System and method for affixing gateboxes to an aircraft

• US 10,196,145 B2
• Filed: 10/28/2013
• Issued: 02/05/2019
• Est. Priority Date: 04/01/2011
• Status: Active Grant

• Current Assignee: Texas Transland, LLC
• Original Assignee: Texas Transland, LLC
• Inventors: Thompson, Larry D.
• Primary Examiner(s): Dinh, Tien Q
• Assistant Examiner(s): Fabula, Michael A.
• Application Number:
  US14/064,561
• Publication Number:
  US 20140048653A1
• Time in Patent Office: 1,926 Days
• CPC Class Codes: B64C 39/02 characterised by special use
• CPC Class Codes: B64C 7/00 Structures or fairings not otherwise provided for
• CPC Class Codes: B64D 1/00 Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight with respect to weapon sights devices F41G takes precedence, parachutes per se B64D17/00; ejectable seats B64D25/10; ejectable capsules B64D25/12; refuelling during flight B64D39/00; launching apparatus for projecting projectiles or missiles F41F1/00, F41F7/00; rocket or torpedo launchers F41F3/00
• CPC Class Codes: B64D 1/16 Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting jettisoning fuel B64D37/26
• CPC Class Codes: B64D 1/18 by spraying, e.g. insecticides spraying apparatus per se B05B
• CPC Class Codes: B64F 5/50 Handling or transporting aircraft components
• CPC Class Codes: B66F 5/00 Mobile jacks of the garage type mounted on wheels or rollers
• CPC Class Codes: Y10T 29/49826 Assembling or joining

Abstract

A system for affixing a gatebox to an aircraft includes a first type of gatebox operable to release material from an aircraft, a second type of gatebox operable to release material from the aircraft, a frame coupled to the aircraft operable to receive a selected one of the first type of gatebox and the second type of gatebox; and a plurality of fastenings operable to secure the selected one of the first type of gatebox and the second type of gatebox to the frame.

Claims

1. An aircraft gatebox affixing system, comprising:

a first gatebox configured to provide a firefighting functionality and to release a first material selected from one of water and a fire retardant while affixed to an aircraft;

a second gatebox configured to provide agricultural functionality and to release a second material selected from one of a fertilizer, an insecticide, an herbicide, and seeds while affixed to an aircraft, the first gatebox and the second gatebox being of different constructions;

a frame configured to affix to an aircraft and interchangeably couple to a selected one of the first gatebox and the second gatebox;

a plurality of fastenings configured to interchangeably couple the selected one of the first gatebox and the second gatebox to the frame; and

a seal configured to create a barrier between the frame and the selected one of the first gatebox and the second gatebox, wherein the seal is recessed within the frame to receive a compression structure from the selected one of the first gatebox and second gatebox, the recessed seal is operable to self-align the selected one of the first gatebox and second gatebox when coupled to the frame.

2. The system of claim 1, wherein the seal is a compressible seal and is coupled to one or more from the set comprising:

the first gatebox, the second gatebox, and the frame.

3. The system of claim 2, further comprising:

a seal housing structure adapted to house the compressible seal, the seal housing comprising a flange extending from the frame; and

a seal compression structure adapted to mate to the seal housing structure, wherein the plurality of fastenings secure the selected one of the first gatebox and the second gatebox to the frame and the seal compression structure mates with the seal housing structure and compresses the compressible seal against the seal housing structure.

4. The system of claim 1, wherein the seal has a cross sectional shape of one from a set comprising:

X-shaped, O-shaped, and U-shaped.

5. The system of claim 1, further comprising a cart comprising:

a gatebox support configured to secure a selected one of the first gatebox and the second gatebox; and

a lift configured to vertically lift the support.

6. The system of claim 1, wherein the plurality of fastenings are over-center latches.

7. The system of claim 1, further comprising a controller communicatively coupled to at least one of the aircraft, the selected one of the first gatebox and the second gatebox, and a sensor, wherein the controller is configured to receive signals to control the selected one of the first gatebox and the second gatebox.

