Aircraft having versatile door systems

Patent metadata

Field	Value
Publication number	US-11220852-B2
Application number	US-201916401475-A
Country	US
Kind code	B2
Filing date	May 2, 2019
Priority date	May 2, 2019
Publication date	Jan 11, 2022
Grant date	Jan 11, 2022

Abstract

A versatile door system for an aircraft includes forward and aft door assemblies. The forward door assembly includes a forward hingeable door hingeably coupled to the airframe proximate a forward location of an aircraft opening and a forward slidable door slidably coupled to the forward hingeable door. The aft door assembly includes an aft hingeable door hingeably coupled to the airframe proximate an aft location of the aircraft opening and an aft slidable door slidably coupled to the aft hingeable door. In a closed configuration, the forward hingeable door, the forward slidable door, the aft hingeable door and the aft slidable door are securably disposed within the aircraft opening. In operation, the forward hingeable door, the forward slidable door, the aft hingeable door and the aft slidable door are individually operable to collectively provide access to a selectable width of the aircraft opening.

First claim

What is claimed is:

1. A versatile door system for an aircraft having an airframe including a wing and an aircraft opening that is forward of the wing, the door system comprising:
a forward door assembly including a forward hingeable door and a forward slidable door, the forward hingeable door hingeably coupled to the airframe proximate a forward location of the aircraft opening, the forward slidable door slidably coupled to the forward hingeable door;
an aft door assembly including an aft hingeable door and an aft slidable door, the aft hingeable door hingeably coupled to the airframe proximate an aft location of the aircraft opening, the aft slidable door slidably coupled to the aft hingeable door;
a limiter coupled between the aft hingeable door and the airframe; and
a rail system including a segmented aft upper rail having a first portion coupled to the airframe and a second portion formed on an exterior side of the aft hingeable door;
wherein, the aft slidable door includes a slider bearing configured to sequentially engage the first and second portions of the segmented aft upper rail along a path of travel of the aft slidable door;
wherein, in a closed configuration, the forward hingeable door, the forward slidable door, the aft hingeable door and the aft slidable door are securably disposed within the aircraft opening;
wherein, the limiter is configured to restrict rotational travel of the aft door assembly to prevent contact between the aft door assembly and the wing; and
wherein, the forward hingeable door, the forward slidable door, the aft hingeable door and the aft slidable door are individually operable to collectively provide access to a selectable width of the aircraft opening.

2. The door system as recited in claim 1 wherein the forward slidable door has a closed position in which the forward slidable door is disposed within the aircraft opening and is longitudinally aligned with the forward hingeable door and an open position in which the forward slidable door is slid forward and into an exterior position relative to the forward hingeable door;
wherein the forward hingeable door has a closed position in which the forward hingeable door is disposed within the aircraft opening and an open position in which the forward hingeable door is pivoted forward relative to the forward location of the aircraft opening together with the forward slidable door;
wherein the aft slidable door has a closed position in which the aft slidable door is disposed within the aircraft opening and is longitudinally aligned with the aft hingeable door and an open position in which the aft slidable door is slid aft and into an exterior position relative to the aft hingeable door; and
wherein the aft hingeable door has a closed position in which the aft hingeable door is disposed within the aircraft opening and an open position in which the aft hingeable door is pivoted aft relative to the aft location of the aircraft opening together with the aft slidable door.

3. The door system as recited in claim 2 wherein, in an open configuration, the forward slidable door is in the open position, the forward hingeable door is in the closed position, the aft slidable door is in the closed position and the aft hingeable door is in the closed position such that the door system provides access to about a quarter width of the aircraft opening.

4. The door system as recited in claim 2 wherein, in an open configuration, the forward slidable door is in the closed position, the forward hingeable door is in the closed position, the aft slidable door is in the open position and the aft hingeable door is in the closed position such that the door system provides access to about a quarter width of the aircraft opening.

5. The door system as recited in claim 2 wherein, in an open configuration, the forward slidable door is in the open position, the forward hingeable door is in the open position, the aft slidable door is in the closed position and the aft hingeable door is in the closed position such that the door system provides access to about a half width of the aircraft opening.

6. The door system as recited in claim 2 wherein, in an open configuration, the forward slidable door is in the open position, the forward hingeable door is in the closed position, the aft slidable door is in the open position and the aft hingeable door is in the closed position such that the door system provides access to about a half width of the aircraft opening.

7. The door system as recited in claim 2 wherein, in an open configuration, the forward slidable door is in the closed position, the forward hingeable door is in the closed position, the aft slidable door is in the open position and the aft hingeable door is in the open position such that the door system provides access to about a half width of the aircraft opening.

8. The door system as recited in claim 2 wherein, in an open configuration, the forward slidable door is in the open position, the forward hingeable door is in the open position, the aft slidable door is in the open position and the aft hingeable door is in the closed position such that the door system provides access to about a three quarter width of the aircraft opening.

9. The door system as recited in claim 2 wherein, in an open configuration, the forward slidable door is in the open position, the forward hingeable door is in the closed position, the aft slidable door is in the open position and the aft hingeable door is in the open position such that the door system provides access to about a three quarter width of the aircraft opening.

10. The door system as recited in claim 2 wherein, in an open configuration, the forward slidable door is in the open position, the forward hingeable door is in the open position, the aft slidable door is in the open position and the aft hingeable door is in the open position such that the door system provides access to about a full width of the aircraft opening.

11. The door system as recited in claim 2 wherein, when the forward slidable door is in the open position, the forward slidable door is secured against movement relative to the forward hingeable door; and
wherein, when the aft slidable door is in the open position, the aft slidable door is secured against movement relative to the aft hingeable door.

12. The door system as recited in claim 1 wherein, in the closed configuration, the forward hingeable door, the forward slidable door, the aft hingeable door and the aft slidable door are latched to the airframe.

13. The door system as recited in claim 1 wherein the rail system further comprises a forward upper rail, a forward lower rail and an aft lower rail;
wherein the forward upper rail is at least partially coupled to the airframe;
wherein the forward lower rail is coupled to the forward hingeable door;
wherein the aft lower rail is coupled to the aft hingeable door;
wherein the forward slidable door travels on the forward upper rail and the forward lower rail between open and closed positions; and
wherein the aft slidable door travels on the segmented aft upper rail and the aft lower rail between open and closed positions.

14. The door system as recited in claim 1 wherein the limiter is configured to restrict rotational travel of the aft hingeable door to between about ninety degrees and about one hundred degrees relative to the aft location of the aircraft opening to prevent contact between the aft door assembly and the wing.

15. The door system as recited in claim 1 wherein the limiter further comprises at least one hinge.

16. The door system as recited in claim

Assignees

• Textron Innovations Inc

Inventors

• Groninga Kirk Landon
• Robertson Daniel Bryan

Classifications

• E05D15/58 Primary

  with both swinging and sliding movements · CPC title

• E05Y2900/502

  for aircraft or spacecraft · CPC title

• E05Y2900/00

  Application of doors, windows, wings or fittings thereof · CPC title

• E05Y2600/46

  in or on the wing · CPC title

• E05Y2201/684

  Rails; Tracks · CPC title