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:
Apr. 24, 2018

Filed:

Mar. 29, 2016
Applicant:

B/e Aerospace, Inc., Wellington, FL (US);

Inventors:

Thao Hoang, Rockford, IL (US);

Bradley J. Buniak, Schaumburg, IL (US);

Stephen M. Niznik, Rockford, IL (US);

William Pedersen, Rockford, IL (US);

Mark A. Pondelick, Rockton, IL (US);

Assignee:

B/E Aerospace, Inc., Winston Salem, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
E03D 11/10 (2006.01); E03D 9/00 (2006.01); B64D 11/02 (2006.01); E03D 11/13 (2006.01); E03D 5/10 (2006.01); E03D 5/012 (2006.01); F16K 3/04 (2006.01); F16K 31/04 (2006.01); F16K 31/46 (2006.01); E03D 11/16 (2006.01); E03F 1/00 (2006.01);
U.S. Cl.
CPC ...
E03D 9/00 (2013.01); B64D 11/02 (2013.01); E03D 5/012 (2013.01); E03D 5/10 (2013.01); E03D 11/13 (2013.01); E03D 11/135 (2013.01); E03D 11/16 (2013.01); E03F 1/006 (2013.01); F16K 3/04 (2013.01); F16K 31/047 (2013.01); F16K 31/465 (2013.01);
Abstract

A toilet system configured for operation on-board an aircraft includes, according to an implementation, a toilet bowl, a left side support bracket supporting the toilet bowl, a right side support bracket supporting the toilet bowl, a control box including a first set of pins, and a harness connector configured to electrically couple the toilet to the aircraft. The harness connector includes a set of pins, where the first set of pins of the control box are configured to be connected to the set of pins included in the harness connector, and the control box is configured to determine a platform of the aircraft based on the presence or absence of a pin in the set of pins included in the harness connector.


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