Aerial delivery system

• US 8,083,184 B2
• Filed: 06/09/2009
• Issued: 12/27/2011
• Est. Priority Date: 06/10/2008
• Status: Active Grant

• Current Assignee: Roy L. Fox Jr
• Original Assignee: Roy L. Fox Jr
• Inventors: Fox, Roy L. Jr.
• Primary Examiner(s): Dinh, Tien
• Assistant Examiner(s): BENEDIK, JUSTIN M
• Application Number:
  US12/481,356
• Publication Number:
  US 20090302164A1
• Time in Patent Office: 931 Days
• Field of Search: 244/151.R, 244/151.B, 244/151.A, 244/152, 244/138.R, 244/137.3, 102/387, 102/393, 102/489, 89/18.15
• US Class Current: 244/137.3
• CPC Class Codes: B64D 1/08 the articles being load-carrying devices
• CPC Class Codes: B64D 1/12 Releasing
• CPC Class Codes: B64D 17/22 Load suspension

Abstract

An aerial delivery system is configured to allow delivery of one or more releasable items after the system is extracted from an aircraft. One or more linear guidance devices and releasable securing mechanisms allow the aerial delivery system to deploy one or more releasable items at an appropriate time. The one or more releasable items may be deployed simultaneously, or in a staged or staggered fashion. Through use of drag or lift-producing devices, the system may be recovered and reused. The attitude and/or azimuth orientation of the system may be varied prior to, during, and/or after release of a releasable item.

Claims

1. An aerial delivery system, comprising:

a platform extractable from an aircraft via a parachute;

a first linear guidance device coupled to the platform; and

a first releasable securing mechanism,

wherein the first releasable securing mechanism is configured to couple a first releasable item to the first linear guidance device,

wherein the first linear guidance device comprises a monorail configured to permit the release of the first releasable item having all control surfaces extended prior to extraction of the platform from the aircraft, and

wherein, responsive to operation of the first releasable securing mechanism, the first releasable item separates from the platform under the guidance of the first linear guidance device during parachute-controlled descent of the platform through the air.

2. The aerial delivery system of claim 1, wherein the platform is tiltable with respect to a parachute to influence the separation trajectory of the first releasable item.

3. The aerial delivery system of claim 1, wherein the first releasable item is a rocket, and wherein the platform is tilted with respect to a parachute in order to at least partially point the rocket toward a desired target.

4. The aerial delivery system of claim 1, further comprising a plurality of sling attachment fittings.

5. The aerial delivery system of claim 4, wherein the sling attachment fittings are configured to cause the aerial delivery system to exhibit a horizontal attitude when the aerial delivery system is suspended beneath a parachute.

6. The aerial delivery system of claim 4, further comprising a rotation mechanism coupled to a parachute and coupled to the plurality of sling attachment fittings, wherein the rotation mechanism is configured to allow the azimuth of the aerial delivery system with respect to the parachute to be varied.

7. The aerial delivery system of claim 6, wherein the rotation mechanism comprises a lead screw, a nut, and a brake.

8. The aerial delivery system of claim 7, wherein the azimuth of the aerial delivery system with respect to the parachute is varied responsive to the weight of the aerial delivery system exerted on the lead screw.

9. The aerial delivery system of claim 6, wherein the rotation mechanism is configured to be controlled from a remote location.

10. The aerial delivery system of claim 4, further comprising:

a first strap coupled to one of the plurality of sling attachment fittings located near the midpoint of the platform, the first strap having a first length;

a second strap coupled to another of the plurality of sling attachment fittings located near the rear of the platform, the second strap having a second length different from the first length; and

a parachute coupled to the first strap and the second strap, wherein, responsive to inflation of the parachute, the first strap and the second strap cause the platform to achieve a predetermined orientation.

11. The aerial delivery system of claim 10, wherein the predetermined orientation of the platform is an inclined attitude.

12. The aerial delivery system of claim 1, wherein the first releasable securing mechanism is a reefing cutter.

13. The aerial delivery system of claim 1, wherein the first releasable securing mechanism comprises a stored energy spring that imparts a force to the first releasable item to at least partially eject the first releasable item from the aerial delivery system under the guidance of the first linear guidance device.

14. The aerial delivery system of claim 1, further comprising a second linear guidance device coupled to the platform.

15. The aerial delivery system of claim 14, wherein the second linear guidance device is configured to permit the release of a second releasable item having all control surfaces extended prior to extraction of the platform from the aircraft.

16. The aerial delivery system of claim 1, wherein all control surfaces of the first releasable item are non-retractable.

17. The aerial delivery system of claim 1, wherein the first releasable item is a bomb.

18. The aerial delivery system of claim 1, wherein the first releasable item is a missile.

19. The aerial delivery system of claim 1, wherein the first releasable item is piece of ordnance deployable only via the rear cargo door of the aircraft.

20. An aerial delivery system, comprising:

a platform extractable from an aircraft via a parachute;

a linear guidance device coupled to the platform, wherein the linear guidance device is configured as a dovetail;

a releasable securing mechanism for coupling a releasable item to the linear guidance device, wherein the releasable securing mechanism is configured to allow the releasable item to separate from the aerial delivery system during parachute-controlled descent of the aerial delivery system through the air; and

a rotation mechanism coupled to the platform, wherein the rotation mechanism is configured to allow the azimuth of the aerial delivery system with respect to the parachute to be varied during descent of the aerial delivery system through the air.

21. The aerial delivery system of claim 20, wherein the rotation mechanism comprises a lead screw, a nut, and a brake.

22. The aerial delivery system of claim 20, wherein the rotation mechanism is configured to vary the azimuth of the aerial delivery system with respect to the parachute prior to separation of the releasable item from the aerial delivery system.