8. The system of claim 1, further comprising a fairing configured to couple to at least one of the aircraft, the frame, and the selected one of the first gatebox and the second gatebox, and further configured to change airflow around the selected one of the first gatebox and the second gatebox.

9. An aircraft gatebox affixing system, comprising:

a frame affixable to an aircraft, wherein the frame is configured to receive a first gatebox configured to provide a firefighting functionality and to release a first material selected from one of water and a fire retardant and a second gatebox configured to provide agricultural functionality and to release a second material selected from one of a fertilizer, an insecticide, an herbicide, and seeds, the first gatebox and the second gatebox being of different constructions, and the frame is configured to interchangeably couple to a selected one of the first gatebox and the second gatebox;

a plurality of fastenings configured to couple the selected one of the first gatebox and the second gatebox to the frame; and

a seal configured to create a barrier between the frame and a selected one of the first gatebox and the second gatebox, wherein the seal is recessed within the frame to receive a compression structure from the selected one of the first gatebox and second gatebox, the recessed seal is operable to self-align the selected one of the first gatebox and second gatebox when coupling to the frame.

10. The apparatus of claim 9, further comprising:

a first gatebox configured to release a first material while affixed to an aircraft;

a second gatebox configured to release a second material while affixed to an aircraft, and

wherein the seal is coupled to one or more from a set comprising;

the first gatebox, the second gatebox, and the frame.

11. The apparatus of claim 10, further comprising:

a seal housing structure adapted to house the seal, the seal housing comprising a flange extending from the frame, and wherein the seal is a compressible seal; and

a seal compression structure adapted to mate to the seal housing structure, wherein the plurality of fastenings secure the selected one of the first gatebox and the second gatebox to the frame and the seal compression structure mates with the seal housing structure and compresses the compressible seal against the seal housing structure.

12. The apparatus of claim 9, wherein the plurality of fastenings are over-center latches.

13. The apparatus of claim 9, wherein the seal has a cross sectional shape of one from a set comprising:

X-shaped, O-shaped, and U-shaped.

14. An aircraft gatebox affixing method, comprising:

affixing to an aircraft a frame configured to couple to a first aircraft gatebox configured to provide a firefighting functionality and to release a first material selected from one of water and a fire retardant and a second aircraft gatebox configured to provide agricultural functionality and to release a second material selected from one of a fertilizer, an insecticide, an herbicide, and seeds, the first gatebox and the second gatebox being of different constructions, and wherein the frame is configured to interchangeably couple to a selected one of the first gatebox and the second gatebox, wherein one or more of the frame, the first gatebox, and the second gatebox include a recessed seal configured to create a self-aligned barrier between the frame and the selected one of the first gatebox and the second gatebox;

coupling to the frame the first gatebox by engaging one or more of a plurality of fastenings;

removing from the frame the first gatebox by disengaging one or more of the plurality of fastenings; and

coupling to the frame the second gatebox by engaging one or more of the plurality of fastenings.

15. The method of claim 14, wherein the seal is a compressible seal and is coupled to one or more from the set comprising:

the first gatebox, the second gatebox, and the frame.

16. The method of claim 15, wherein one or more of the frame and the selected one of the first gatebox and the second gatebox include:

a seal housing structure adapted to house the compressible seal, the seal housing comprising a flange extending from the frame; and

a seal compression structure adapted to mate to the seal housing structure, wherein the plurality of fastenings secure the selected one of the first gatebox and the second gatebox to the frame and the seal compression structure mates with the seal housing structure and compresses the compressible seal against the seal housing structure.

17. The method of claim 14, wherein the plurality of fastenings are over-center latches.

18. The method of claim 14, wherein the seal has a cross sectional shape of one from a set comprising:

X-shaped, O-shaped, and U-shaped.

19. The method of claim 14, further comprising communicatively coupling a controller to at least one of the aircraft, the selected one of the first gatebox and the second gatebox, and a sensor, wherein the controller is configured to receive signals to control the selected one of the first gatebox and the second gatebox.

20. The method of claim 14, further comprising coupling a fairing configured to change airflow around the selected one of the first gatebox and the second gatebox coupled to the aircraft to at least one of the aircraft, the frame, and the selected one of the first gatebox and the second gatebox.