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:
Oct. 01, 2024

Filed:

Jan. 10, 2022
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Levi Charles Hefner, Dallas, TX (US);

Kevin Fisher, Fort Worth, TX (US);

Manuel Adrian Gonzalez, Plano, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 39/02 (2023.01); B64D 1/12 (2006.01); B64D 27/40 (2024.01); F16B 2/06 (2006.01); B64U 101/60 (2023.01);
U.S. Cl.
CPC ...
B64C 29/0016 (2013.01); B64C 29/00 (2013.01); B64C 39/02 (2013.01); B64C 39/024 (2013.01); B64D 1/12 (2013.01); B64D 27/40 (2024.01); F16B 2/06 (2013.01); B64U 2101/60 (2023.01); B64U 2201/20 (2023.01);
Abstract

A tailsitter aircraft includes an airframe having first and second wings with first and second pylons extending therebetween, a thrust array attached to the airframe, payloads and payload saddle assemblies coupled to the pylons each configured to secure a respective payload. The thrust array includes propulsion assemblies configured to transition the airframe between a forward flight orientation for wing-borne lift and a VTOL orientation for thrust-borne lift. Each payload saddle assembly includes a latch assembly and a retainer configured to secure the respective payload against a respective pylon. A latch assembly is movable between various positions including an open position and a closed position and is configured to secure the respective payload in the closed position and release the respective payload in the open position. Each latch assembly is configured to move from the closed position to the open position to release the respective payload in the VTOL orientation.


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