Aircraft door and privacy panel assemblies

• US 10,421,546 B2
• Filed: 09/26/2017
• Issued: 09/24/2019
• Est. Priority Date: 04/04/2017
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Dowty, Mark B., Kroener, Kent M.
• Primary Examiner(s): Ellis, Christopher P
• Application Number:
  US15/716,205
• Publication Number:
  US 20180281963A1
• Time in Patent Office: 728 Days
• Field of Search: 2441185
• CPC Class Codes: B64C 1/1461 Structures of doors or surrounding frames
• CPC Class Codes: B64D 11/0606 with privacy shells, screens, separators or the like class dividers B64D11/0023
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00

Abstract

A panel door assembly for providing access to an aircraft passenger suite includes a stationary panel with a side portion extending between upper and lower ends of the panel door assembly. A lower portion of the stationary panel may extend across a width of the panel door assembly and slide along a rail between open and closed positions. A removable panel may connect to the stationary panel and may include a first latching mechanism connecting the removable panel to an upper portion of the stationary panel and a second latching mechanism connecting the removable panel to the lower portion of the stationary panel. An emergency handle may be connected on an inner side of the removable panel, that when actuated, engages the first latching mechanism and the second latching mechanism, disconnecting the removable panel from the stationary panel and providing an egress path from the suite.

Claims

1. A panel door assembly for providing access to an aircraft passenger suite comprising:

a stationary panel having a side portion extending from an upper end to a lower end of the panel door assembly, and a lower portion extending across a width of the panel door assembly, wherein the lower portion is configured to slide along a rail disposed at a lower end of the panel door assembly between an open position and a closed position during normal operations; and

a removable panel detachably attached to the stationary panel, the removable panel including

a first latching mechanism configured to connect the removable panel to an upper portion of the stationary panel,

a second latching mechanism configured to connect the removable panel to the lower portion of the stationary panel, and

an emergency handle connected on an inner side of the removable panel;

wherein the stationary panel and the removable panel are configured to operate as a single panel structure in a normal operational mode as the lower portion of the stationary panel slides along the rail between the open position and the closed position; and

wherein, in an emergency operational mode, the emergency handle is configured, upon actuation, to engage the first latching mechanism and the second latching mechanism such that the removable panel is disconnected from the stationary panel to provide an emergency egress path from the passenger suite.

2. The panel door assembly of claim 1, wherein the removable panel, upon disconnection from the stationary panel, is configured to hinge toward an interior of the aircraft passenger suite.

3. The panel door assembly of claim 1, further comprising a first cable configured to couple of the first latching mechanism to the emergency handle, and a second cable configured to couple the first latching mechanism to the emergency handle such that actuation of the emergency handle causes the first cable to cause release of the first latching mechanism and the second cable to cause release of the second latching mechanism.

4. The panel door assembly of claim 3, wherein each of the first latching mechanism and the second latching mechanism comprises:

a lever configured to rotate about a pivot in response to a pulling force applied by a respective cable coupled to the lever, the pulling force from the respective cable caused by the actuation of the emergency handle; and

a rotating gear coupled to the lever by a connection bar, the connection bar causing rotation of the rotating gear in response to rotation of the lever.

5. The panel door assembly of claim 4, wherein the connection bar includes a groove defining a translation path for a fastener attaching the connection bar to the lever, the groove configured to limit an amount of rotation of the lever.

6. The panel door assembly of claim 5, wherein each lever of the first latching mechanism and the second latching mechanism includes a set of complementary teeth configured to engage gear teeth of the rotating gear, the complementary teeth configured to limit an amount of rotation of the rotating gear.

7. The panel door assembly of claim 4, wherein each of the first latching mechanism and the second latching mechanism further comprises a pivoting latch coupled to the rotating gear, the pivoting latch configured to latch a respective latching mechanism to the stationary panel of the panel door assembly.

8. The panel door assembly of claim 7, wherein rotation of the rotating gear causes rotation of the pivoting latch such that the respective latching mechanism unlatches from the stationary panel of the panel door assembly.

9. The panel door assembly of claim 7, wherein each of the first latching mechanism and the second latching mechanism further comprises a retention mechanism configured resist movement of the pivoting latch when the latching mechanism is in a latched position connecting the removable panel to the stationary panel.

10. The panel door assembly of claim 1, wherein the emergency handle is configured to be actuated in response to pulling the emergency handle in an inward direction toward a passenger within an interior of the passenger suite.

11. The panel door assembly of claim 1, wherein the panel door assembly is configured to extend across at least a portion of an egress path of a front row passenger suite, wherein at least a portion of a forward boundary of the front row passenger suite is defined by a forward cabin monument.

12. The panel door assembly of claim 11, wherein the egress path of the front row passenger suite is defined by an aisle-side edge of the forward cabin monument and an aisle-side privacy panel of the passenger suite.

13. The panel door assembly of claim 12, wherein the aisle-side edge of the forward cabin monument is aligned with the aisle-side privacy panel such that the panel door assembly is configured to extend from the aisle-side privacy panel to the aisle-side edge of the forward cabin monument when the panel door assembly is in the closed position.

14. The panel door assembly of claim 12, wherein the aisle-side edge of the forward cabin monument is out of alignment with the aisle-side privacy panel such that a gap exists between the panel door assembly and the aisle-side edge of the forward cabin monument when the panel door assembly is in the closed position.

15. The panel door assembly of claim 14, wherein a filler door portion is configured to bridge the gap between the panel door assembly in the closed position and the aisle-side edge of the forward cabin monument.

16. A front row aircraft cabin passenger suite including a forward boundary defined by a forward cabin monument, the front row aircraft cabin passenger suite comprising:

an aisle-side privacy panel; and

a panel door assembly for providing access to the aircraft passenger suite configured to extend across at least a portion of an egress path of the passenger suite, the egress path defined by an aisle-side edge of the forward cabin monument and the aisle-side privacy panel, the panel door assembly including

a stationary panel having a side portion extending from an upper end to a lower end of the panel door assembly, and a lower portion extending across a width of the panel door assembly, wherein the lower portion is configured to slide along a rail disposed at a lower end of the panel door assembly between an open position and a closed position in a normal operational mode, and

a removable panel detachably attached to the stationary panel, the removable panel including an emergency handle connected on an inner side of the removable panel;

wherein the stationary panel and the removable panel are configured to operate as a single panel structure in the normal operational mode as the lower portion of the stationary panel slides along the rail between the open position and the closed position; and

wherein the emergency handle is configured, upon actuation, to engage at least one latching mechanism such that the removable panel is disconnected from the stationary panel to provide an emergency egress path from the passenger suite in an emergency operational mode.

17. The front row passenger suite of claim 16, wherein the aisle-side edge of the forward cabin monument is out of alignment with the aisle-side privacy panel such that a gap exists between the panel door assembly and the aisle-side edge of the forward cabin monument when the panel door assembly is in the closed position.

18. The front row passenger suite of claim 17, further comprising a filler door portion configured to bridge the gap between the panel door assembly in the closed position and the aisle-side edge of the forward cabin monument.

19. The front row passenger suite of claim 18, wherein the filler door portion includes a flexible panel having a straight or curved shape.

20. The front row passenger suite of claim 18, wherein the filler door portion is hingedly connected to the forward cabin monument such that the filler door portion hingedly rotates to contact an edge of the panel door assembly when the panel door assembly is in the closed position.