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:
Jun. 28, 2011

Filed:

Feb. 21, 2008
Applicants:

Jorge Pablo Verde Preckler, Madrid, ES;

José Miguel Vizarro Toribio, Madrid, ES;

Raúl Carlos Llamas Sandin, Madrid, ES;

Stephane Viala, Mamers, FR;

Inventors:
Assignee:

Airbus Espana, S.L., Madrid, ES;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 15/12 (2006.01);
U.S. Cl.
CPC ...
Abstract

The invention relates to a configuration of engines () for aircraft located in the rear part of the fuselage () of said aircraft, the engines () being attached in a fixed manner by pylons () to the structure of the aircraft, said structure comprising a torsion box () which traverses the fuselage () and is used to attach the pylons (), the fuselage () comprising an opening () allowing the passage of the suspension pylons () for the engines (), said configuration further comprising a pivoting area (), an actuator () and a fitting () through which the actuator () is attached to the suspension pylons () and to the torsion box () of the aircraft, such that the assembly formed by the actuator () and the fitting () allow balancing the pylon () and engine () assembly of the aircraft through the pivoting area (), thus achieving controllable and optimal thrust vectoring of the aircraft for each flight phase.


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