Temporarily installed aircraft observer door plug, chair, sonotube ejection and control system

• US 8,807,482 B2
• Filed: 10/15/2008
• Issued: 08/19/2014
• Est. Priority Date: 10/15/2007
• Status: Active Grant

• Current Assignee: 1281329 Alberta Ltd.
• Original Assignee: 1281329 Alberta Ltd.
• Inventors: Woodland, Richard, Neyedly, Ross James
• Primary Examiner(s): Lee, Benjamin P
• Application Number:
  US12/734,158
• Publication Number:
  US 20100206988A1
• Time in Patent Office: 2,134 Days
• Field of Search: 244/118.2, 244/137.1, 244/137.4, 244/118.1, 244/129.1, 244/129.5, 244/129.4, 244/129.3, 89/15.4, 89/15.8, 89/15.9, 89/371.6, 89/371.7, 89/372.1, 89/372.2
• US Class Current: 244/129.4
• CPC Class Codes: B64C 1/1407 Doors; surrounding frames
• CPC Class Codes: B64C 1/1484 Windows B64C1/1492 takes precedence
• CPC Class Codes: B64C 1/18 Floors
• CPC Class Codes: B64C 1/20 specially adapted for freight
• CPC Class Codes: B64D 1/02 Dropping, ejecting, or releasing articles jettisonable fuel reservoirs B64D37/12
• CPC Class Codes: B64D 11/00 Passenger or crew accommodation; Flight-deck installations not otherwise provided for
• CPC Class Codes: B64D 11/06 Arrangements of seats, or adaptations or details specially adapted for aircraft seats crew seat constructions for emergency purposes B64D25/04
• CPC Class Codes: B64D 11/0616 with ejection means
• CPC Class Codes: B64D 11/062 Belts or other passenger restraint means for passenger seats
• CPC Class Codes: B64D 7/00 Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft dropping bombs or the like B64D1/00; armaments or mountings therefor per se F41

Abstract

The system and apparatus of the present invention is generally comprised of a non-dedicated, temporarily-installed, aircraft observer bubble door, chair, sonotube ejection system, mission electronics LRU rack and workstation assembly which are affixed to the Air Deployment System (ADS) rails, cargo tie down “D” rings, seat belt restraint ring bolt sockets, and litter bar of a host aircraft, thereby precluding the requirement for dedicated airframe modifications. One embodiment of the present invention also utilizes a multi-axis, articulated, foldable chair temporarily-installed in conjunction with a segmented or one piece pressurized observer bubble door plug and door retraction system. Once installed the subject apparatus can be stowed outboard of the fuselage cargo transit envelope to permit use of the ADS rail system in-flight, without affecting normal air drop operations, crew egress, the flight performance envelope, or emergency procedures of the host aircraft.

Claims

1. A pressurized aircraft observer door plug assembly comprising:

a segmented two-piece observation bubble comprising a protruding upper segment portion and a protruding lower segment portion, wherein;

the upper segment portion comprises a transparent glazing;

the lower segment portion comprises a composite or metal protruding kick panel; and

the segmented two-piece observation bubble is continuous in shape from the upper segment portion through the lower segment portion.

2. The pressurized aircraft door plug assembly of claim 1, wherein the pressurized aircraft door plug assembly is a segmented two-piece pressurized aircraft door plug assembly, further comprising:

a door plug upper panel comprising the segmented two-piece observation bubble; and

a door plug lower panel.

3. The pressurized aircraft door plug assembly of claim 2, further comprising two or more interlocking latches that are operable to:

join the door plug lower panel and the door plug upper panel; and

disengage the door plug lower panel from the door plug upper panel.

4. The pressurized aircraft door plug assembly of claim 2, further comprising:

a tube port that provides an orifice through the door plug upper panel; and

a valve interfaced with the tube port that is operable between an open position and a closed position.

5. The pressurized aircraft door plug assembly of claim 4, further comprising a sonotube launch system that is operable to interface with the valve.

