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.
Patent No.:
Date of Patent:
May. 03, 2016
Filed:
Sep. 03, 2013
Applicant:
Airbus Operations (Sas), Toulouse, FR;
Inventors:
Wolfgang Brochard, Toulouse, FR;
Romain Terral, Toulouse, FR;
Assignee:
Airbus Operations (SAS), Toulouse, FR;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01); F01D 25/24 (2006.01); B64D 27/20 (2006.01); B64D 27/26 (2006.01); B64D 29/06 (2006.01);
U.S. Cl.
CPC ...
F01D 25/24 (2013.01); B64D 27/20 (2013.01); B64D 27/26 (2013.01); B64D 29/06 (2013.01); Y02T 50/44 (2013.01);
Abstract
A propulsion unit for an aircraft, comprising one turbine engine and a mounting device for a turbine engine designed to be added laterally on an aircraft structure and comprising a rigid mounting structure. The rigid mounting structure supports at least one arch which is concave towards the longitudinal axis of the propulsion unit and which has a distal end at an angular distance of between 45 and 120 degrees from a vertical plane passing through the axis, on the other side of the structure, and supporting a distal connecting element connecting the turbine engine to the arch.