Gas generators, launch tube assemblies including gas generators, and related systems and methods

• US 10,281,248 B2
• Filed: 11/11/2015
• Issued: 05/07/2019
• Est. Priority Date: 11/11/2015
• Status: Active Grant

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Innovation Systems, Inc. (Northrop Grumman Corporation)
• Inventors: Dunaway, James D.
• Primary Examiner(s): Clement, Michelle
• Application Number:
  US14/938,646
• Publication Number:
  US 20170131070A1
• Time in Patent Office: 1,273 Days
• Field of Search: 89 1818
• CPC Class Codes: B60R 21/2644 using only solid reacting substances, e.g. pellets, powder
• CPC Class Codes: F41F 3/04 for rockets
• CPC Class Codes: F42B 3/04 for producing gas under pressure generators of inflation fluid especially adapted for vehicle air bags B60R21/26

Abstract

A gas generator includes a housing sized and configured to be located within a launch tube for a projectile. The housing defines a first propellant chamber; at least a second propellant chamber comprising a ring situated concentrically around the first propellant chamber; an expansion chamber; at least one first aperture between the first propellant chamber and the expansion chamber; and at least one second aperture between the at least a second propellant chamber and the expansion chamber. The gas generator also includes at least one propellant within each of the first propellant chamber and the at least a second propellant chamber of the housing; and a pyrotechnic delay connecting the first propellant chamber and the second propellant chamber. A launch tube assembly includes a tube containing at least one projectile and a gas generator. Related methods of launching a projectile are also disclosed.

Claims

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

a housing sized and configured to be located within a launch tube for the projectile, the housing defining;

a first propellant chamber;

at least a second propellant chamber comprising a ring situated concentrically around the first propellant chamber;

an expansion chamber;

at least one first aperture between the first propellant chamber and the expansion chamber; and

at least one second aperture between the at least a second propellant chamber and the expansion chamber;

at least one propellant within each of the first propellant chamber and the at least a second propellant chamber of the housing; and

a pyrotechnic delay connecting the first propellant chamber and the at least a second propellant chamber.

2. The gas generator of claim 1, wherein the at least one first aperture and the at least one second aperture comprise a plurality of first apertures and a plurality of second apertures.

3. The gas generator of claim 1, further comprising a burst foil between at least one of the first propellant chamber and the at least a second propellant chamber and the at least one first aperture and the at least one second aperture.

4. The gas generator of claim 1, wherein the at least a second propellant chamber comprises a plurality of concentric propellant chambers.

5. The gas generator of claim 4, further comprising a pyrotechnic delay between each of the concentric propellant chambers.

6. The gas generator of claim 1, further comprising a screen between at least one of the first propellant chamber and the second propellant chamber and at least one of the at least one first aperture and the at least one second aperture.

7. The gas generator of claim 1, further comprising an initiator for igniting the pyrotechnic delay and the at least one propellant within the first propellant chamber.

8. The gas generator of claim 7, wherein the pyrotechnic delay is configured to ignite the at least one propellant within the at least a second propellant chamber after ignition of the at least one propellant within the first propellant chamber.

9. The gas generator of claim 1, wherein the housing has a substantially cylindrical shape.

10. 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.

11. The gas generator of claim 1, wherein the expansion chamber of the gas generator is in unrestricted communication with at least one third aperture to enable gas within the expansion chamber of the gas generator to exit the gas generator via the at least one third aperture as at least one propulsive jet.

12. The gas generator of claim 11, wherein a cross-sectional area of each of the at least one first aperture and the at least one second aperture is less than a cross-sectional area of each of the at least one third aperture.

13. The gas generator of claim 1, wherein the at least one propellant comprises a powdered or cast material.

21. The gas generator of claim 1, wherein the pyrotechnic delay comprises a material selected from the group consisting of boron potassium nitrate (BKNO₃), magnesium strontium nitrate (MgSr(NO₃)₂), and magnesium-potassium perchlorates.

22. The gas generator of claim 1, wherein the at least one propellant comprises solid grains of propellant.

14. A launch tube assembly, comprising:

a launch tube containing at least one projectile; and

a gas generator within the launch tube proximate the at least one projectile, the gas generator comprising;

a housing comprising;

a first propellant chamber;

at least a second propellant chamber comprising a ring situated concentrically around the first propellant chamber;

an expansion chamber;

at least one first aperture between the first propellant chamber and the expansion chamber; and

at least one second aperture between the at least a second propellant chamber and the expansion chamber;

at least one propellant within each of the first propellant chamber and the at least a second propellant chamber of the housing; and

a pyrotechnic delay connecting the first propellant chamber and the at least a second propellant chamber.

15. A method of launching a projectile, the method comprising:

igniting a first propellant within a first propellant chamber within a housing of a gas generator;

igniting a pyrotechnic delay within the housing, the pyrotechnic delay connecting the first propellant chamber and at least a second propellant chamber, the at least a second propellant chamber comprising a ring situated concentrically around the first propellant chamber;

igniting a second propellant within the at least a second propellant chamber;

combusting at least a portion of the first propellant and the second propellant to form a gas;

flowing the gas into an expansion chamber within the housing via at least one first aperture between the expansion chamber and the first propellant chamber and at least one second aperture between the expansion chamber and the at least a second propellant chamber;

flowing the gas through a plurality of third apertures formed in the housing to form at least one propulsive jet exiting the housing; and

imparting an initial velocity to a projectile with the at least one propulsive jet.

16. The method of claim 15, further comprising retaining the gas within at least the first propellant chamber with a burst foil until the gas reaches a predetermined pressure within the first propellant chamber.

17. The method of claim 15, further comprising reducing the pressure of the gas as the gas flows into the expansion chamber.

18. The method of claim 15, further comprising forming a 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.

19. The method of claim 15, further comprising simultaneously igniting the pyrotechnic delay and the first propellant with an initiator.

20. The method of claim 15, wherein igniting the second propellant comprises igniting the second propellant after igniting the first propellant.