Shock hardened initiator and initiator assembly

Patent metadata

Field	Value
Publication number	US-9816790-B2
Application number	US-201414257181-A
Country	US
Kind code	B2
Filing date	Apr 21, 2014
Priority date	Feb 7, 2011
Publication date	Nov 14, 2017
Grant date	Nov 14, 2017

Abstract

Embodiments of an initiator support assembly that includes an initiator housing including an initiator cavity system are generally described herein. In some embodiments, a bridge substrate is positioned within the initiator cavity. The bridge substrate includes a substrate base including a uniform first planar surface and an opposed second surface. The bridge substrate further includes a first bridge contact extending over the substrate base. The first bridge contact is substantially flush with the first planar surface. A second bridge contact extends over the substrate base. The second bridge contact is substantially flush with the first planar surface. The first and second bridge contacts and the uniform first planar surface form a continuous planar mounting surface. An explosive charge, positioned within the initiator cavity, includes a charge mounting surface that is continuously coupled in surface-to-surface contact across the continuous planar mounting surface.

First claim

What is claimed is:

1. An initiator assembly comprising:
an initiator housing including an initiator cavity having a cavity cross sectional area;
an explosive charge within the initiator cavity having a charge cross sectional area corresponding to the cavity cross sectional area;
a bridge substrate within the initiator cavity, the bridge substrate including:
a substrate base including a uniform first planar surface, and
a continuous planar mounting surface extending along the explosive charge, the continuous planar mounting surface includes first and second bridge contacts and the first planar surface, the first and second bridge contacts are substantially flush with the first planar surface, and the continuous planar mounting surface has a mounting surface cross sectional area corresponding to each of the charge cross sectional area and the cavity cross sectional area;

a flyer plate within the initiator cavity and engaged along the continuous planar mounting surface;
a barrel engaged along the flyer plate, the barrel faces the explosive charge and extends continuously outward from a barrel lumen to an initiator cavity wall of the initiator cavity; and
wherein each of the continuous planar mounting surface, the explosive charge, the flyer plate and the barrel are in continuous surface-to-surface contact across the initiator cavity from the barrel lumen to the initiator cavity wall.

2. The initiator assembly of claim 1 , wherein the continuous planar mounting surface and the explosive charge extend continuously across the initiator cavity and the explosive charge, the continuous planar mounting surface and any intervening components including the flyer plate and the barrel are continuously statically engaged in surface-to-surface contact across the initiator cavity.

3. The initiator assembly of claim 1 , wherein the first and second bridge contacts are elevated around 0.0015 inches or less relative to the first planar surface.

4. The initiator assembly of claim 1 , wherein one or more of the first and second bridge contacts include plated through holes, and the plated through holes are recessed relative to at least the first planar surface.

5. The initiator assembly of claim 1 comprising an ionizing bridge electrically coupled between the first and second bridge contacts,
wherein the bridge substrate includes a plate, and
wherein the plate supports the bridge substrate and directs a pressure within the initiator cavity developed by ionization of the ionizing bridge toward the explosive charge.

6. The initiator assembly of claim 1 comprising a flyer plate positioned within the initiator cavity and adjacent to the explosive charge,
wherein the bridge substrate, the explosive charge and the flyer plate are axially compressed within an initiator housing.

7. The initiator assembly of claim 1 , wherein the bridge substrate continuously spreads mechanical loads across the explosive charge through surface-to-surface contact with the continuous planar mounting surface.

