00 (2023.01); B64U 101/30 (2023.01); F41G 7/36 (2006.01);
U.S. Cl.
CPC ...
B64U 70/70 (2023.01); B64C 27/10 (2013.01); B64C 27/50 (2013.01); B64C 39/024 (2013.01); B64C 39/028 (2013.01); F42B 10/14 (2013.01); B64U 10/10 (2023.01); B64U 80/00 (2023.01); B64U 2101/30 (2023.01); F41G 7/36 (2013.01);
Abstract

A projectile-launched aircraft system includes a projectile launcher including a triggering mechanism, a rotary-wing, hover-capable aircraft including a rotor assembly that includes at least one rotor blade, wherein the rotor blade includes a stowed configuration and a deployed configuration that is circumferentially spaced from the stowed configuration about a pivot axis, wherein, upon actuation of the triggering mechanism, the projectile launcher is configured to launch the aircraft along a flightpath.


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