US3034335A - Primer testing device - Google Patents

Primer testing device Download PDF

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Publication number
US3034335A
US3034335A US784826A US78482659A US3034335A US 3034335 A US3034335 A US 3034335A US 784826 A US784826 A US 784826A US 78482659 A US78482659 A US 78482659A US 3034335 A US3034335 A US 3034335A
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primer
barrel
firing pin
retainer
testing device
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US784826A
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Hollis L Muller
Stanley J Kent
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C21/00Checking fuzes; Testing fuzes

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  • This invention relates to devices for testing primers such as are utilized to detonate explosive charges, and more especially to a primer testing device which functions to test a primer under substantially the same as those encountered in its use.
  • the firing pin is held in place by a shear pin until there has been applied to it a gas pressure suificient to shear the shear pin.
  • the firing pin then travels under extremely high pressure until it strikes the primer with a force greatly in excess of that imparted by a spring actuated firing pin,
  • the conventional drop test method is therefore unsuitable for testing primers intended to be fired by gas operated firing pins.
  • FIG. 1 illustrates the invention as applied to a high energy primer testing device
  • FIG. 2 illustrates a low energy primer tester
  • FIG. 3 illustrates a short cartridge container which permits the performance of the tested primer to be determined by photographing the flash produced by it.
  • the primer testing device of FIG. 1 includes a barrel it) which is threaded at both ends. Threaded onthe gas pressure inlet end of this barrel is a cap 11 and threaded on its gas pressure outlet end is a cartridge retainer 12. The end cap 11 is internally threaded for connection to a gas supply pipe or hose.
  • the purpose of the cartridge container 12 is to hold a cartridge (containing the primer to be tested) against a firing pin receiving head 13. This head 13 functions to stop the firing pin at the end of its travel and has an opening through which a protruded end of the firing pin extends and strikes the primer. This stopping of the firing pin means after it has performed its purpose of firing the primer.
  • the firing pin 14 is slidable in the barrel 16, is fixed to this barrel by a shear pin 15' and has a seal ring 16.
  • the length of the firing pin protrusion 17 depends on the amount of indentation required to be formed in the particular primer under test.
  • the firing head end of the barrel it) is provided with tour vents 18 to permit escape of the air ahead of the moving firing pin.
  • the short barrel retainer 19 of FIG. 2' may be used.
  • the firing pin is fixed to a barrel 2% which includes a firing pin receiving head 13 and is inserted into the retainer 19 after which a cartridge retainer similar to cartridge retainer 12 of FIG. 1 is threaded onto the retm'ner 19.
  • a barrel of predetermined length and a firing pin having a predetermined protrusion are selected after which the firing pin is fixed to the barrel by a shear pin as illustrated. Then the primer to be tested is inserted into a cartridge, the cartridge is placed in the cartridge retainer 12, the firing pin receiving head 13 is positioned at the end of the barrel and the cartridge retainer is screwed onto the barrel. The end cap 11 is then screwed onto the other end of the barrel and the gas supply pipe or hose is screwed into the end cap.
  • the actual test of the primer is consummated by admitting gas under pressure through the end cap connection. This ruptures the shear pin and drives the firing pin against the primer with a force similar to that to be encountered by this particular type of primer in actual use.
  • a short cartridge retainer 21 (see FIG. 3) may be used.
  • the preparation for a test with the device of PEG. 2 is similar to that outlined in connection with the device of FIG. 1.
  • a purpose of the longitudinal slots 22 shown in the drawing in the cartridge case retainer 12 in FIG. 1, is to enable the primer flame alone to be visible. Were a propellant present the issuing flame would be much longer and any photographic record of the flame would no longer be that of the primer being tested.
  • An advantage of the head 13 is to absorb the energy of the firing pin 14 after it has performed its function of firing the primer being tested.
  • a testing device for primers actuated by gas pressure in which the length of a primer flame may be measured for the gas pressure used for actuating such primer said device comprising in combination a barrel provided at one end with connection for a source of gas pressure and at the opposite end with a retainer for holding a primer being tested while a primer flame may be visible, said connection including a cap threaded onto the outside of said barrel and having an internally threaded passageway leading into said'barrel, said retainer for a primer being tested being threaded onto an end of said barrel opposite said cap, a firing pin having a cylindrical main body with a cylindrical protrusion fixed on the forward end and of smaller diameter than the main body'and slidable in said barrel to fire a primer, a shear pin between said barrel and firing pin adjacent said cap, a firing pin receiving head between said retainer and said barrel and adapted to be pressed against an end .of said barrel by said retainer, said head iirniting the penetration of said firing pin intosaid primer and absorb the energy

