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:
Sep. 25, 2018

Filed:

Mar. 02, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Gregg W. Podnar, Chicago, IL (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B01D 19/00 (2006.01); B64C 1/06 (2006.01); B64C 3/00 (2006.01); B64D 37/02 (2006.01); B64F 5/00 (2017.01); B05C 5/02 (2006.01); B05C 17/005 (2006.01);
U.S. Cl.
CPC ...
B01D 19/0052 (2013.01); B01D 19/0026 (2013.01); B05C 5/02 (2013.01); B05C 5/0225 (2013.01); B05C 17/005 (2013.01); B05C 17/00579 (2013.01); B64C 1/068 (2013.01); B64C 3/00 (2013.01); B64D 37/02 (2013.01); B64F 5/0009 (2013.01);
Abstract

Systems for removing gas from a sealant and transferring gas-less sealant to an applicator are provided. The system may comprise: a rotatable chamber including: a first opening for receiving sealant; a hollow conduit arranged such that when gas accumulates in the center of the rotatable chamber when the rotatable chamber is rotating, the gas is ventable from the rotatable chamber; a second opening for receiving gas-less sealant from the rotatable chamber after the gas is vented from the hollow conduit; and a motor operatively configured to rotate the rotatable chamber; and a gas-less sealant applicator in fluid communication with the second opening of the rotatable chamber such that gas-less sealant released by the second opening is flowable into the applicator. The system may also include a robot arm including an end effector with a sealant dispensing nozzle. A method for applying sealant to an aircraft structure is also provided.


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