Actuators for gun-fired projectiles and mortars

Patent metadata

Field	Value
Publication number	US-9151581-B2
Application number	US-201113164730-A
Country	US
Kind code	B2
Filing date	Jun 20, 2011
Priority date	Sep 7, 2005
Publication date	Oct 6, 2015
Grant date	Oct 6, 2015

Abstract

A method for providing actuation thrust to a projectile. The method including: providing two or more individual actuators movably disposed in a stack housing, each of the two or more individual actuators being separated by a separation layer; accelerating exhaust from the two or more individual actuators with an accelerating nozzle having at least a convergent section terminating at a throat; and maintaining a constant volume in the accelerating nozzle after actuation of each of the two or more individual actuators.

First claim

What is claimed is:

1. An actuator stack comprising:
a stack housing;
two or more individual actuators movably disposed in the stack housing;
a separation layer formed between adjacent individual actuators;
an accelerating nozzle having at least a convergent section terminating at a throat; and
a biasing member for moving one of the two or more individual actuators towards the accelerating nozzle after another of the two or more individual actuators has been burned, wherein at least one of the two or more individual actuators comprises; a detonation charge; a primer for igniting the detonation charge; and detonation wiring for powering the primer.

2. The actuator stack of claim 1 , wherein the accelerating nozzle further includes a divergent section for expansion of matter emanating through the throat.

3. The actuator stack of claim 1 , wherein the biasing member is a compression spring.

4. The actuator stack of claim 1 , wherein each of the two or more individual actuators comprises an outer enclosure formed of a combustible material, wherein the separation layer extends between adjacent outer enclosures.

5. The actuator stack of claim 1 , wherein the stack housing includes a stop for limiting movement of the two or more individual actuators at a predetermined distance from the accelerating nozzle.

6. A projectile comprising;
an actuator stack disposed in or on a casing of the projectile, the actuator stack comprising:
a stack housing;
two or more individual actuators movably disposed in the stack housing;
a separation layer formed between adjacent individual actuators;
an accelerating nozzle having at least a convergent section terminating at a throat; and
a biasing member for biasing one of the two or more individual actuators towards the accelerating nozzle after another of the two or more individual actuators has been burned, wherein at least one of the two or more individual actuators comprises; a detonation charge; a primer for igniting the detonation charge; and detonation wiring for powering the primer.

7. The projectile of claim 6 , wherein the accelerating nozzle further includes a divergent section for expansion of matter emanating through the throat.

8. The projectile of claim 6 , wherein the biasing member is a compression spring.

9. The projectile of claim 6 , wherein each of the two or more individual actuators comprises an outer enclosure formed of a combustible material, wherein the separation layer extends between adjacent outer enclosures.

10. The projectile of claim 6 , wherein the stack housing includes a stop for limiting movement of the two or more individual actuators at a predetermined distance from the accelerating nozzle.

11. A method for providing actuation thrust to a projectile, the method comprising: providing two or more individual actuators movably disposed in a stack housing, each of the two or more individual actuators being separated by a separation layer; accelerating exhaust from the two or more individual actuators with an accelerating nozzle having at least a convergent section terminating at a throat; and maintaining a constant volume in the accelerating nozzle after actuation of each of the two or more individual actuators, wherein the maintaining step comprises moving one of the two or more individual actuators towards the accelerating nozzle after another of the two or more individual actuators has been actuated.

Assignees

• Rastegar Jahangir S
• Spinelli Thomas
• Omnitek Partners Llc

Inventors

• Rastegar Jahangir S
• Spinelli Thomas

Classifications

• F42B10/668

  Injection of a fluid, e.g. a propellant, into the gas shear in a nozzle or in the boundary layer at the outer surface of a missile, e.g. to create a shock wave in a supersonic flow · CPC title

• F42B10/661 Primary

  using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge · CPC title