IP Library Granted Patent US 8,967,046
Granted Patent B2
US 8,967,046 · App. 13/690,040 · Granted Mar 3, 2015

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

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Quick Facts
Patent No.
US 8,967,046
App. No.
13/690,040
Granted
Mar 3, 2015
Kind
B2
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.

Claims (65)

1. A gas generator for use in launching a projectile, comprising:

a housing having a longitudinal axis and configured to be used with a launch tube for the projectile, the housing comprising:

a first plenum;

a second plenum adjacent to the first plenum;

a first plurality of apertures in the housing extending from the first plenum to the second plenum in a first direction transverse to the longitudinal axis of the housing; and

a second plurality of apertures in the housing, the second plurality of apertures extending from the second plenum to an exterior portion of the housing in a second direction along the longitudinal axis of the housing, wherein the gas generator is configured to form a plurality of propulsive jets exiting the gas generator through the second plurality of apertures in a direction substantially parallel to the longitudinal axis of the housing of the gas generator to launch the projectile, wherein the second plenum of the gas generator is in unrestricted communication with the second plurality of apertures to enable 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;

at least one propellant positioned within the first plenum of the housing; and

an initiator for igniting the at least one propellant, the initiator positioned proximate to the at least one propellant in the housing.

2. The gas generator of claim 1 , wherein the first plenum is positioned at a central portion of the housing.

3. The gas generator of claim 1 , wherein the housing has an outer surface sized and configured to be positioned adjacent to and engage with an inner surface of the launch tube when the gas generator is disposed within the launch tube.

4. The gas generator of claim 1 , wherein the housing comprises:

an outer housing; and

an inner housing disposed at least partially within the outer housing, wherein the first plenum is located within the inner housing, wherein the second plenum is located between the inner housing and the outer housing, and wherein the first plurality of apertures and the second plurality of apertures are located in the inner housing.

5. The gas generator of claim 4 , wherein the second plurality of apertures in the inner housing are located to form a ring of apertures about the longitudinal axis of the housing.

6. The gas generator of claim 1 , wherein a diameter of each of the first plurality of apertures is less than a diameter of each of the second plurality of apertures.

7. The gas generator of claim 1 , further comprising a burst foil disposed between the at least one propellant and each aperture of the first plurality of apertures.

8. A launch tube assembly, comprising:

a tube containing at least one projectile; and

the gas generator of claim 1 disposed within the tube adjacent the at least one projectile.

9. A method of launching a projectile using the gas generator of claim 1 adjacent a projectile in a launch tube, the method comprising:

providing the gas generator of claim 1 ;

igniting the at least one propellant with the initiator;

combusting at least a portion of the at least one propellant to form a gas;

flowing the gas through the first plurality of apertures formed in the housing surrounding the first plenum in the first direction to the second plenum; and

flowing the gas through the second plurality of apertures formed in the housing in the second direction to form the plurality of propulsive jets exiting from the housing; and

imparting an initial velocity to the projectile with the plurality of propulsive jets.

10. The method of claim 9 , further comprising retaining the gas in the first plenum with a burst foil until the gas reaches a predetermined pressure within the first plenum.

11. The method of claim 9 , further comprising introducing the gas into the second plenum to reduce the pressure of the gas.

12. The method of claim 9 , further comprising reorienting flow of the gas from the first direction to the second direction that is transverse to the first direction.

13. The method of claim 9 , further comprising forming the plurality of propulsive jets in a ring extending about the longitudinal axis of the housing of the gas generator at an exit portion of the gas generator.

14. A gas generator for use in launching a projectile, comprising:

a housing having a longitudinal axis and configured to be used with a launch tube for the projectile, the housing comprising:

a first plenum positioned at a central portion of the housing;

a second plenum adjacent to the first plenum;

a first plurality of apertures in the housing extending from the first plenum to the second plenum in a first direction transverse to the longitudinal axis of the housing; and

a second plurality of apertures in the housing, the second plurality of apertures extending from the second plenum to an exterior portion of the housing in a second direction along the longitudinal axis of the housing, wherein the gas generator is configured to form a plurality of propulsive jets exiting the gas generator through the second plurality of apertures in a direction substantially parallel to the longitudinal axis of the housing of the gas generator to launch the projectile, wherein the second plenum substantially surrounds the first plenum, and wherein the second plenum is substantially free of a combustible gas generating material immediately prior to ignition of the gas generator;

at least one propellant positioned within the first plenum of the housing; and

an initiator for igniting the at least one propellant, the initiator positioned proximate to the at least one propellant in the housing.

