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:
Dec. 22, 2020

Filed:

Sep. 14, 2017
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventor:

Moritz Buesing, Augsburg, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/59 (2006.01); B64C 27/605 (2006.01); B64C 27/00 (2006.01); B64C 11/32 (2006.01); B64C 27/32 (2006.01); B64C 27/72 (2006.01);
U.S. Cl.
CPC ...
B64C 27/59 (2013.01); B64C 11/32 (2013.01); B64C 27/008 (2013.01); B64C 27/32 (2013.01); B64C 27/605 (2013.01); B64C 2027/7216 (2013.01);
Abstract

A multi-blade rotor of a rotary wing aircraft, the multi-blade rotor comprising at least one rotor blade that defines a pitch axis and that is provided with an associated pitch-control lever that is operatively coupled to a pitch link rod, the pitch link rod defining a longitudinal axis, wherein the associated pitch-control lever comprises an accommodation that is located on the longitudinal axis of the pitch link rod at a predetermined distance from the pitch axis of the at least one rotor blade, the pitch link rod being operatively coupled to the associated pitch-control lever at the accommodation of the associated pitch-control lever, wherein the predetermined distance is adjustable in order to enable adjustment of track and balance of the multi-blade rotor.


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