Vertical drop segmented munitions dispenser

Patent metadata

Field	Value
Publication number	US-9863739-B2
Application number	US-201514861010-A
Country	US
Kind code	B2
Filing date	Sep 22, 2015
Priority date	Sep 22, 2015
Publication date	Jan 9, 2018
Grant date	Jan 9, 2018

Abstract

A munitions dispenser employs a plurality of launch tubes mounted in an array as a segmented dispenser assembly. Each tube in the array is configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture. A frame, mountable to an air vehicle, carries the array of launch tubes. A skin covers the array of launch tubes with the skin and frame with the array configured for nested engagement of multiple segmented assemblies.

First claim

What is claimed is:

1. A munitions dispenser comprising:
a plurality of launch tubes mounted in an array as a segment, each tube in the array configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture;
a frame carrying the array of launch tubes, said frame mountable to an air vehicle; and,
a skin covering the array of launch tubes, said skin and frame with the array configured for nested engagement of multiple additional munitions dispensers as a segmented dispenser assembly, wherein each of the multiple additional munitions dispensers includes a plurality of launch tubes mounted in an additional array as an additional segment, each tube in the additional array configured to carry a selected munition releasably coupled in a cylindrical bore thereof for substantially vertical release through a lower aperture, an additional frame carrying the additional array of launch tubes, said additional frame mountable to an air vehicle, and a skin covering the additional array of launch tubes.

2. The munitions dispenser as defined in claim 1 further comprising at least one sleeve mountable in the cylindrical bore of at least one of the plurality of tubes, said sleeve adapted to closely receive one type of munition available as a selected munition.

3. The munitions dispenser as defined in claim 1 further comprising a retention mechanism adapted to releasably constrain the selected munition in the cylindrical bore.

4. The munitions dispenser as defined in claim 1 wherein the array of launch tubes comprise a plurality of US Common Launch Tubes, tubes sleeved with US Common Launch Tubes, tubes containing sleeves of a diameter accommodating expandable folded wings equipped munitions, un-sleeved tubes or a combination thereof.

5. The munitions dispenser as defined in claim 1 wherein the array of tubes are inclined to a rear of the munitions dispenser to enhance munitions separation.

6. The munitions dispenser as defined in claim 1 further comprising an electronics segment having a frame and skin adapted for nested engagement with at least one segmented dispenser assembly to form a munitions dispenser pod.

7. The munitions dispenser defined in claim 6 wherein the electronics segment comprises a target acquisition sensor and a target designator.

8. The munitions dispenser as define in claim 7 wherein the electronic segment further comprises a processor module and a memory module, said processor module connected to receive input from the target acquisition sensor and provide an output to the target designator; a ballistic computer, a communication module and a power supply, said ballistic computer operable to define timing for ballistic release of munitions carried in the tube array, said communications module adapted to exchange ordnance release timing with the ballistic computer for remote activation, recording, or a combination thereof.

9. The munitions dispenser as defined in claim 2 wherein the selected munition comprises a 120 mm mortar round, a 81 mm mortar round or a winged self-guided munition.

10. A munitions dispenser pod comprising:
at least one segment having
a plurality of launch tubes mounted in an array, each tube in the array configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture;
a frame carrying the array of launch tubes, said frame mountable to an air vehicle;
a skin covering the array of launch tubes, said skin and frame with the array configured for nested engagement of multiple additional segments as an assembly, wherein each additional segment includes a plurality of launch tubes mounted in an additional array, each tube in the additional array configured to carry a selected munition releasably coupled in a cylindrical bore thereof for substantially vertical release through a lower aperture, an additional frame carrying the additional array of launch tubes, said additional frame mountable to an air vehicle, and a skin covering the additional array of launch tubes; and

an electronics segment having a frame and skin adapted for nested engagement with the at least one segment.

11. The munitions dispenser pod as defined in claim 10 wherein the at least one segment comprises a plurality of segments mounted in nested engagement.

12. The munitions dispenser as defined in claim 10 further comprising at least one sleeve mountable in the cylindrical bore of at least one of the plurality of tubes, said sleeve adapted to closely receive one type of munition available as a selected munition.

13. The munitions dispenser as defined in claim 10 further comprising a retention mechanism adapted to releasably constrain the selected munition in the cylindrical bore.

14. The munitions dispenser as defined in claim 10 wherein the array of launch tubes comprise a plurality of US Common Launch Tubes, tubes sleeved with US Common Launch Tubes, tubes containing sleeves of a diameter accommodating expandable folded wings equipped munitions, un-sleeved tubes or a combination thereof.

15. The munitions dispenser as defined in claim 10 wherein the array of tubes are inclined to a rear of the munitions dispenser pod to enhance munitions separation.

16. A method for dispensing munitions comprising:
mounting in a frame a plurality of launch tubes in an array as a segment with or without sleeves to accommodate a desired load of selected munitions of varying sizes, each tube in the array configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture and covering the array of launch tubes with a skin, said skin and frame with the array configured for nested engagement of multiple additional assemblies, wherein each additional assembly includes a plurality of launch tubes mounted in an additional array, each tube in the additional array configured to carry a selected munition releasably coupled in a cylindrical bore thereof for substantially vertical release through a lower aperture, an additional frame carrying the additional array of launch tubes, said additional frame mountable to an air vehicle, and a skin covering the additional array of launch tubes;
releasably coupling the selected munitions into the cylindrical bores of the tubes; and
mounting the frame to a UAV.

17. The method as defined in claim 16 further comprising mounting an electronic segment nested with the segment.

18. The method as defined in claim 17 further comprising:
deploying the UAV to a desired target area using either an on board guidance and navigation systems or a data provided by the electronic segment of the pod;
sensing of targets by a target acquisition sensor;
dispensing munitions by vertical release from the tubes to engage the targets.

19. The method as defined in claim 18 further comprising employing a target designator to illuminate the target for munitions guidance.

20. The method as defined in claim 18 further comprising:
dispensing self-guided munitions by vertical release;
separating any shroud or fairing; and,
deploying wing and control systems on the munition.

Assignees

• Boeing Co

Inventors

• Hester Jr William C

Classifications

• F41G7/2293

  using electromagnetic waves other than radio waves · CPC title

• F41G9/002

  for guiding a craft to a correct firing position (for bombing control F41G9/02) · CPC title

• B64D1/06

  Bomb releasing; Bomb doors · CPC title

• F41G7/346

  using global navigation satellite systems, e.g. GPS, GALILEO, GLONASS · CPC title

• F41F3/065

  Rocket pods, i.e. detachable containers for launching a plurality of rockets · CPC title