15. The gas generator of claim 14 , wherein the housing has a substantially cylindrical shape.

16. A gas generator for use in launching a projectile, comprising:

a housing having a longitudinal axis and configured to be used with a launch tube for the projectile, the housing comprising:

a first plenum;

a second plenum adjacent to the first plenum;

a first plurality of apertures in the housing extending from the first plenum to the second plenum in a first direction transverse to the longitudinal axis of the housing;

a second plurality of apertures in the housing, the second plurality of apertures extending from the second plenum to an exterior portion of the housing in a second direction along the longitudinal axis of the housing, wherein the gas generator is configured to form a plurality of propulsive jets exiting the gas generator through the second plurality of apertures in a direction substantially parallel to the longitudinal axis of the housing of the gas generator to launch the projectile;

at least one propellant positioned within the first plenum of the housing;

an initiator for igniting the at least one propellant, the initiator positioned proximate to the at least one propellant in the housing; and

a shock attenuator comprising a shield positioned within the at least one propellant and disposed between the initiator and at least a portion of the at least one propellant.

17. The gas generator of claim 16 , further comprising an explosive booster disposed between the initiator and at least a portion of the at least one propellant.

18. A gas generator for use in launching a projectile, comprising:

a housing having a longitudinal axis, the housing comprising:

a first plenum;

a second plenum adjacent to the first plenum;

a first plurality of apertures in the housing extending from the first plenum to the second plenum in a first direction transverse to the longitudinal axis of the housing; and

a second plurality of apertures in the housing, the second plurality of apertures extending from the second plenum to an exterior portion of the housing in a second direction along the longitudinal axis of the housing, wherein the gas generator is configured to enable gas within the second plenum to exit the second plenum unrestricted through the second plurality of apertures in a direction substantially parallel to the longitudinal axis of the housing of the gas generator to form a plurality of propulsive jets exiting the gas generator and to launch the projectile;

at least one propellant positioned within the first plenum of the housing; and

an initiator for igniting the at least one propellant, the initiator positioned proximate to the at least one propellant in the housing.

19. A gas generator for use in launching a projectile, comprising:

a housing having a longitudinal axis, the housing comprising:

a first plenum;

a second plenum adjacent to the first plenum;

a first plurality of apertures in the housing extending from the first plenum to the second plenum in a first direction transverse to the longitudinal axis of the housing; and

a second plurality of apertures in the housing, the second plurality of apertures extending from the second plenum to an exterior portion of the housing in a second direction along the longitudinal axis of the housing;

at least one propellant positioned within the first plenum of the housing, wherein the second plenum is substantially free of a propellant prior to ignition of the gas generator; and

an initiator for igniting the at least one propellant, the initiator positioned proximate to the at least one propellant in the housing.

Assignments (10)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 8, 2021
From: NORTHROP GRUMMAN INNOVATION SYSTEMS LLC
To: NORTHROP GRUMMAN SYSTEMS CORPORATION
Reel/Frame 055256/0892 →
CHANGE OF NAME Recorded Feb 4, 2021
From: NORTHROP GRUMMAN INNOVATION SYSTEMS, INC.
To: NORTHROP GRUMMAN INNOVATION SYSTEMS LLC
Reel/Frame 055223/0425 →
CHANGE OF NAME Recorded Nov 1, 2018
From: ORBITAL ATK, INC.
To: NORTHROP GRUMMAN INNOVATION SYSTEMS, INC.
Reel/Frame 047400/0381 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jun 6, 2018
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS ADMINISTRATIVE AGENT
To: ORBITAL ATK, INC.
Reel/Frame 046477/0874 →
RELEASE OF SECURITY INTEREST Recorded Oct 8, 2015
From: BANK OF AMERICA, N.A.
To: ALLIANT TECHSYSTEMS INC.; FEDERAL CARTRIDGE CO.; EAGLE INDUSTRIES UNLIMITED, INC.; AMMUNITION ACCESSORIES, INC.; ORBITAL ATK, INC. (F/K/A ALLIANT TECHSYSTEMS INC.)
Reel/Frame 036816/0624 →
SECURITY AGREEMENT Recorded Sep 30, 2015
From: ORBITAL ATK, INC.; ORBITAL SCIENCES CORPORATION
To: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS ADMINISTRATIVE AGENT
Reel/Frame 036732/0170 →
CHANGE OF NAME Recorded May 22, 2015
From: ALLIANT TECHSYSTEMS INC.
To: ORBITAL ATK, INC.
Reel/Frame 035753/0373 →
SECURITY AGREEMENT Recorded Nov 26, 2013
From: ALLIANT TECHSYSTEMS INC.; CALIBER COMPANY; EAGLE INDUSTRIES UNLIMITED, INC.; FEDERAL CARTRIDGE COMPANY; SAVAGE ARMS, INC.; SAVAGE RANGE SYSTEMS, INC.; SAVAGE SPORTS CORPORATION
To: BANK OF AMERICA, N.A.
Reel/Frame 031731/0281 →
INTELLECTUAL PROPERTY SECURITY AGREEMENT SUPPLEMENT Recorded Jan 31, 2013
From: ALLIANT TECHSYSTEMS INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 029732/0140 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 30, 2012
From: DUNAWAY, JAMES D.; GARBE, DUANE J.; SAMPSON, WILLIAM P.; HATCH, ROBERT L.
To: ALLIANT TECHSYSTEMS INC.
Reel/Frame 029383/0219 →