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:
Jan. 17, 2012

Filed:

Feb. 17, 2009
Applicants:

Francisco DE Paula Burgos Gallego, Madrid, ES;

Manuel Maroto DE Hoyos, Madrid, ES;

Inventors:
Assignee:

Airbus España S.L., Madrid, ES;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 9/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A lifting or stabilising component () for an aircraft comprising in the area of its trailing edge a rotary control element () rotating around an axis () with at least one slot () between the tip () of the component () and the control element (), the edges of which are configured such that the distance therebetween, that is, the dimension of the slot (), is constant for different angles of deflection of the control element (), being located between them a seal () that assure the aerodynamic continuity of the component () when the control element () is at rest. In a preferred embodiment, the component () is a horizontal tail stabilizer and the control element () is a rudder.


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