logo

For the Inventor, By the Inventor

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.

Patent No.:

US 12325540 B1

PDFFull Text
Date of Patent:
Jun. 10, 2025

Filed:

Dec. 06, 2023

Aircraft with multifunctional structure

Applicant:

Pipistrel D.o.o., Ajdovscina, SI;

Inventors:

Matej Andrejasic, Postojna, SI;

David Erzen, Ljubljana, SI;

Rok Lapuh, Ljubljana, SI;

Blaz Mocan, Ljubljana, SI;

Andres Znidar, Vrhnika, SI;

Tine Tomazic, Vrhnika, SI;

Jernej Drofelnik, Ljubljana, SI;

Gregor Cretnik, Ljubljana, SI;

Assignee:

PIPISTREL D.O.O., Ajdovscina, SI;

Attorney:

SLATER MATSIL, LLP

Primary Examiner:

Timothy D Collins

Assistant Examiner:

Justin Michael Heston

Int. Cl.
CPC ...
B64U 10/20 (2023.01); B64C 25/58 (2006.01); B64U 30/20 (2023.01); B64U 101/60 (2023.01);
U.S. Cl.
CPC ...
B64U 10/20 (2023.01); B64C 25/58 (2013.01); B64U 30/20 (2023.01); B64U 2101/60 (2023.01);
Abstract

An embodiment aircraft boom includes a boom member, a vertical stabilizer, a rear landing gear, and a front landing gear. The boom member may extend in a first direction and have a front internal structural member disposed therein, where a portion of the front internal structural member is a first attachment point for a first wing. The vertical stabilizer may extend from the boom member, where the vertical stabilizer has a rear internal structural member disposed therein and extends from the boom member and through an interior of the vertical stabilizer, and where a portion of the rear internal structural member is a second attachment point for a second wing. The rear landing gear may be coupled to the rear internal structural member. The front landing gear may be coupled to the front internal structural member of the boom member.

Find Patent Forward Citations

Andrejasic, Matej. (2025). Aircraft with multifunctional structure (U.S. Patent No. 12325540). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12325540

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

Loading…