Sliding door

Patent metadata

Field	Value
Publication number	US-11597492-B2
Application number	US-202016733244-A
Country	US
Kind code	B2
Filing date	Jan 3, 2020
Priority date	Jan 3, 2019
Publication date	Mar 7, 2023
Grant date	Mar 7, 2023

Abstract

Systems and methods include providing an aircraft with a fuselage having a sliding door system disposed on at least one side of the fuselage. The sliding door system includes a forward sliding door having an upper slide rail and a lower slide rail, a rearward sliding door having an upper slide rail and a lower slide rail, an upper rail coupled to each of the upper slide rail of the forward sliding door and the upper slide rail of the rearward sliding door, a lower rail coupled to each of the lower slide rail of the forward sliding door and the lower slide rail of the rearward sliding door, and a plurality of actuators coupled to each of the upper rail and the lower rail and configured to displace and retract the forward sliding door and the rearward sliding door linearly with respect to the fuselage.

First claim

What is claimed is:

1. An aircraft, comprising:
a fuselage having a sliding door system disposed on at least one side of the fuselage, the sliding door system, comprising:
a forward sliding door having an upper slide rail and a lower slide rail;
a rearward sliding door having an upper slide rail and a lower slide rail;
an upper rail coupled to each of the upper slide rail of the forward sliding door and the upper slide rail of the rearward sliding door;
a lower rail coupled to each of the lower slide rail of the forward sliding door and the lower slide rail of the rearward sliding door; and
a plurality of actuators coupled to each of the upper rail and the lower rail and configured to displace and retract the forward sliding door and the rearward sliding door linearly with respect to the fuselage;
wherein at least one of the upper rail and the lower rail are movable relative to the fuselage.

2. The aircraft of claim 1 , wherein the forward sliding door and the rearward sliding door are configured to move away from the fuselage simultaneously.

3. The aircraft of claim 1 , wherein the forward sliding door and the rearward sliding door are configured to move toward the fuselage simultaneously.

4. The aircraft of claim 1 , wherein the forward sliding door is configured to slide forward independent of whether the rearward sliding door is moved rearward or forward.

5. The aircraft of claim 1 , wherein the rearward sliding door is configured to slide rearward independent of whether the forward sliding door is moved rearward or forward.

6. The aircraft of claim 1 , wherein the rearward sliding door must be moved fully forward and the forward sliding door must be moved fully rearward to retract the rearward sliding door and the forward sliding door toward the fuselage.

7. A sliding door system, comprising:
a forward sliding door having an upper slide rail and a lower slide rail;
a rearward sliding door having an upper slide rail and a lower slide rail;
an upper rail coupled to each of the upper slide rail of the forward sliding door and the upper slide rail of the rearward sliding door;
a lower rail coupled to each of the lower slide rail of the forward sliding door and the lower slide rail of the rearward sliding door; and
a plurality of actuators coupled to displace at least one of the upper rail and the lower rail.

8. The sliding door system of claim 7 , wherein the forward sliding door and the rearward sliding door are configured to move away from a fuselage simultaneously.

9. The sliding door system of claim 7 , wherein the forward sliding door and the rearward sliding door are configured to move toward a fuselage simultaneously.

10. The sliding door system of claim 7 , wherein the forward sliding door is configured to slide forward independent of whether the rearward sliding door is moved rearward or forward.

11. The sliding door system of claim 7 , wherein the rearward sliding door is configured to slide rearward independent of whether the forward sliding door is moved rearward or forward.

12. The sliding door system of claim 7 , wherein the rearward sliding door must be moved fully forward and the forward sliding door must be moved fully rearward to retract the rearward sliding door and the forward sliding door toward a fuselage.

13. A method of operating an aircraft, comprising:
providing an aircraft comprising a fuselage having a sliding door system disposed on at least one side of the fuselage, the sliding door system comprising a forward sliding door having an upper slide rail and a lower slide rail, a rearward sliding door having an upper slide rail and a lower slide rail, an upper rail coupled to each of the upper slide rail of the forward sliding door and the upper slide rail of the rearward sliding door, a lower rail coupled to each of the lower slide rail of the forward sliding door and the lower slide rail of the rearward sliding door, and a plurality of actuators coupled to each of the upper rail and the lower rail;
selectively operating the plurality of actuators to displace at least one of the upper rail and the lower rail to displace the doors from the fuselage and externally beyond a bulkhead of the fuselage; and
sliding at least one of the forward sliding door forward with respect to the fuselage and the rearward sliding door rearward with respect to the fuselage.

14. The method of claim 13 , wherein the selectively operating the plurality of actuators is initiated by at least one of: (1) a passenger actuating a door handle associated with one of the forward sliding door and the rearward sliding door, (2) a remotely located control center, (3) a control center proximate to the aircraft, (4) a smart communication device, and (5) a pilot or co-pilot of the aircraft via a flight control system, cockpit controls, or other application specific control system of the aircraft.

15. The method of claim 13 , further comprising: sliding the forward sliding door rearward and the rearward sliding door forward until the forward sliding door and the rearward sliding door make contact; and
selectively operating the plurality of actuators to retract the doors within the bulkhead of the fuselage to the closed position.

Assignees

• Bell Textron Inc
• Textron Innovations Inc

Inventors

• Griffiths Paul Charles
• Sugg Bryan
• Bryk Samuel

Classifications

• E05F5/003

  for sliding wings (Fasteners specially adapted for holding sliding wings open E05D13/04) · CPC title

• B64C1/1438 Primary

  of the sliding type · CPC title

• E05Y2900/531

  Doors · CPC title

• E05D15/0621

  Details, e.g. suspension or supporting guides (E05D15/0604, E05D15/08 - E05D15/14 take precedence) · CPC title

• B64C1/1461

  Structures of doors or surrounding frames · CPC title