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:
Oct. 14, 2014

Filed:

Apr. 15, 2009
Applicants:

Ralf-henning Stolte, Hamburg, DE;

Uwe Wollrab, Soltau, DE;

Inventors:

Ralf-Henning Stolte, Hamburg, DE;

Uwe Wollrab, Soltau, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 15/02 (2006.01); B64D 15/04 (2006.01); B64C 21/04 (2006.01); B64D 13/06 (2006.01); B64D 41/00 (2006.01);
U.S. Cl.
CPC ...
B64C 21/04 (2013.01); Y02T 50/166 (2013.01); B64D 2013/0614 (2013.01); B64D 15/04 (2013.01); Y02T 50/56 (2013.01); B64D 2041/005 (2013.01); B64D 2013/0622 (2013.01); Y02T 90/36 (2013.01); B64D 2013/0607 (2013.01);
Abstract

The invention pertains to a de-icing system for an aircraft with at least one heat source and at least one air delivery means for delivering air into regions of the aircraft to be de-iced. In comparison with the prior art, the invention is characterized in that the air delivery means is connected to an air-conditioning system of the aircraft for discharging air from the cabin of the aircraft via an air heating device, wherein the air heating device is connected to at least one heat source in order to heat the air from the cabin of the aircraft. The de-icing system according to the invention is able to realize a wing de-icing that not only fulfills an anti-icing function, but also a de-icing function on the ground without additional expenditure of energy. The function of the de-icing system according to the invention could also be advantageously supplemented by utilizing the cabin waste air for increasing the flow energy on the upper side of the wing in order to delay a change-over or separation of the boundary layer and to generally increase the lift or lower the resistance.


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