Cradle assembly for supporting a door of an aircraft to facilitate servicing the door, and arrangements and methods for the same

Patent metadata

Field	Value
Publication number	US-10946985-B2
Application number	US-201815985566-A
Country	US
Kind code	B2
Filing date	May 21, 2018
Priority date	May 21, 2018
Publication date	Mar 16, 2021
Grant date	Mar 16, 2021

Abstract

Cradle assemblies for supporting a door of an aircraft to facilitate servicing the door, and arrangements and methods for the same are provided. In one example, a cradle assembly includes a base and a cradle support subassembly pivotably coupled to the base. The cradle support subassembly is configured to support an outer section of the door.

First claim

What is claimed is:

1. A cradle assembly for supporting a door of an aircraft to facilitate servicing the door, the cradle assembly comprising:
a base comprising a base plate; and
a cradle support subassembly pivotably coupled to the base above the base plate and configured to support an outer section of the door, the cradle support subassembly comprising:
a first pair of arms that are spaced apart from each other and that extend in a first direction;
a second pair of arms that are spaced apart from each other and that extend in a second direction that is at an angle to the first direction; and
a gusseted skin coupled to the first and second pair of arms, and wherein the gusseted skin is operatively coupled to the base to allow the cradle support subassembly to pivot relative to the base.

2. The cradle assembly of claim 1 , wherein the angle is from about 100° to about 150°.

3. The cradle assembly of claim 1 , wherein the cradle support subassembly comprises:
a first plurality of rollers extending between and rotationally coupled to the first pair of arms; and
a second plurality of rollers extending between and rotationally coupled to the second pair of arms, and wherein the first and second plurality of rollers are configured to support outer sections of the door.

4. The cradle assembly of claim 3 , wherein the first plurality of rollers are substantially parallel to and spaced apart from each other and the second plurality of rollers are substantially parallel to and spaced apart from each other.

5. The cradle assembly of claim 3 , wherein each of the first plurality of rollers and the second plurality of rollers comprise an elastomeric material for interfacing with the outer sections of the door.

6. The cradle assembly of claim 3 , wherein the cradle support subassembly comprises:
a first brace extending between and coupled to the first pair of arms; and
a second brace extending between and coupled to the second pair of arms.

7. The cradle assembly of claim 6 , wherein the cradle support subassembly comprises:
a first cross-brace extending between and coupled to first end sections of the first and second braces; and
a second cross-brace extending between and coupled to second end sections of the first and second braces.

8. The cradle assembly of claim 7 , wherein the first and second cross-braces are spaced apart from and substantially parallel to each other.

9. The cradle assembly of claim 6 , wherein the first brace is substantially parallel with the first plurality of rollers, and the second brace is substantially parallel with the second plurality of rollers.

10. The cradle assembly of claim 1 , further comprises a rod, wherein the gusseted skin comprises a first gusseted sidewall and a second gusseted sidewall that are spaced apart from each other and that are operatively coupled to the rod such that the cradle support subassembly rotates about the rod, wherein the base plate has a first section disposed outboard of the first gusseted sidewall and a second section disposed outboard of the second gusseted sidewall, and wherein the base further comprises:
a first pivot rod holder extending generally upward from the first section of the base plate; and
a second pivot rod holder extending generally upward from the second section of the base plate, wherein the first and second pivot rod holders are operatively coupled to the rod to support the rod above the base plate and allow the cradle support subassembly to pivot relative to the base above the base plate.

11. A cradle assembly for supporting a door of an aircraft to facilitate servicing the door, the cradle assembly comprising:
a base; and
a cradle support subassembly pivotably coupled to the base and configured to support an outer section of the door, wherein the cradle support subassembly comprises:
a first pair of arms that are spaced apart from each other and that extend in a first direction; and
a second pair of arms that are spaced apart from each other and that extend in a second direction at an angle to the first direction, wherein the cradle support subassembly comprises:
a first plurality of rollers extending between and rotationally coupled to the first pair of arms; and
a second plurality of rollers extending between and rotationally coupled to the second pair of arms, wherein the first and second plurality of rollers are configured to support outer sections of the door, and wherein the cradle support subassembly comprises:
a gusseted skin coupled to and at least partially surrounding proximal end sections of the first and second pair of arms, and wherein the first and second plurality of rollers are disposed distally from the gusseted skin.

12. The cradle assembly of claim 11 , further comprising a rod that pivotally couples the cradle support subassembly to the base.

13. The cradle assembly of claim 12 , wherein the gusseted skin comprises a first gusseted sidewall and a second gusseted sidewall that is spaced apart from the first gusseted sidewall, and wherein the first and second gusseted sidewalls are operatively coupled to the rod such that the cradle support subassembly rotates about the rod.

14. The cradle assembly of claim 13 , wherein the base comprises:
a base plate having a first section disposed outboard of the first gusseted sidewall and a second section disposed outboard of the second gusseted sidewall;
a first pivot rod holder extending generally upward from the first section of the base plate; and
a second pivot rod holder extending generally upward from the second section of the base plate, wherein the first and second pivot rod holders are operatively coupled to the rod to support the rod above the base plate and allow the cradle support subassembly to pivot relative to the base.

Assignees

• Gulfstream Aerospace Corp

Inventors

• Leonard Patrick
• Shearouse Derek

Classifications

• B62B3/108 Primary

  the objects being plates, doors, panels, or the like · CPC title

• B64F5/40

  Maintaining or repairing aircraft · CPC title

• B64C1/1407

  Doors; surrounding frames · CPC title

• B62B2202/90

  Vehicles · CPC title

• B64F5/50 Primary

  Handling or transporting aircraft components · CPC title