Spooled propellant charge and method of manufacture thereof

• US 4,660,475 A
• Filed: 07/31/1985
• Issued: 04/28/1987
• Est. Priority Date: 07/31/1985
• Status: Expired due to Fees

• Current Assignee: Morton-Thiokol, Inc. (Howmet Aerospace, Inc.)
• Original Assignee: Morton-Thiokol, Inc. (Howmet Aerospace, Inc.)
• Inventors: Rogowski, Gerald W., Bell, Frank H.
• Primary Examiner(s): Nelson, Peter A.
• Application Number:
  US06/761,130
• Time in Patent Office: 636 Days
• Field of Search: 264/3 R, 264/3 A, 264/3 B, 264/3.1, 264/3.2, 264/3.3, 102/284
• US Class Current: 102/284
• CPC Class Codes: C06B 21/0075 by extrusion
• CPC Class Codes: C06B 45/00 Compositions or products which are defined by structure or arrangement of component of product explosive charges of particular form or shape F42B1/00, F42B3/00
• CPC Class Codes: F42B 5/16 characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder chemical composition C06B; F42B5/24 takes precedence

Abstract

A propellant charge is manufactured by spooling a strand of propellant onto a form member. In accordance with one embodiment of the invention, the form member is a spool composed of propellant, and the spooled propellant, including the spool, is loaded into a charge housing.

Claims

1. A method of manufacturing a propellant charge comprises the steps of:

a. preparing a strand of propellant;

b. preparing a form member to include an elongated member and a ridge member at each end of the elongated member which ridge member extends radially outwardly from the elongated member such that the form member has the shape of a spool upon which the propellant strand may be spooled; and

c. spooling the propellant strand on the form member between the ridge members whereby the ridge members serve to maintain the integrity of the spooled propellant on the elongated member.

2. A method according to claim 1 further comprises forming the form member from propellant.

3. A method according to claim 2 further comprises forming a hollow core in the form member and inserting an igniter in the hollow core.

4. A method according to claim 3 further comprises forming apertures in the core to provide communication between the igniter and the spooled propellant.

5. A method according to claim 2 further comprises loading the spooled propellant into a charge housing.

6. A method according to claim 5 wherein the step of loading the spooled propellant includes loading the form member with the propellant spooled thereon into the charge housing.

7. A method according to claim 5 further comprises curing the spooled propellant before loading it into a charge housing.

8. A method according to claim 1 further comprises loading the spooled propellant into a charge housing.

9. A method according to claim 1 wherein the step of preparing the propellant strand comprises extruding the propellant strand.

10. A propellant charge comprises a form member including an elongate member and a ridge member disposed at each end of and extending radially outwardly from said elongate member such that the form member has the shape of a spool, and at least one strand of propellant material spooled on said form member between said ridge members whereby the ridge members serve to maintain the integrity of the spooled propellant on the elongate member.

11. A propellant charge according to claim 10 wherein said form member is composed of propellant material.

12. A propellant charge according to claim 10 further comprises a charge housing in which said form member with propellant material spooled thereon is inserted.

13. A propellant charge according to claim 10 further comprises means defining a hollow core in said form member for inserting an igniter, and an igniter inserted in said hollow core.

14. A propellant charge according to claim 13 further comprises means defining apertures in said form member for providing communication between said hollow core and said spooled strand of propellant material.

15. A propellant charge according to claim 10 wherein said strand of propellant material is extruded propellant material.

16. A propellant charge comprises a form member composed of propellant material and at least one strand of propellant material spooled onto said form member.

17. A propellant charge according to claim 16 further comprises means defining a hollow core in said form member for inserting an igniter, and an igniter inserted in said hollow core.

18. A propellant charge according to claim 17 further comprises means defining apertures in said form member for providing communication between said hollow core and said spooled strand of propellant material.