System and method for enhancing the payload capacity, carriage efficiency, and adaptive flexibility of external stores mounted on an aerial vehicle

• US 7,610,841 B2
• Filed: 11/21/2002
• Issued: 11/03/2009
• Est. Priority Date: 05/21/2002
• Status: Expired due to Fees

• Current Assignee: Nir Padan
• Original Assignee: Nir Padan
• Inventors: Padan, Nir
• Primary Examiner(s): Chambers; Troy
• Application Number:
  US10/514,757
• Publication Number:
  US 20050204910A1
• Time in Patent Office: 2,539 Days
• Field of Search: 89/18.13, 89/18, 89/18.14, 89/18.15, 89/18.16, 244/118.1, 244/119, 244/136, 244/137.1, 244/137.4
• US Class Current: 89/1.815
• CPC Class Codes: B64D 1/04 the articles being explosive, e.g. bombs arming or setting bomb fuzes F42C
• CPC Class Codes: B64D 37/12 jettisonable
• CPC Class Codes: F41F 3/065 Rocket pods, i.e. detachable containers for launching a plurality of rockets
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

A system and method for the conversion of fuel tanks, detachably mountable on the exterior of an aerial vehicle, into high volume, high capacity, diverse functionality and aerodynamically efficient airborne stores is disclosed. A conventional external fuel drop tank is modified such that the exterior shape of the tank is substantially retained while the interior of the tank is suitable restructured to allow for the introduction of diverse airborne stores, associated airborne store mounting means, control and monitoring means and support means therein, which replace the fuel store. The airborne store is suitably interfaced to the stores control and management system of the aerial vehicle. The airborne store is integrated into a new external stores configuration The enhanced airborne store will have aerodynamic characteristics substantially similar to the original external fuel tank while its payload capacity is substantially improved.

Claims

1. A system for mounting a load on an aerial vehicle, the system comprising:

an aerodynamically shaped structure mounted on the exterior of an aerial vehicle;

said aerodynamically shaped structure substantially surrounds at least one airborne store;

interior airborne store mounting means attached to the internal surface of the aerodynamically shaped enclosure to provide stability to the at least one airborne store;

airborne store operation control means linked to the aerodynamically shaped structure to monitor and control the operation of the at least one airborne store;

airborne store operation support means to provide for the release of the at least one airborne store during flight responsive to instructions by said airborne store operation control means; and

wherein said aerodynamically shaped structure is shaped the same as a fuel tank designed for use with the aerial vehicle and is mounted on the exterior of the aerial vehicle in the position in which a fuel tank of the same shape would be placed.

2. The system according to claim 1 wherein the aerodynamically shaped structure is a modified fuel tank attachable to the exterior of aerial vehicle.

3. The system according to claim 2 wherein the modified fuel tank is structurally strengthened up to maintain its aerodynamic shape and characteristics during flight, to manage loads associated with the suspension, storage, delivery and release of the at least one airborne store mounting means, the at least one airborne store control means, the at least one airborne store support means and the at least one airborne store.

4. The system according to claim 2 wherein the modified fuel tank is of modular construction.

5. The system according to claim 2 wherein the modified fuel tank is a standard external fuel drop tank.

6. The system according to claim 5 wherein the standard external fuel drop tank is a 370-gallon fuel tank.

7. The system according to claim 1 wherein the at least one airborne store mounting means is an expendable electronic counter measure magazine.

8. The system according to claim 1 wherein the at last one airborne store mounting means is a multiple missile launcher.

9. The system according to claim 1 wherein the at least one airborne store support means is a multiple bomb ejector.

10. The system according to claim 1 wherein the at least one airborne store mounting means is multiple miniature aerial vehicle launcher.

11. The system according to claim 1 wherein the at least one airborne store mounting means is a multiple micro-satellite launcher.

12. The system according Co claim 1 wherein the at least one airborne store operation control means comprises communication media to interconnect the at least one airborne store to the stores management and control system of the aerial vehicle.

13. The system according to claim 1 where the at least one airborne store operation support means comprises the elements of:

at least one airborne store loading and reloading access door;

at least one airborne store release door.

14. The system according to claim 1 wherein the at least one airborne store is an expendable electronic counter measure device.

15. The system according to claim 14 wherein the expendable electronic counter measure device is chaff.

16. The system according to claim 1 wherein the at least one airborne store is an aerodynamic missile.

17. The system according to claim 1 wherein the at least one airborne store is an aerial bomb.

18. The system according to claim 1 wherein the at least one airborne store is a miniature aerial vehicle.

19. The system according to claim 1 wherein the at least one airborne store is a micro-satellite.

20. The system according to claim 1 wherein the at least one airborne store is a multi-payload airborne store comprising the elements of:

an expendable electronic counter measure dispenser; and

a tactical reconnaissance assembly.

21. The system according to claim 1 wherein the at least one airborne store is a missile.

22. The system according to claim 1 wherein the aerodynamically shaped structure comprises a chaff or Flare dispenser pod.

23. The system according to claim 1 wherein the aerodynamically shaped structure comprises a missile launcher pod.

24. The system according to claim 1 further comprises secondary control, monitoring, and emergency release means.