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. 24, 2018

Filed:

Jan. 19, 2015
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

Rupert Pfaller, Riemerling, DE;

Martin Schulz, Hoehenkirchen, DE;

Tobias Bodemann, Wittmund, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/33 (2006.01); B64C 27/32 (2006.01);
U.S. Cl.
CPC ...
B64C 27/33 (2013.01); B64C 27/32 (2013.01);
Abstract

A flexbeam unit for a multi-blade rotor of a rotary wing aircraft, said flexbeam unit defining a predetermined number of torsion elements that are connectable with associated rotor blades, at least one torsion element comprising a flexbeam element having an associated longitudinal direction and comprising inner layers of a first fiber reinforced material that are embedded between outer layers of a second fiber reinforced material, said outer layers being composed of main plies comprising unidirectional fibers and said inner layers defining a cross section profile center in said associated longitudinal direction, said cross section profile center being composed of interconnected bias plies comprising fibers that are oriented transversely relative to said unidirectional fibers.


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