|Publication number||US3750581 A|
|Publication date||Aug 7, 1973|
|Filing date||Sep 20, 1971|
|Priority date||Sep 20, 1971|
|Publication number||US 3750581 A, US 3750581A, US-A-3750581, US3750581 A, US3750581A|
|Inventors||R Betts, N Williams|
|Original Assignee||Us Army|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (5), Referenced by (5), Classifications (9)|
|External Links: USPTO, USPTO Assignment, Espacenet|
United States Patent 1 i 3,750,581 Betts et al. Aug. 7, 1973  MISSILE MOTOR IGNITER ASSEMBLY 3,446,022 5/1969 Olliff, Jr. et al. 60/256  Inventors: Robert E. Betts; Nathan P. Williams, 1 3:51;: 222 both of Humsvllle, 2,39l,865 H1946 Chandler 60/256  Assignee: The United States of America as represented b th secretary of h Primary Examiner-Benjamin A. Borchelt Army, W hi C Assistant Examiner-G. E. Monto ne Attorney-- Harry M. Saragovitz, Edward J.  Filed: Sept. 20, 1971 Kelly et al  I App]; No.: 181,784 7 ABSTRACT An assembly for igniting a missile motor from a percus-  US. Cl 102/49-7, 60/256, 102/27 ign primer carried in a cartridge case to an ignite!  Int. Cl. F42b 15/00, FOZk 9/04 h r lo ated in the missle motor. A detonating cord,  Field of Search l02/49.7, 27 R; h i n of it ends positioned in the cartridge case,
39-82 E is used to transfer ignition from the primer to the igniter charge. The end of the detonating cord adjacent References Cited the cartridge case is retained in position by a holder UNITED STATES PATENTS mounted in the cartridge case. 3,103,884 9/1963 Ciccone et al. 102/27 R 2 Claims, 2 Drawing Fi PATENTED M13 7 FIG. I
Robert E Befls Nathan P. Williams, INVENTORY;
MISSILE MOTOR IGNITER ASSEMBLY BACKGROUND OF THE INVENTION This invention relates to the field of missile motor igniters. Existing missile motor igniter assemblies are rather detailed in design and hence very costly. These igniters require extensive screw machining of the cap end of igniter and other machine operations to fit a detonating cord in the igniter which causes a high cost.
SUMMARY OF THE INVENTION The present invention has utilized a cartridge case provided with a percussion primer at the cap end of the igniter assembly to actuate the igniter charge. The use of this cartridge case in conjunction with a percussion primer has resulted in a much cheaper cap for missile motor igniters.
The invention may be better understood from the following detailed description taken in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. I is a diagrammative view showing the igniter assembly mounted in position on a missile.
FIG. 2 is a enlarged sectional view of the igniter assembly removed from the missile motor.
DESCRIPTION OF THE PREFERRED EMBODIMENT Reference numeral generally indicates an igniter assembly for igniting a motor of a missile 50. The assembly includes a tube 3 attached to a cap 5 which is provided with means 7 thereon for mounting the assembly on the missile motor. An igniter charge 9 is located in the tube which is vented by several openings 11 for allowing the igniter charge gases to escape thus enhancing the burning rate of the charge. The cap is provided with a central opening 13 and a cartridge case 15 is located in this opening. The cartridge case includes a portion 17 to provide a support for mounting a PLEXIGLAS holder 19 thereon. This holder is fitted snug in the cartridge case and is sealed thereto by a sealing means 20 such as epoxy. A detonating cord 21, such as pyrocore or a mild detonating fuse, is fixedly mounted in the holder by a sealing means 22. By sealing the holder to the cartridge case protection is provided against external environmental effects on the igniter charge and against deterioration of the end of the detonating cord. One end of the cord is disposed adjacent a percussion primer 23 located in the end of the cartridge case. Experimentation has determined that the proper stand-off distance of the detonating cord from the percussion primer will insure reliable ignition of the detonating cord. This stand-off distance is in the range of 20 thousands of an inch to one-fourth of an inch. The opposite end of the cord extends into the igniter charge 9 for transferring the ignition from the primer to the igniter charge. A member 25, provided with a firing pin opening 27, is located in an enlarged section of opening 13 and is provided with means 29 for engaging cap 3 to retain the cartridge case in the cap.
In operation a firing pin (not shown) strikes the percussion primer and causes it to fire and ignite the detonating cord. The ignited cord then burns until it ignites the igniter charge which in turn ignites a propellant 51 of the missile motor.
I. An assembly for igniting a missile motor comprising: a cartridge case provided with a percussion primer; a PLEXIGLAS holder mounted in said case in spaced relationship to said percussion primer cartridge, and a detonating cord secured to said holder with one of its ends at a predetermined distance from said percussion primer to enhance ignition of said cord and its opposite end extending away from said holder and into the motor igniter charge.
2. An assembly for igniting a missile motor comprising: a cap provided with means for mounting said assembly in said missile motor; a cartridge case supported in said cap and provided with a percussion primer; said cap having a member for retaining the cartridge case in said cap, said member having an opening juxtaposition said percussion primer; a tube connected to said cap and provided with an igniter charge; said tube having a plurality of openings to enhance the burning rate of the igniter charge; a PLEXIGLAS holder mounted in said cartridge case in spaced relationship to said percussion primer, and a detonating cord secured to said holder with one of its ends at a predetermined distance from said percussion primer to enhance ignition of said cord and its opposite end extending away from said holder and into the motor igniter charge.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US2391865 *||Feb 14, 1942||Jan 1, 1946||Chandler Edward F||Self-propelled projectile|
|US3062147 *||Sep 28, 1959||Nov 6, 1962||Du Pont||Igniter for solid propellant grains|
|US3103884 *||Mar 16, 1962||Sep 17, 1963||Thomas Q Ciccone||Cartridge for more nearly uniform projectile velocities|
|US3388666 *||Mar 15, 1967||Jun 18, 1968||Karlsruhe Augsburg Iweka||Rifle grenade|
|US3446022 *||Feb 6, 1967||May 27, 1969||Thiokol Chemical Corp||Integral motor case and nozzle for solid propellant rocket motors|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US4068591 *||Mar 10, 1976||Jan 17, 1978||The United States Of America As Represented By The Secretary Of The Army||Ignition system used in testing solid propellant compositions for smokelessness|
|US4691633 *||Jun 6, 1986||Sep 8, 1987||Societe Nationale Des Poudres Et Explosifs||Igniter intended for gas-generating charges in shells|
|US6474239 *||Dec 8, 2000||Nov 5, 2002||Giat Industries||Igniter tube for artillery ammunition|
|US6857370 *||Apr 10, 2003||Feb 22, 2005||General Dynamics Ordnance And Tactical Systems, Inc.||Primer body|
|EP0204623A1 *||May 30, 1986||Dec 10, 1986||Societe Nationale Des Poudres Et Explosifs||Igniter for an additional charge in a shell|
|U.S. Classification||102/380, 102/202, 60/256|
|International Classification||F42C19/00, F42C19/08|
|Cooperative Classification||F42C19/0826, F42C19/0819|
|European Classification||F42C19/08G, F42C19/08H2|