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. 12, 2024

Filed:

Aug. 16, 2021
Applicant:

Zsm Holdings Llc, Dover, DE (US);

Inventors:

Scott David Rewerts, Summerfield, NC (US);

Jason C. Bell, Boulder, CO (US);

Mark Emil Lundstrom, Boulder, CO (US);

Assignee:

ZSM Holdings LLC, Dover, DE (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 9/00 (2006.01); B64C 1/06 (2006.01); B64C 1/14 (2006.01); B64C 1/20 (2006.01); B64C 1/22 (2006.01); B64C 3/32 (2006.01); B64C 3/34 (2006.01); B64C 17/08 (2006.01); B64D 37/04 (2006.01); B64F 1/32 (2006.01); F03D 13/40 (2016.01);
U.S. Cl.
CPC ...
B64D 9/003 (2013.01); B64C 1/0683 (2020.01); B64C 1/1415 (2013.01); B64C 1/20 (2013.01); B64C 1/22 (2013.01); B64C 3/32 (2013.01); B64C 3/34 (2013.01); B64C 17/08 (2013.01); B64D 9/00 (2013.01); B64D 37/04 (2013.01); B64F 1/32 (2013.01); F03D 13/40 (2016.05); B64D 2009/006 (2013.01); F05B 2260/02 (2013.01);
Abstract

A fixed-wing cargo aircraft having a kinked fuselage to extend the useable length of a continuous interior cargo bay while still meeting a tailstrike requirement is disclosed. The fuselage defines a continuous interior cargo bay along a majority of its length and a pitch axis about which the cargo aircraft rotates during takeoff while still on the ground. The fuselage includes a forward portion defining longitudinal-lateral plane of the cargo aircraft an aft portion extending aft from the pitch axis to the aft end and containing an aft region of the continuous interior cargo bay that extends along a majority of a length of the aft portion. The aft portion has a centerline extending above the forward upper surface of the aircraft.


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