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Description

y 15, 1962 H. L. MULLER ET AL 3,034,335
PRIMER TESTING DEVICE Filed Jan. 2 1959 V I 2y FIG.2.
FIG.3.
HOLLIS L.III\\AIEEIIY%R' YBYJSQANLEY KENT aafi mke #W W ATTORNEYS United States Patent 3,034,335 PR TESTING DEVIQE Hollis L. Mulier, York Springs, and Stanley J. Kent,
Abington, Pa, assignors to the United States oi America as represented by the Secretary of the Army Filed Jan. 2, 1959, Ser. No. 784,826
1 Claim. (Cl. 73-35) (Granted under Title 3'5, US. Code (1952), see. 266) The invention described herein may be manufactured and'used by or for the Government for governmental purposes without the payment of any royalty thereon.
- This invention relates to devices for testing primers such as are utilized to detonate explosive charges, and more especially to a primer testing device which functions to test a primer under substantially the same as those encountered in its use.
Heretofore primers have been tested by the drop test method. In this method, a mass is dropped from a certain height. This mass strikes a firing pin which, in turn, strikes the primer being tested. By changing the mass or the height from which it is dropped, it is possible to vary the energy delivered to the primer. This method is adequate for testing primers intended to be fired by a spring actuated firing pin. I
Where the primer is intended to be fired by gas pressure, however, altogether different conditions are encountered. In this case, the firing pin is held in place by a shear pin until there has been applied to it a gas pressure suificient to shear the shear pin. The firing pin then travels under extremely high pressure until it strikes the primer with a force greatly in excess of that imparted by a spring actuated firing pin, The conventional drop test method is therefore unsuitable for testing primers intended to be fired by gas operated firing pins.
in accordance with the present invention, this d'ilficulty is avoided by the provision of a primer testing device which establishes conditions similar to those under which the primer is put to actual use. The invention will be better understood from the following description when considered in connection with the accompanying drawings and its scope is indicated by the appended claim.
Referring to the drawings:
FIG. 1 illustrates the invention as applied to a high energy primer testing device,
FIG. 2 illustrates a low energy primer tester, and
FIG. 3 illustrates a short cartridge container which permits the performance of the tested primer to be determined by photographing the flash produced by it.
The primer testing device of FIG. 1 includes a barrel it) which is threaded at both ends. Threaded onthe gas pressure inlet end of this barrel is a cap 11 and threaded on its gas pressure outlet end is a cartridge retainer 12. The end cap 11 is internally threaded for connection to a gas supply pipe or hose. The purpose of the cartridge container 12 is to hold a cartridge (containing the primer to be tested) against a firing pin receiving head 13. This head 13 functions to stop the firing pin at the end of its travel and has an opening through which a protruded end of the firing pin extends and strikes the primer. This stopping of the firing pin means after it has performed its purpose of firing the primer.
The firing pin 14 is slidable in the barrel 16, is fixed to this barrel by a shear pin 15' and has a seal ring 16. The length of the firing pin protrusion 17 depends on the amount of indentation required to be formed in the particular primer under test. The firing head end of the barrel it) is provided with tour vents 18 to permit escape of the air ahead of the moving firing pin.
By varying the length of the barrel 10, it is possible to vary the energy with which the firing pin strikes the primer and by varying the length'of the protrusion 17, the indentation of the primer is varied. It is thus possible to change these two factors which most afiect the performance of the primer.
When the length of the barrel is too short for the end cap 11 and cartridge retainer 12 to be threaded onto it, the short barrel retainer 19 of FIG. 2' may be used. In this case, the firing pin is fixed to a barrel 2% which includes a firing pin receiving head 13 and is inserted into the retainer 19 after which a cartridge retainer similar to cartridge retainer 12 of FIG. 1 is threaded onto the retm'ner 19.
