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:
Aug. 16, 2016

Filed:

Jun. 12, 2014
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Robert Henry Willie, Bothell, WA (US);

David F. Cerra, Woodinville, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F15D 1/00 (2006.01); B64D 29/00 (2006.01); B64D 37/00 (2006.01); B64C 1/14 (2006.01); B64D 37/26 (2006.01); F01D 25/32 (2006.01);
U.S. Cl.
CPC ...
F15D 1/001 (2013.01); B64C 1/1453 (2013.01); B64D 29/00 (2013.01); B64D 37/005 (2013.01); B64D 37/26 (2013.01); F01D 25/32 (2013.01); F15D 1/008 (2013.01); Y10T 137/0391 (2015.04); Y10T 137/2082 (2015.04);
Abstract

A method and apparatus for draining fluid from a structure on an aircraft. The apparatus comprises a drainage tube, a housing, a number of inlet holes in the housing, and a number of outlet holes in the housing. The drainage tube has first end that connects to a structure on an aircraft and a second end opposite the first end. The housing connects to the structure. The drainage tube is located within the housing. Air flows into the housing during flight of the aircraft through the number of inlet holes in the housing. The air flows out of the housing during flight of the aircraft through the number of outlet holes. The air flowing into the housing through the number of inlet holes and out the housing through the number of outlet holes directs fluid out of the drainage tube and away from the structure during flight of the aircraft.


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