Cargo doors for payload bay having internal payload extension and retraction mechanism

Patent metadata

Field	Value
Publication number	US-11401035-B2
Application number	US-202016841043-A
Country	US
Kind code	B2
Filing date	Apr 6, 2020
Priority date	Apr 6, 2020
Publication date	Aug 2, 2022
Grant date	Aug 2, 2022

Abstract

A system is described and includes a rack for carrying payload disposed in payload bay; a rack extension assembly for affecting linear displacement of the rack between a first position in which the rack is stowed within the payload bay and a second position in which the rack is supported outside the payload bay; a payload actuator system for selectively causing the rack extension assembly to move the rack between the first and second positions; a payload bay door; and a door actuator system for selectively opening and closing the payload bay door.

First claim

What is claimed is:

1. A system comprising:
a rack for carrying a payload disposed in a payload bay of a vehicle;
a rack extension assembly for affecting linear translation of the rack between a first position in which the rack is stowed within the payload bay and a second position in which the rack is supported outside the payload bay;
a payload actuator system for selectively causing the rack extension assembly to move the rack between the first and second positions while the vehicle is in motion;
a payload bay door in at least one of a port side of the vehicle and a starboard side of the vehicle; and
a door actuator system for selectively opening and closing the payload bay door.

2. The system of claim 1 , wherein the payload bay door comprises a single door panel and the door actuator system comprises a forward actuator mechanism comprising upper and lower links for connecting a forward side of the single door panel to a forward wall of the payload bay and an aft actuator mechanism comprising upper and lower links for connecting an aft side of the single door panel to an aft wall of the payload bay.

3. The system of claim 2 , wherein a first end of each of the upper links is rotatably connected to a respective upper link mount provided in the respective wall of the payload bay and a second end of each of the upper links is connected to respective attachment fitting provided in the respective side of the single panel door and wherein a first end of each of the lower links is rotatably connected to a respective lower link mount provided in the respective wall of the payload bay and a second end of each of the lower links is connected to the respective attachment fitting.

4. The system of claim 3 further comprising a track provided in each of the payload bay walls for engaging a respective one of the lower links for providing fore-aft restraint for the single panel door.

5. The system of claim 3 , wherein the vehicle comprises an aircraft, the system further comprising slots disposed in a belly skin of the aircraft for accommodating movement of the lower links.

6. The system of claim 1 , wherein the vehicle is an aircraft and wherein the payload bay door comprises first and second door panels connected to one another via at least one first hinge and the payload bay door is connected to belly skin of the aircraft along a bottom edge of the payload bay via a second hinge, the system further comprising rollers disposed along forward and aft upper edges of the payload bay door, the rollers being in contact with tracks disposed on forward and aft walls of the payload bay for guiding a path of the payload bay door between an open position and a closed position.

7. The system of claim 6 , wherein the first hinge comprises a piano hinge and the second hinge comprises at least one of a piano hinge and a gooseneck hinge.

8. The system of claim 1 , wherein the payload bay door comprises first and second panels, wherein a forward side of each of the first and second panels is connected to a shared curved forward track disposed in a forward wall of the payload bay and an aft side of each of the first and second panels is connected to a shared curved aft track disposed in an aft wall of the payload bay, the forward and aft curved tracks for guiding the payload bay door between an open and a closed position.

9. The system of claim 1 , wherein the payload bay door comprises a single panel door connected to an outboard side of the rack such that the payload bay door translates linearly with the rack between the first and second positions.

10. The system of claim 1 , wherein the payload bay door comprises a plurality of panels, wherein each of the panels is hingedly connected to one or more adjacent ones of the plurality of panels and wherein forward and aft sides of the payload bay door respectively roll along curved tracks disposed in forward and aft walls of the payload bay.

11. An aircraft comprising:
a rack;
a payload bay for storing a payload in the rack;
a rack extension assembly for affecting linear translation of the rack between a first position in which the rack is stowed within the payload bay and a second position in which the rack is supported outside the payload bay;
a payload actuator system for selectively causing the rack extension assembly to move the rack between the first and second positions while the aircraft is in motion;
a payload bay door in at least one of a port side of the vehicle and a starboard side of the vehicle; and
a door actuator system for selectively opening and closing the payload bay door.

12. The aircraft of claim 11 , wherein the payload bay door comprises a single door panel and the door actuator system comprises a forward actuator mechanism comprising upper and lower links for connecting a forward side of the single door panel to a forward wall of the payload bay and an aft actuator mechanism comprising upper and lower links for connecting an aft side of the single door panel to an aft wall of the payload bay.

13. The aircraft of claim 12 , wherein a first end of each of the upper links is rotatably connected to a respective upper link mount provided in the respective wall of the payload bay and a second end of each of the upper links is connected to respective attachment fitting provided in the respective side of the single panel door and wherein a first end of each of the lower links is rotatably connected to a respective lower link mount provided in the respective wall of the payload bay and a second end of each of the lower links is connected to the respective attachment fitting.

14. The aircraft of claim 13 further comprising a track provided in each of the payload bay walls for engaging a respective one of the lower links for providing fore-aft restraint for the single panel door.

15. The aircraft of claim 13 further comprising slots disposed in a belly skin of the aircraft for accommodating movement of the lower links.

16. The aircraft of claim 11 , wherein the payload bay door comprises first and second door panels connected to one another via at least one first hinge and the payload bay door is connected to belly skin of the aircraft along a bottom edge of the payload bay via a second hinge, the aircraft further comprising rollers disposed along forward and aft upper edges of the payload bay door, the rollers being in contact with tracks disposed on forward and aft walls of the payload bay for guiding a path of the payload bay door between an open position and a closed position.

17. The aircraft of claim 16 , wherein the first hinge comprises a piano hinge and the second hinge comprises at least one of a piano hinge and a gooseneck hinge.

18. The aircraft of claim 11 , wherein the payload bay door comprises first and second panels, wherein a forward side of each of the first and second panels is connected to a shared curved forward track disposed in a forward wall of the payload bay and an aft side of each of the first and second panels is connected to a shared curved aft track disposed in an aft wall of the payload bay, the forward and aft curved tracks for guiding the payload bay door between an open and a closed position.

19. The aircraft of claim 11 , wherein the payload bay door comprises a single panel door connected to an outboard side of the rack such that the payload bay door translates linearly with the rack between the first and second positions.

20. The aircraft of claim 11 , wherein the payload bay door comprises a plurality of panels, wherein each of the panels is hing

Assignees

• Bell Textron Inc
• Textron Innovations Inc

Inventors

• Kooiman James Everett
• Williams Jeffrey Matthew
• Smith Clegg Benjamin Brian
• Rinehart Michael E
• Caldwell Franklin Foster
• Heeringa Tjepke

Classifications

• B64C1/1415

  Cargo doors, e.g. incorporating ramps · CPC title

• E05F15/605

  for folding wings · CPC title

• E05Y2800/122

  Telescopic action · CPC title

• E05Y2201/702

  Spindles; Worms · CPC title

• B64D1/06 Primary

  Bomb releasing; Bomb doors · CPC title