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:
Sep. 10, 2019

Filed:

Sep. 28, 2016
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

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

Christian Wehle, Augsburg, DE;

Henry Gunn, Augsburg, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); F16H 57/025 (2012.01); B64C 27/14 (2006.01); B64D 35/08 (2006.01); F16H 57/028 (2012.01); B64C 27/12 (2006.01);
U.S. Cl.
CPC ...
F16H 57/025 (2013.01); B64C 27/12 (2013.01); B64C 27/14 (2013.01); B64D 35/08 (2013.01); F16H 57/028 (2013.01); B64C 2027/002 (2013.01);
Abstract

A mounting arrangement for mounting at least a gear box of a rotorcraft to a fuselage of a rotorcraft, the mounting arrangement comprising a gear box of a rotorcraft and at least two support plates that are rigidly attached to at least approximately opposing sides of the gear box, each one of the at least two support plates comprising at least two attachment means that are adapted to allow attachment of the at least two support plates to a fuselage of a rotorcraft by means of associated struts in order to enable transfer of induced loads occurring in operation, which are directed into a predetermined load direction, via the associated struts.


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