Muzzle exit tester

Patent metadata

Field	Value
Publication number	US-9310284-B2
Application number	US-201414189777-A
Country	US
Kind code	B2
Filing date	Feb 25, 2014
Priority date	Feb 25, 2014
Publication date	Apr 12, 2016
Grant date	Apr 12, 2016

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.

First claim

What is claimed is:

1. A muzzle exit tester system, comprising:
a barrel having an input end and an exit end;
a shock plunger freely movable within the barrel;
a shock plate having a first side that faces the exit end of the barrel;
a support isolation structure that resiliently supports the shock plate, and receives a portion of the barrel that includes the exit end of the barrel; and
a pneumatic shock apparatus operatively coupled to the input end of the barrel, the pneumatic shock apparatus configured to retract the shock plunger in the barrel via a vacuum while producing a gas pressure charge, and subsequently release the gas pressure charge, such that the shock plunger accelerates to the exit end of the barrel and impacts the shock plate;
wherein the shock plate is dimensioned and shaped with selected geometries and cutouts to create resonances that when excited produce a desired shock response spectrum;
wherein 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 shock plunger.

2. The system of claim 1 , wherein the barrel comprises a cylindrical tube having a plurality of vent holes located around the portion of the barrel received in the isolation structure.

3. The system of claim 1 , wherein the shock plunger has a cylindrical dumbbell shape.

4. The system of claim 1 , wherein the shock plate includes a mounting structure for attaching a unit under test on a second side of the shock plate opposite from the first side.

5. The system of claim 1 , wherein the shock plate includes a strike plate on the first side that faces the exit end of the barrel.

6. The system of claim 1 , wherein the support isolation structure comprises:
a plurality of legs;
a roof structure supported by the legs and having an opening for exhaust and visualization; and
a set of die springs coupled to each of the legs and the shock plate;
wherein the shock plate is located between the legs of the support isolation structure.

7. The system of claim 1 , wherein the pneumatic shock apparatus comprises:
a pressure regulator;
a charge valve in communication with the pressure regulator;
a safety valve in communication with the charge valve;
a pressure reservoir in communication with the safety valve; and
a release valve in communication with the pressure reservoir and the input end of the barrel.

8. The system of claim 7 , wherein the pneumatic shock apparatus further comprises a vacuum assembly comprising:
a vacuum pump;
a vacuum reservoir in communication with the vacuum pump; and
a vacuum valve in communication with the vacuum reservoir and the input end of the barrel;
wherein the vacuum assembly provides suction for retracting the shock plunger toward the input end of the barrel.

9. The system of claim 7 , wherein the pneumatic shock apparatus further comprises a pressure relief device and a pressure indicator.

10. The system of claim 8 , wherein the pneumatic shock apparatus further comprises a programmable logic controller operatively coupled to the vacuum valve, the charge valve, the safety valve, and the release valve.

11. The system of claim 10 , wherein the vacuum valve, the charge valve, the safety valve, and the release valve each comprises a solenoid valve.

12. A muzzle exit testing method, comprising:
providing a muzzle exit tester comprising:
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;
wherein the shock plate is dimensioned and shaped with selected geometries and cutouts to create resonances that when excited produce a desired shock response spectrum;

retracting the shock plunger within the barrel via a vacuum;
producing a gas pressure charge;
releasing the gas pressure charge into the input end of the barrel to cause the shock plunger to accelerate through the barrel to the exit end and impact the first side of the shock plate; and
measuring a shock response of the shock plate after impact of the shock plunger with the first side of the shock plate.

13. The method of claim 12 , wherein the shock plate resonates at frequencies and amplitudes corresponding to a shock condition of a gun muzzle exit when impacted by the shock plunger.

14. The method of claim 12 , further comprising:
mounting a unit under test (UUT) on a second side of the shock plate opposite from the first side prior to retracting the shock plunger.

15. The method of claim 14 , wherein the UUT comprises an accelerometer, a gyroscope, an inertial measurement unit, or a global positioning system sensor.

16. The method of claim 12 , wherein the shock response of the shock plate is measured with a laser Doppler vibrometer.

17. The method of claim 12 , wherein the muzzle exit tester is automated and operated via a programmable logic controller that controls solenoid pressure valves in a pneumatic shock apparatus.

18. The method of claim 17 , wherein the solenoid pressure valves comprise a vacuum valve, a charge valve, a release valve, and a safety valve.

19. The method of claim 18 , wherein the programmable logic controller is configured to:
control timing of the vacuum valve to retract the shock plunger within the barrel and provide post-shock pressurization relief;
control timing of the charge valve to produce the gas pressure charge;
control timing of the release valve to release the gas pressure charge into the input end of the barrel; and
actuate the safety valve to release all gas pressure on a power outage or abort command.

20. The method of claim 12 , wherein operational data is collected and recorded before, during, and after the impact of the shock plunger with the first side of the shock plate.

Assignees

• Honeywell Int Inc

Inventors

• Graham Jason
• Grossman Owen D

Classifications

• F41B11/681

  Pumping or compressor arrangements therefor · CPC title

• F41B11/87

  for industrial purposes, e.g. for surface treatment · CPC title

• F41B11/722 Primary

  for controlling gas pressure for loading or feeding only · CPC title

• G01M7/08

  Shock-testing · CPC title

• F41B11/723

  for controlling gas pressure for firing the projectile only · CPC title