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:
Jul. 28, 2020

Filed:

Feb. 25, 2019
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

Patrik Schmiedel, Buchdorf, DE;

Harald Leitner, Augsburg, DE;

Julian Kraus, Dillingen, DE;

Ludwig Dannemann, Augsburg, DE;

Uwe Kiesewetter, Rain am Lech, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/72 (2006.01); B64C 27/04 (2006.01); B64C 27/39 (2006.01); B64C 27/59 (2006.01); B64C 27/51 (2006.01); B64C 27/58 (2006.01);
U.S. Cl.
CPC ...
B64C 27/72 (2013.01); B64C 27/04 (2013.01); B64C 27/39 (2013.01); B64C 27/51 (2013.01); B64C 27/59 (2013.01); B64C 27/58 (2013.01); B64C 2027/7205 (2013.01);
Abstract

A rotor or propeller may have rotor blades and a passive pitch angle adjustment apparatus. The passive pitch angle adjustment apparatus may include levers, rods, and central rod. Levers may be connected to rotor blades and rotate them around a respective pitch axis. Rods may be connected to levers and mechanically link levers with each other via central point that is located outside rotor plane. Central rod may connect central point with base point that is located in a longitudinal direction of rotor axis. The passive pitch angle adjustment apparatus may enable a cyclic pitch adjustment of the rotor blades and block a collective pitch adjustment of the rotor blades.


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