Integrated spacing and orientation control system

• US 5,524,524 A
• Filed: 10/24/1994
• Issued: 06/11/1996
• Est. Priority Date: 10/24/1994
• Status: Expired due to Term

• Current Assignee: Tracor Aerospace, Inc.
• Original Assignee: Tracor Aerospace, Inc.
• Inventors: McDuffie, Philip L., Coleman, Edward R., Kelley, Mark J., Schorr, David J., Richards, Les H.
• Primary Examiner(s): Jordan, Charles T.
• Assistant Examiner(s): Wesson, Theresa M.
• Application Number:
  US08/328,255
• Time in Patent Office: 596 Days
• Field of Search: 89/1.13, 89/1.11, 89/1.1, 89/1.15, 102/402, 102/403, 102/302, 102/310, 244/570, 244/239, 206/485
• US Class Current: 89/1.13
• CPC Class Codes: F21S 2/00 Systems of lighting devices, not provided for in main groups F21S4/00 - F21S10/00 or F21S19/00, e.g. of modular construction
• CPC Class Codes: F41H 11/12 Means for clearing land minefields; Systems specially adapted for detection of landmines
• CPC Class Codes: F41H 11/14 Explosive line charges, e.g. snakes
• CPC Class Codes: H01Q 15/147 provided with means for controlling or monitoring the shape of the reflecting surface for scanning H01Q3/01; aerials or aerial systems providing multiple beamwidths H01Q25/002
• CPC Class Codes: H01Q 15/20 Collapsible reflectors

Abstract

An integrated spacing and orientation control system is provided for carrying an array of objects and maintaining a predetermined orientation of the objects and a predetermined spacing between objects. In a presently preferred application, the spacing and orientation system carries an array of anti-mine munitions for clearing a path through a minefield. The invention deploys the anti-mine munitions in a downwardly pointed orientation with proper spacing between munitions, even when the array of munitions is deployed using rocket motors.

Claims

1. A remotely deployable munition array for destroying mines in a minefield, comprising:

an array of jet-type munitions each having a top end and a bottom end, each munition being designed to fire an explosive jet from its bottom end when detonated;

a generally planar network of upper flexible strapping members connected to the top ends of the munitions; and

a generally planar network of lower flexible strapping members connected to the bottom ends of the munitions;

the upper strapping members being fastened to the lower strapping members at locations between the munitions.

2. The array of claim 1, wherein the munitions are arrayed in a generally square pattern.

3. The array of claim 1, wherein the munitions are arrayed in a generally triangular pattern.

4. The array of claim 1, further comprising detonating cord operatively coupled to each of the munitions in the array.

5. The array of claim 1, wherein the strapping members comprise plastic ribbon.

6. The array of claim 1, further comprising detonating conductors integrally formed with the top strapping member.

7. The array of claim 1, wherein the strapping members comprise tubular braided sheathing.

8. An integrated spacing and orientation control system for supporting an array of objects in a preselected arrangement and orientation, each object having a top and a bottom, the control system comprising:

objects, said objects further defined as munitions;

upper means for interconnecting the tops of the objects so as to restrict lateral movement of said tops;

lower means for interconnecting the bottoms of the objects so as to restrict lateral movement of said bottoms;

the upper means and lower means being joined to one another at spaced locations between the objects.

9. The system of claim 8, wherein the upper means and the lower means comprise flexible sheeting.

10. The system of claim 8, wherein the upper means and the lower means comprise flexible strapping.

11. A remotely deployable munition array for destroying mines comprising:

an array of jet-type munitions disposed in a preselected pattern and having preselected spacing and orientation for deployment over a mine field; and

means for supporting the munitions during transport and deployment such that the preselected spacing and orientation of the munitions is attained after deployment;

wherein the supporting means is coupled to a top end of each munition and to a bottom end of each munition so as to control the orientation of the munitions.

12. The array of claim 11, wherein the supporting means comprises means for distributing detonating energy to each munition.

13. The remotely deployable munition array of claim 11, wherein the supporting means comprises detonating cord.