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. 08, 2018

Filed:

Feb. 26, 2016
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

Christian Wehle, Augsburg, DE;

Justus Steger, Neustadt A. D. Aisch, DE;

Marc Nothen, Rain am Lech, DE;

Stefan Probst, Buchdorf, DE;

Antonia Horstmann, Dillingen, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/82 (2006.01); B64C 27/20 (2006.01); B64F 5/10 (2017.01);
U.S. Cl.
CPC ...
B64C 27/82 (2013.01); B64C 27/20 (2013.01); B64F 5/10 (2017.01); B64C 2027/8272 (2013.01);
Abstract

A tail assembly for a rotorcraft. The tail assembly is manufactured to include at least one transition structure provided in the tail assembly. The transition structure is longitudinally arranged between a longitudinal median boom portion and a tail fin. A power transmission shaft of the rotorcraft extends at least partly externally above a longitudinal median boom portion of the tail assembly. The transition structure includes at an entering region a cut-out elevation step, where is made a passing through opening for the power transmission shaft.


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