RAPIDLY RECONFIGURABLE PALLETIZED MISSION EQUIPMENT MOUNTING SYSTEMS AND METHODS

• US 20190308725A1
• Filed: 04/05/2018
• Published: 10/10/2019
• Est. Priority Date: 04/05/2018
• Status: Active Application

• Current Assignee: Bell Helicopter Textron Incorporated (Textron Inc)
• Original Assignee: Bell Helicopter Textron Incorporated (Textron Inc)
• Inventors: Sherman, Jimmy Dale, Tynes, Mark Gibson, Robertson, Eric John, May, Carl Alan, Willnow, Randall Thompson
• Application Number:
  US15/946,598
• Publication Number:
  US 20190308725A1
• Time in Patent Office: Days
• CPC Class Codes: B64D 9/003 Devices for retaining pallets or freight containers securing freight containers on vehicles B60P7/00

Abstract

Rapidly reconfigurable palletized mission equipment mounting systems and methods employ a plurality of tracks or rails installed in an aircraft fuselage. Mission equipment is secured on a pallet. The pallet is a rapidly reconfigurable mission equipment mounting pallet body defining a plurality of orifices sized to accept releasable anchor hardware, positioned to align with the tracks or rails installed in the aircraft and readily releasable anchors disposed in the orifices and configured to rapidly mount to, and rapidly dismount from, the tracks or rails. The pallet with the mission package(s) secured thereto is transferred into the aircraft and mounted the pallet in the aircraft on the tracks or rails, via the readily releasable anchors, for rapidly dismounting from the tracks or rails.

Claims

1. A rapidly reconfigurable palletized mission equipment mounting method comprising:

installing a plurality of tracks or rails in an aircraft fuselage;

securing at least one mission package on a pallet outside the aircraft;

transferring the pallet with the at least one mission package secured thereto, into the aircraft; and

mounting the pallet in the aircraft on the tracks or rails, via readily releasable anchors positioned in the pallet to align with the tracks or rails installed in the aircraft, for rapidly dismounting from the tracks or rails.

2. The rapidly reconfigurable mission equipment mounting method of claim 1, wherein the tracks or rails are installed in or on a flat interior surface of a fuselage of the aircraft and the pallet is mounted via the readily releasable anchors to the interior surface, inside the aircraft.

3. The rapidly reconfigurable mission equipment mounting method of claim 1, wherein the tracks or rails are installed in or on a deck of a fuselage of the aircraft and the pallet is mounted via the readily releasable anchors to the deck, inside the aircraft.

4. The rapidly reconfigurable mission equipment mounting method of claim 1, wherein the pallet further comprises a pallet body that has a plurality of orifices accepting the readily releasable anchors, the orifices positioned to align with the tracks or rails installed in the aircraft.

5. The rapidly reconfigurable mission equipment mounting method of claim 1, wherein the one or more mission packages comprises at least one avionics package and the rapidly reconfigurable mission equipment mounting method further comprises connecting electrical harnesses of the aircraft to the at least one avionics package, following mounting of the pallet via the readily releasable anchors in the aircraft.

6. The rapidly reconfigurable mission equipment mounting method of claim 1, further comprising adjusting a center of gravity of the aircraft, wherein adjusting the center of gravity of the aircraft comprises:

loosening the readily releasable anchors;

moving the pallet along the rails, repositioning the aircraft center of gravity; and

resecuring the readily releasable anchors.

7. The rapidly reconfigurable mission equipment mounting method of claim 1, further comprising replacing the one or more mission packages with one or more replacement mission packages, wherein replacing the one or more mission packages with one or more replacement mission packages comprises:

dismounting one or more current mission packages from the pallet mounting the current mission packages;

removing dismounted current mission packages from the aircraft;

transferring one or more replacement mission packages into the aircraft; and

mounting the one or more replacement mission packages on the pallet, in the aircraft.

8. The rapidly reconfigurable mission equipment mounting method of claim 1, further comprising replacing the one or more mission packages with one or more replacement mission packages, wherein replacing the one or more mission packages with the one or more replacement mission packages comprises:

dismounting the pallet mounting current mission packages from the tracks or rails by releasing the readily releasable anchors;

removing the pallet mounting current mission packages from the aircraft;

transferring a pallet mounting the one or more replacement mission packages into the aircraft; and

mounting the pallet mounting the one or more replacement mission packages via the readily releasable anchors, in the aircraft on the tracks or rails, for rapid dismount from the tracks or rails.