6. The pressurized aircraft observer door plug assembly of claim 1, further comprising:

one or more upper rail support struts operable to interface with one or more door retraction rail guides of an aircraft.

7. The pressurized aircraft observer door plug assembly of claim 1, wherein a lower part of the pressurized aircraft observer door plug assembly is operable to interface with one or more of:

an air deployment system rail of an aircraft;

or

one or more adaptive floor plates operable to interface with a floor of an aircraft.

8. The pressurized aircraft observer door plug assembly of claim 1, further comprising:

an observer chair assembly comprising;

a stanchion post operable to interface with a floor of an aircraft;

a telescoping pivot arm operable to interface with the stanchion post; and

an observer chair operable to interface with the telescoping pivot arm;

wherein the observer chair assembly is operable to move the observer chair into the segmented two-piece observation bubble.

9. A segmented two-piece pressurized aircraft door plug assembly comprising:

a door plug upper panel; and

a door plug lower panel which is contoured and indented about its lower proximity to accommodate a pressurized seal around the periphery of an articulated- or fixed-position payload strut which transits from the interior to the exterior of an aircraft.

10. The segmented two-piece pressurized aircraft door plug assembly of claim 9, further comprising two or more interlocking latches that are operable to:

join the door plug lower panel and the door plug upper panel; and

disengage the door plug lower panel from the door plug upper panel.

11. The segmented two-piece pressurized aircraft door plug assembly of claim 9, further comprising:

one or more upper rail support struts operable to interface with one or more door retraction rail guides of an aircraft.

12. The segmented two-piece pressurized aircraft door plug assembly of claim 9, wherein a lower part of the pressurized aircraft observer door plug assembly is operable to interface with one or more of:

an air deployment system rail of an aircraft;

or

one or more adaptive floor plates operable to interface with as a floor of the aircraft.

13. The segmented two-piece pressurized aircraft door plug assembly of claim 9, further comprising:

a tube port that provides an orifice through the door plug upper panel; and

a valve interfaced with the tube port that is operable between an open position and a closed position.

14. The segmented two-piece pressurized aircraft door plug assembly of claim 13, further comprising a sonotube launch system that is operable to interface with the valve.

15. A segmented two-piece pressurized aircraft door plug assembly comprising:

a door plug upper panel comprising a segmented two-piece observation bubble window assembly comprising an upper segment portion and a lower segment portion, wherein;

the upper segment portion comprises a transparent glazing; and

the lower segment portion comprises a composite or metal protruding kick panel; and

a door plug lower panel which is contoured and indented about its lower proximity to accommodate a pressurized seal around the periphery of an articulated- or fixed-position payload strut which transits from the interior to the exterior of an aircraft.

16. The segmented two-piece pressurized aircraft door plug assembly of claim 15, further comprising two or more interlocking latches that are operable to:

join the door plug lower panel and the door plug upper panel; and

disengage the door plug lower panel from the door plug upper panel.

17. The segmented two-piece pressurized aircraft door plug assembly of claim 15, further comprising:

one or more upper rail support struts operable to interface with one or more door retraction rail guides of an aircraft.

18. The segmented two-piece pressurized aircraft door plug assembly of claim 15, wherein a lower part of the pressurized aircraft observer door plug assembly is operable to interface with one or more of:

an air deployment system rail of an aircraft;

or

one or more adaptive floor plates operable to interface with as a floor of the aircraft.

19. The segmented two-piece pressurized aircraft door plug assembly of claim 15, further comprising:

a tube port that provides an orifice through the door plug upper panel;

a valve interfaced with the tube port that is operable between an open position and a closed position; and

a sonotube launch system that is operable to interface with the valve.

20. The segmented two-piece pressurized aircraft door plug assembly of claim 15, further comprising:

an observer chair assembly comprising;

a stanchion post operable to interface with a floor of an aircraft;

a telescoping pivot arm operable to interface with the stanchion post; and

an observer chair operable to interface with the telescoping pivot arm;

wherein the observer chair assembly is operable to move the observer chair into the segmented two-piece observation bubble window assembly.