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:
Nov. 30, 2021

Filed:

Mar. 22, 2018
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

Ching-Yu Hui, Bristol, GB;

Alan Mann, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 21/08 (2006.01); B64C 21/06 (2006.01); B64D 15/12 (2006.01);
U.S. Cl.
CPC ...
B64C 21/08 (2013.01); B64C 21/06 (2013.01); B64D 15/12 (2013.01); B64C 2230/06 (2013.01); B64C 2230/20 (2013.01); B64C 2230/22 (2013.01);
Abstract

An aerodynamic body for use on an aircraft including at least a first perforated surface portion () and an ice-protection system (). The first perforated surface portion () has perforations. The ice-protection system () includes an actuatable element () and the actuatable element () is movable or deformable between a first position and a second position. In the first position, the actuatable element () is thermally coupled to the first perforated surface portion () and configured to prevent an inflow or outflow between a boundary layer of an outer aerodynamic airflow and the aerodynamic body through at least one of the perforations. In the second position, the actuatable element () is distanced from the first perforated surface portion () and configured to allow an inflow from a boundary layer of an outer aerodynamic airflow through at least one of the perforations into the aerodynamic body.


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