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. 25, 2015

Filed:

Feb. 12, 2014
Applicants:

Benjamin Abruzzo, Newark, NJ (US);

Thomas Recchia, Succasunna, NJ (US);

Michael Pica, Levittown, PA (US);

Mark Mellini, Denville, NJ (US);

Eric Marshall, Wyckoff, NJ (US);

Jason Devenezia, Newton, NJ (US);

Sean Schumer, Lincoln Park, NJ (US);

John Thomas, Morris Plains, NJ (US);

Inventors:

Benjamin Abruzzo, Newark, NJ (US);

Thomas Recchia, Succasunna, NJ (US);

Michael Pica, Levittown, PA (US);

Mark Mellini, Denville, NJ (US);

Eric Marshall, Wyckoff, NJ (US);

Jason DeVenezia, Newton, NJ (US);

Sean Schumer, Lincoln Park, NJ (US);

John Thomas, Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F42B 15/01 (2006.01); F42B 30/00 (2006.01); F42C 19/00 (2006.01);
U.S. Cl.
CPC ...
F42B 30/006 (2013.01); F42C 19/00 (2013.01);
Abstract

A new fuze that reduces projectile miss-distance to a target, by correcting for discrepancies in anticipated round velocities through its flight. As a result, the fuze-equipped projectile is nominally aimed at a target and maintains improved accuracy relative to a conventional round. The fuze adjusts for the discrepancies in velocity by using an internal electric motor to mechanically actuate a drag-altering surface on the fuze body. In order to adjust for errors in the anticipated velocity, the fuze compares its preprogrammed velocity to its actual velocity at a given point in time during flight. An anticipated velocity table versus time in flight is constantly referenced so that appropriate adjustments in velocity can be made.


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