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:
Dec. 31, 2019

Filed:

Jun. 16, 2016
Applicant:

Simmonds Precision Products, Inc., Vergennes, VT (US);

Inventors:

Lubomir A. Ribarov, West Hartford, CT (US);

Richard J. Carpenter, Gales Ferry, CT (US);

Russell P. Rourke, Jr., East Granby, CT (US);

Charles J. Russo, Manchester, CT (US);

William Luker, Glastonbury, CT (US);

Assignee:

SIMMONDS PRECISION PRODUCTS, INC., Vergennes, VT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 17/10 (2006.01); B64D 37/04 (2006.01);
U.S. Cl.
CPC ...
B64C 17/10 (2013.01); B64D 37/04 (2013.01);
Abstract

A method of aircraft fuel distribution includes selecting a longitudinal center of gravity and predicting a rate of change of the center of gravity during flight. Fuel is located in a tail fin tank of a vertical tail fin of the aircraft, and is transferred from the tail fin tank forward at a predetermined transfer rate to counteract the predicted rate of change thereby maintaining the selected center of gravity. An aircraft fuel distribution system includes a center main fuel tank, a tail fin tank and a tail fin fuel pump to pump fuel between the tail fin tank and the center main fuel tank. An electronic controller operates the tail fin fuel pump such that fuel is flowed between the tail fin tank and the center main fuel tank at a predetermined transfer rate to maintain automatically an optimal position of a longitudinal center of gravity of the aircraft.


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