9. A rapidly reconfigurable mission equipment mounting method comprising:

installing a plurality of tracks or rails in an aircraft fuselage;

mounting a pallet in the aircraft on the tracks or rails, via readily releasable anchors positioned in the pallet to align with the tracks or rails installed in the aircraft, for rapidly dismounting from the tracks or rails;

transferring one or more mission packages into the aircraft; and

securing the at least one mission packages on the pallet, inside the aircraft.

10. The rapidly reconfigurable mission equipment mounting method of claim 9, wherein the tracks or rails are installed in or on a flat interior surface of a fuselage of the aircraft and the pallet is mounted via the readily releasable anchors to the interior surface, inside the aircraft.

11. The rapidly reconfigurable mission equipment mounting method of claim 9, wherein the tracks or rails are installed in or on a deck of a fuselage of the aircraft and the pallet is mounted via the readily releasable anchors to the deck, inside the aircraft.

12. The rapidly reconfigurable mission equipment mounting method of claim 9, wherein the pallet further comprises a pallet body that has a plurality of orifices accepting the readily releasable anchors, the orifices positioned to align with the tracks or rails installed in the aircraft.

13. The rapidly reconfigurable mission equipment mounting method of claim 9, wherein the one or more mission packages comprises at least one avionics package and the rapidly reconfigurable mission equipment mounting method further comprises connecting electrical harnesses of the aircraft to the at least one avionics package, following mounting of at least one avionics package on the pallet in the aircraft.

14. The rapidly reconfigurable mission equipment mounting method of claim 9, further comprising adjusting a center of gravity of the aircraft, wherein adjusting the center of gravity of the aircraft comprises:

loosening the readily releasable anchors;

moving the pallet along the rails, repositioning the aircraft center of gravity; and

resecuring the readily releasable anchors.

15. The rapidly reconfigurable mission equipment mounting method of claim 9, further comprising replacing the one or more mission packages with one or more replacement mission packages, wherein replacing the one or more mission packages with one or more replacement mission packages comprises:

dismounting one or more current mission packages from the pallet mounting the current mission packages;

removing dismounted current mission packages from the aircraft;

transferring one or more replacement mission packages into the aircraft; and

mounting the one or more replacement mission packages on the pallet, in the aircraft.

16. The rapidly reconfigurable mission equipment mounting method of claim 9, further comprising replacing the one or more mission packages with one or more replacement mission packages, wherein replacing the one or more mission packages with the one or more replacement mission packages comprises:

dismounting the pallet mounting current mission packages from the tracks or rails by releasing the readily releasable anchors;

removing the pallet mounting current mission packages from the aircraft;

transferring a pallet mounting the one or more replacement mission packages into the aircraft; and

mounting the pallet mounting the one or more replacement mission packages via the readily releasable anchors, in the aircraft on the tracks or rails, for rapid dismount from the tracks or rails.

17. A rapidly reconfigurable palletized mission equipment mounting system comprising:

a plurality of tracks or rails installed in an aircraft fuselage;

a mission equipment mounting pallet, mounting at least one mission package, the mission equipment mounting pallet comprising a rapidly reconfigurable mission equipment mounting pallet body defining a plurality of orifices sized to accept releasable anchor hardware and positioned to align with the tracks or rails installed in the aircraft; and

readily releasable anchors disposed in the orifices and configured to rapidly mount to, and rapidly dismount from, the tracks or rails.

18. The rapidly reconfigurable mission equipment mounting system of claim 17, wherein the tracks or rails are installed in or on an interior flat surface of a fuselage of the aircraft.

19. The rapidly reconfigurable mission equipment mounting system of claim 17, wherein the tracks or rails are installed in or on a deck of a fuselage of the aircraft.

20. The rapidly reconfigurable mission equipment mounting system of claim 17, wherein the pallet body comprises a lightweight honeycomb core bonded panel.

21. The rapidly reconfigurable mission equipment mounting system of claim 17, wherein the orifices are each pallet through-holes that extend generally perpendicular to a mission equipment mounting surface of the pallet body, sized to accept and retain the readily releasable anchors.