Gas generators, launch tubes including gas generators and related systems and methods

Patent metadata

Field	Value
Publication number	US-9605932-B2
Application number	US-201514606601-A
Country	US
Kind code	B2
Filing date	Jan 27, 2015
Priority date	Nov 30, 2012
Publication date	Mar 28, 2017
Grant date	Mar 28, 2017

Abstract

Gas generators may be utilized for launching a projectile. Launch tubes may include gas generators. Methods of launching a projectile may include utilizing gas generators to impart an initial velocity to a projectile.

First claim

What is claimed is:

1. A method of launching a projectile, the method comprising:
positioning a gas generator within a launch tube;
placing the projectile in the launch tube proximate the gas generator;
igniting a propellant with an initiator disposed in a first plenum of a housing of the gas generator;
combusting at least a portion of the propellant to form a gas;
flowing the gas through a first plurality of apertures formed in the housing surrounding the first plenum in a first direction to a second plenum at least partially laterally surrounding the first plenum and the first plurality of apertures;
flowing the gas through a second plurality of apertures formed in the housing in a second direction that is transverse to the first direction to form a plurality of propulsive jets exiting from the housing;
imparting an initial velocity to the projectile responsive to contact thereof by the plurality of propulsive jets exiting from the housing; and
launching the projectile from the launch tube with the plurality of propulsive jets produced by the gas generator.

2. The method of claim 1 , further comprising retaining the gas in the first plenum with a burst foil until the gas reaches a predetermined pressure within the first plenum.

3. The method of claim 1 , further comprising introducing the gas directly into the second plurality of apertures from the second plenum, wherein the second plenum is positioned radially outward from the first plenum.

4. The method of claim 1 , further comprising forming the plurality of propulsive jets in a ring extending about a longitudinal axis of the housing of the gas generator at an exit portion of the gas generator.

5. The method of claim 1 , further comprising dissipating a shockwave formed by actuation of the initiator with a shock attenuation device positioned within the propellant.

6. The method of claim 1 , further comprising enabling gas within the second plenum of the gas generator to freely exit the gas generator via the second plurality of apertures as the plurality of propulsive jets to impart the initial velocity to the projectile.

7. The method of claim 1 , further comprising forming the plurality of propulsive jets exiting the gas generator through the second plurality of apertures in a direction substantially parallel to a longitudinal axis of the housing of the gas generator to impart the initial velocity to the projectile.

8. The method of claim 1 , wherein flowing the gas through the first plurality of apertures formed in the housing surrounding the first plenum in a first direction to the second plenum comprises flowing the gas through the first plurality of apertures to the second plenum, wherein the second plenum is substantially free of a combustible gas generating material immediately prior to ignition of the propellant in the gas generator.

9. The method of claim 1 , wherein imparting an initial velocity to the projectile comprises imparting the initial velocity to the projectile comprising a self-propelled projectile having an integrated propulsion system.

10. The method of claim 1 , further comprising:
positioning a piston between the projectile and the gas generator to at least partially isolate the projectile from the plurality of propulsive jets produced by the gas generator; and
imparting the initial velocity to the projectile by applying thrust to the piston with the plurality of propulsive jets produced by the gas generator.

11. A method of launching a projectile, the method comprising:
positioning a gas generator separate from the projectile within a launch tube;
placing the projectile in the launch tube in a position proximate the separate gas generator;
igniting the gas generator to form a gas in a first plenum of the gas generator;
flowing the gas through a first plurality of apertures surrounding the first plenum in a first direction to a second plenum;
reorienting flow of the gas from the first direction to a second direction that is transverse to the first direction and directed toward the projectile in the launch tube;
flowing the gas through a second plurality of apertures in the second direction to form a plurality of propulsive jets exiting from the gas generator in a direction toward the projectile; and
launching the projectile from the launch tube with the plurality of propulsive jets produced by the gas generator.

12. The method of claim 11 , further comprising positioning the gas generator in the launch tube to orient flow of the gas in the first direction to be transverse to a longitudinal axis of the launch tube and to orient flow of the gas in the second direction to be substantially parallel to the longitudinal axis of the launch tube.

13. The method of claim 11 , further comprising, after launching the projectile from the launch tube, increasing a velocity of the projectile with a propellant system of the projectile separate from the gas generator.

14. The method of claim 11 , further comprising sealing a portion of the gas generator within the launch tube at a closed end of the launch tube opposing an open end of the launch tube through which the projectile is launched.

15. The method of claim 11 , further comprising directing the gas through the first plurality of apertures to the second plenum to reduce at least one of a temperature and a pressure of the gas, wherein the second plenum is substantially free of a combustible gas generating material immediately prior to ignition of the gas generator.

16. A method of launching a projectile, the method comprising:
igniting at least one propellant positioned within a first plenum defined in a central portion of a gas generator positioned in a launch tube with an initiator positioned proximate to the at least one propellant;
flowing gas from the first plenum into a second plenum substantially surrounding the at least one propellant through a plurality of apertures;
flowing the gas out of the second plenum through a second plurality of apertures into a chamber containing the projectile; and
forming a plurality of propulsive jets with the gas generator exiting the gas generator through the second plurality of apertures in a direction substantially parallel to a longitudinal axis of the launch tube to impart an initial velocity to a projectile positioned within the launch tube.

Assignees

• Orbital Atk Inc

Inventors

• Dunaway James D
• Garbe Duane J
• Sampson William P
• Hatch Robert L

Classifications

• F42B3/04 Primary

  for producing gas under pressure {(generators of inflation fluid especially adapted for vehicle air bags B60R21/26)} · CPC title

• F41F3/04

  for rockets · CPC title

• F41A1/04

  Missile propulsion using the combustion of a liquid, {loose powder} or gaseous fuel, e.g. hypergolic fuel · CPC title