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:
May. 10, 2022

Filed:

Oct. 03, 2016
Applicant:

Aeronext Inc., Tokyo, JP;

Inventor:

Youichi Suzuki, Fuefuki, JP;

Assignee:

AERONEXT INC., Tokyo, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/52 (2006.01); B64C 27/20 (2006.01); B64C 27/54 (2006.01); B64C 29/00 (2006.01); B64D 9/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/52 (2013.01); B64C 27/20 (2013.01); B64C 27/54 (2013.01); B64C 29/0033 (2013.01); B64D 9/00 (2013.01); B64C 2201/027 (2013.01); B64C 2201/128 (2013.01); B64C 2201/141 (2013.01); B64C 2201/18 (2013.01);
Abstract

A delivery rotary-wing aircraft has a plurality of rotary wings, a central portion to which a plurality of arms for supporting the rotary wings are connected, a first mounting portion for loading a package, a second mounting portion which is located on the opposite side to the first mounting portion as viewed from the central portion, a first supporting member for coupling the first mounting portion with the central portion, and a connection portion between the central portion and the first supporting member. The center point of lift occurring in the rotary-wing aircraft with the rotation of the plurality of rotary wings and the center point of gravity of the rotary-wing aircraft coincide with the center point of the connection portion. The first supporting member is equipped with an adjustment mechanism for vertically downwardly extending the length of the first supporting member.


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