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:
Jan. 20, 2015
Filed:
Oct. 27, 2010
Applicants:
Steve Bedoin, Toulouse, FR;
Cyril Bonnaud, Toulouse, FR;
Inventors:
Steve Bedoin, Toulouse, FR;
Cyril Bonnaud, Toulouse, FR;
Assignee:
Airbus Operations S.A.S., Toulouse, FR;
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01); B64C 7/02 (2006.01); B64C 23/06 (2006.01); B64D 29/02 (2006.01); F02C 7/20 (2006.01);
U.S. Cl.
CPC ...
B64C 7/02 (2013.01); B64C 23/06 (2013.01); B64D 29/02 (2013.01); F02C 7/20 (2013.01); Y02T 50/162 (2013.01); Y02T 50/671 (2013.01); F05D 2240/127 (2013.01);
Abstract
The invention relates to a method for manufacturing an engine pylon () to be mounted between an engine () and an aircraft wing (), said method comprising: mounting a pylon box () around a main structure (), the box having a substantially oblong shape along which an air boundary layer (C) is formed while in flight; mounting at least one vortex generator () onto the pylon box such that a thickness (e) of the boundary layer is changed; and previously determining the shape of the pylon on the basis of the changed thickness of the boundary layer and the position of the vortex generators.