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:
Aug. 08, 2023

Filed:

Apr. 15, 2015
Applicant:

Northrop Grumman Systems Corporation, Falls Church, VA (US);

Inventors:

Kyle Rahrig, El Segundo, CA (US);

Geoffrey Sommer, El Segundo, CA (US);

Barnaby S. Wainfan, Long Beach, CA (US);

Assignee:

NORTHROP GRUMMAN SYSTEMS CORPORATION, Falls Church, VA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 39/06 (2006.01); B64C 11/00 (2006.01); B64D 29/02 (2006.01); F02K 1/34 (2006.01); B64C 15/14 (2006.01); B64D 35/08 (2006.01);
U.S. Cl.
CPC ...
B64C 39/066 (2013.01); B64C 11/001 (2013.01); B64C 15/14 (2013.01); B64D 29/02 (2013.01); B64D 33/06 (2013.01); B64D 35/08 (2013.01); Y02T 50/40 (2013.01); Y02T 50/60 (2013.01);
Abstract

An extremely quiet short take-off and landing (STOL) aircraft includes: two wings, wherein each wing comprises an engine system; a fuselage structurally connected to each wing; and a ducted fan thruster positioned on the fuselage in an orientation that is rotated relative to the typical orientation on a helicopter. An extremely quiet STOL aircraft includes: two wings, wherein each wing comprises an engine system; a fuselage structurally connected to each wing; channel shrouds surrounding at least one of the engine systems; and a ducted fan thruster positioned on the fuselage. An extremely quiet STOL aircraft includes: two wings, wherein each wing comprises an engine system, the engine system comprising two engine dual packs; a fuselage structurally connected to each wing; and a ducted fan thruster positioned on the fuselage.


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