8. An initiator assembly comprising:
an initiator housing including an initiator cavity having a cavity cross sectional area;
an explosive charge within the initiator cavity having a charge cross sectional area corresponding to the cavity cross sectional area;
a bridge substrate within the initiator cavity, the bridge substrate includes:
a substrate base including a uniform first planar surface and an opposed second surface, and
a first bridge contact extending from near an edge of the first planar surface to an ionizing bridge,
a second bridge contact extending from near the edge of the first planar surface to the ionizing bridge,
a continuous planar mounting surface extending along the explosive charge, the continuous planar mounting surface includes the first and second bridge contacts and the first planar surface, and the continuous planar mounting surface has a mounting surface cross sectional area corresponding to each of the charge cross sectional area and the cavity cross sectional area;

an isolation sleeve extending around the explosive charge and interposed between the initiator housing and the explosive charge, the isolation sleeve extends to the bridge substrate;
a flyer plate within the initiator cavity and engaged along the continuous planar mounting surface;
a barrel engaged along the flyer plate, the barrel extends continuously from a barrel lumen to a perimeter edge of the explosive charge, and the barrel faces the explosive charge; and
wherein each of the continuous planar mounting surface, the explosive charge, the flyer plate and the barrel are in continuous surface-to-surface contact across the initiator cavity from the barrel lumen to at least the perimeter edge of the explosive charge.

9. The initiator assembly of claim 8 , wherein the first and second bridge contacts are substantially flush with the first planar surface.

10. The initiator assembly of claim 9 , wherein the first and second bridge contacts are elevated around 0.0015 inches or less relative to the first planar surface.

11. The initiator assembly of claim 8 comprising:
a circuit board adjacent to the opposed second surface of the bridge substrate;
a header adjacent to the circuit board; and
wherein the opposed second surface is in continuous surface-to-surface contact with the circuit board, and
wherein the circuit board is in continuous surface-to-surface contact with the header.

12. The method of claim 8 comprising axially compressing at least the explosive charge and the bridge substrate with a flyer plate and a barrel therebetween.

13. The method of claim 8 comprising spreading mechanical loads on the explosive charge across the continuous planar mounting surface according to the corresponding charge cross sectional area and mounting surface cross sectional area.

14. A method of making an initiator assembly comprising:
positioning an explosive charge within an initiator cavity having a cavity cross sectional area, the explosive charge having a charge cross sectional area corresponding to the cavity cross sectional area;
positioning a bridge substrate within the initiator cavity;
positioning a continuous planar mounting surface of the bridge substrate along the explosive charge, positioning including:
positioning a uniform first planar surface across the explosive charge, and
positioning first and second bridge contacts across the explosive charge, the first and second bridge contacts substantially flush with the first planar surface, the continuous planar mounting surface includes each of the first planar surface and the first and second bridge contacts and has a mounting surface cross sectional area corresponding to each of the charge cross sectional area and the cavity cross sectional area;

positioning a barrel along the explosive charge, the barrel extending continuously from a barrel lumen to a perimeter edge of the explosive charge, the barrel having a barrel cross sectional area corresponding to the charge cross sectional area and the cavity cross sectional area; and
positioning a flyer along the barrel and the continuous planar mounting surface, the flyer having a flyer cross sectional area corresponding to the barrel cross sectional area, the cavity cross sectional area and the mounting surface cross sectional area of the continuous planar mounting surface.

15. The method of claim 14 comprising interposing an isolation sleeve between the explosive charge and an initiator housing including the initiator cavity, the isolation sleeve extending to the continuous planar mounting surface.

16. The metho

Assignees

• Raytheon Co

Inventors

• Biggs Bradley
• Bonbrake Timothy B
• Budy George Darryl
• Schott Christopher

Classifications

• F42C14/00

  {Mechanical} fuzes characterised by the ammunition class or type (F42C1/00, {F42C7/00, F42C9/00, F42C11/001}, F42C13/00, F42C15/00 take precedence) · CPC title

• F42B3/124 Primary

  characterised by the configuration or material of the bridge (F42B3/13 takes precedence) · CPC title

• F42B3/125

  characterised by the configuration of the bridge initiator case (F42B3/11 takes precedence) · CPC title

• F42C19/02

  Fuze bodies; Fuze housings · CPC title

• F42C9/00

  Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition · CPC title