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. 12, 2016

Filed:

Feb. 25, 2014
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventors:

Jason Graham, White Bear Lake, MN (US);

Owen D. Grossman, Golden Valley, MN (US);

Assignee:

Honeywell International Inc., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01M 7/00 (2006.01); G01N 3/307 (2006.01); F41B 11/722 (2013.01); F42B 35/00 (2006.01); G01M 7/08 (2006.01); F41B 11/681 (2013.01); F41B 11/723 (2013.01); F41B 11/87 (2013.01);
U.S. Cl.
CPC ...
G01N 3/307 (2013.01); F41B 11/681 (2013.01); F41B 11/722 (2013.01); F41B 11/723 (2013.01); F41B 11/87 (2013.01); F42B 35/00 (2013.01); G01M 7/08 (2013.01);
Abstract

A muzzle exit tester system comprises a barrel having an input end and an exit end, a shock plunger freely movable within the barrel, and a shock plate having a first side that faces the exit end of the barrel. A support isolation structure resiliently supports the shock plate, and receives a portion of the barrel that includes the exit end of the barrel. A pneumatic shock apparatus is operatively coupled to the input end of the barrel. The pneumatic shock apparatus is configured to retract the plunger in the barrel via a vacuum while producing a gas pressure charge, and subsequently release the gas pressure charge, such that the plunger accelerates to the exit end of the barrel and impacts the shock plate. The shock plate is configured to resonate at frequencies and amplitudes corresponding to a shock condition of a gun muzzle exit when impacted by the plunger.


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