In preparing to test a primer in the device of FIG. 1, a barrel of predetermined length and a firing pin having a predetermined protrusion are selected after which the firing pin is fixed to the barrel by a shear pin as illustrated. Then the primer to be tested is inserted into a cartridge, the cartridge is placed in the cartridge retainer 12, the firing pin receiving head 13 is positioned at the end of the barrel and the cartridge retainer is screwed onto the barrel. The end cap 11 is then screwed onto the other end of the barrel and the gas supply pipe or hose is screwed into the end cap.
The actual test of the primer is consummated by admitting gas under pressure through the end cap connection. This ruptures the shear pin and drives the firing pin against the primer with a force similar to that to be encountered by this particular type of primer in actual use.
If it is desired to make a photographic record of the performance of the tested primer, a short cartridge retainer 21 (see FIG. 3) may be used. As will be understood by those skilled in the art, the preparation for a test with the device of PEG. 2 is similar to that outlined in connection with the device of FIG. 1. A purpose of the longitudinal slots 22 shown in the drawing in the cartridge case retainer 12 in FIG. 1, is to enable the primer flame alone to be visible. Were a propellant present the issuing flame would be much longer and any photographic record of the flame would no longer be that of the primer being tested. An advantage of the head 13 is to absorb the energy of the firing pin 14 after it has performed its function of firing the primer being tested. In this way it may preclude the protrusion 17 going further than necessary into a primer cup and reduce the danger of excess gas pressure supplied to the cap 11 puncturing the cup of the primer being tested and allowing the primer fiame to issue rearwardly as well as forwardly under reduced pressure and an error in the photographic record of the primer flame length.
We claim:
A testing device for primers actuated by gas pressure in which the length of a primer flame may be measured for the gas pressure used for actuating such primer, said device comprising in combination a barrel provided at one end with connection for a source of gas pressure and at the opposite end with a retainer for holding a primer being tested while a primer flame may be visible, said connection including a cap threaded onto the outside of said barrel and having an internally threaded passageway leading into said'barrel, said retainer for a primer being tested being threaded onto an end of said barrel opposite said cap, a firing pin having a cylindrical main body with a cylindrical protrusion fixed on the forward end and of smaller diameter than the main body'and slidable in said barrel to fire a primer, a shear pin between said barrel and firing pin adjacent said cap, a firing pin receiving head between said retainer and said barrel and adapted to be pressed against an end .of said barrel by said retainer, said head iirniting the penetration of said firing pin intosaid primer and absorb the energy of the firing pin after it has fired a primer, and a vent passageway from inside the barrel adjacent said head to the outside of said barrel.
References Cited in the file of this patent UNITED STATES PATENTS
US784826A 1959-01-02 1959-01-02 Primer testing device Expired - Lifetime US3034335A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0439998A1 (en) * 1990-01-31 1991-08-07 Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste Testing device with acceleration tube

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US421307A (en) * 1890-02-11 reynolds
US1801449A (en) * 1928-08-30 1931-04-21 Olsen Fredrich Apparatus for testing explosives
US2537096A (en) * 1949-02-04 1951-01-09 Jr Charles A Shreeve High acceleration shock testing air gun
US2843042A (en) * 1951-08-04 1958-07-15 Montedison Spa Non-metallic mine fuse

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US421307A (en) * 1890-02-11 reynolds
US1801449A (en) * 1928-08-30 1931-04-21 Olsen Fredrich Apparatus for testing explosives
US2537096A (en) * 1949-02-04 1951-01-09 Jr Charles A Shreeve High acceleration shock testing air gun
US2843042A (en) * 1951-08-04 1958-07-15 Montedison Spa Non-metallic mine fuse

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0439998A1 (en) * 1990-01-31 1991-08-07 Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste Testing device with acceleration tube
US5184499A (en) * 1990-01-31 1993-02-09 Schweizerische Eidgenossenschaft Vertreten Durch Die Eidg. Munitionsfabrik Thun Der Gruppe Fur Rustungsdienste Testing device with acceleration tube

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