Air curtain systems and methods for vehicle cabins

Patent metadata

Field	Value
Publication number	US-11999490-B2
Application number	US-202117335572-A
Country	US
Kind code	B2
Filing date	Jun 1, 2021
Priority date	Aug 28, 2020
Publication date	Jun 4, 2024
Grant date	Jun 4, 2024

Abstract

A system includes an outflow vent that has a cap releasably mounted to a panel within an internal cabin of a vehicle. The cap is elongated from a first end of the cap to a second end of the cap opposite the first end. The cap has a base wall that is overlaid on the panel and defines at least one slot therethrough. The cap receives an airflow generated by an airflow generator, and the at least one slot emits the airflow from the cap to form an air curtain within the internal cabin.

First claim

What is claimed is:

1. A system comprising:
an outflow vent including a cap releasably mounted to a panel within an internal cabin of a vehicle, the cap having a base wall that is overlaid on the panel and defines a cavity between the panel and the base wall, the base wall defining at least one slot therethrough, the base wall extending from a first end of the cap to a second end of the cap opposite the first end, the first end defining an inlet opening to the cavity and configured to be coupled to a rail so that the inlet opening is fluidly connected to a channel defined by the rail, wherein the cap is configured to receive airflow from the rail into the cavity via the inlet opening and to emit the airflow from the cavity through the at least one slot in the base wall to form an air curtain within the internal cabin.

2. The system of claim 1 , wherein the rail is disposed at an outboard wall of the internal cabin and is elongated to extend along a length of the internal cabin.

3. The system of claim 1 , wherein the outflow vent is a first outflow vent, and the system comprises a second outflow vent including a second cap coupled to the rail at a location that is spaced apart from the cap of the first outflow vent, the second outflow vent configured to emit airflow received from the channel of the rail through at least one slot of the second cap to form a second air curtain within the internal cabin.

4. The system of claim 1 , wherein the panel is a component of a personal service unit (PSU) of an aircraft, the PSU including multiple outlet openings through which air is emitted from the PSU, wherein the cap mounted onto the panel covers at least a first outlet opening of the outlet openings such that the air emitted from the first outlet opening is received into the cavity of the cap and combines with the airflow received through the inlet opening at the first end of the cap.

5. The system of claim 1 , wherein the cap is located above a row of seats within the internal cabin, and the at least one slot of the cap is positioned in front of the row of seats along a longitudinal axis of the internal cabin.

6. The system of claim 1 , wherein the outflow vent includes at least one vane mounted to an interior surface of the cap and angled relative to the interior surface to direct the airflow towards the at least one slot.

7. The system of claim 1 , wherein the outflow vent has a compressible seal along a top edge of the cap, the compressible seal configured to be compressed at an interface between the cap and the panel to seal the interface.

8. The system of claim 1 , wherein the second end of the cap has a hook configured to catch on an edge of the panel.

9. The system of claim 1 , wherein the cap is located above a row of seats within the internal cabin, and the at least one slot defines an air curtain axis that is generally parallel to a row axis of the row of seats.

10. The system of claim 1 , wherein the base wall is elongated parallel to a row axis associated with row of seats within the internal cabin so that the first end of the cap is an outboard end and the second end of the cap is an inboard end.

11. The system of claim 1 , wherein the at least one slot through the base wall includes a first slot that is elongated parallel to row axis associated with row of seats within the internal cabin.

12. A system comprising:
an outflow vent comprising a cap and an attachment unit, the cap releasably mounted to a panel within an internal cabin of a vehicle, the cap having a base wall that is overlaid on the panel and defines at least one slot therethrough,
wherein the attachment unit is mounted to an interior surface of the cap and includes a frame that has a deflectable mounting latch, the frame configured to extend into an outlet opening defined by a vent housing connected to the panel, the deflectable mounting latch configured to catch on the vent housing to secure the outflow vent to the panel,
wherein the cap is configured to receive airflow and to emit the airflow through the at least one slot to form an air curtain within the internal cabin.

13. The system of claim 12 , wherein the attachment unit is releasably coupled to the cap via one or more deflectable coupling latches.

14. The system of claim 12 , wherein the attachment unit is integrally connected to the cap such that the cap and the attachment unit define a unitary, monolithic body.

15. The system of claim 12 , wherein the base wall defines a cavity between the base wall and the panel, wherein a first end of the cap defines an inlet opening to the cavity and the first end is configured to be coupled to a rail within the internal cabin so that the inlet opening is fluidly connected to a channel defined by the rail, wherein the cap is configured to receive airflow from the rail into the cavity via the inlet opening and emits the airflow through the at least one slot in the base wall to form an air curtain within the internal cabin.

16. The system of claim 15 , wherein the rail is disposed at an outboard wall of the internal cabin and the first end of the cap that couples to the rail is an outboard end of the cap, the cavity extending in an inboard direction from the inlet opening.

17. The system of claim 12 , wherein the panel is a component of a personal service unit (PSU) of an aircraft, the outlet opening through which the frame of the attachment unit extends is a first outlet opening of multiple outlet openings of the PSU that emit air into the internal cabin.

18. A vehicle comprising:
an internal cabin including a row of seats and a personal service unit (PSU) disposed above the row of seats, the PSU including a panel and multiple outlet openings through which air is emitted from the PSU; and
an air curtain system within the internal cabin, the air curtain system comprising an outflow vent including a cap releasably mounted to the panel above the row of seats, the cap having a base wall that is overlaid on the panel and defines a cavity between the panel and the base wall, the base wall defining at least one slot therethrough, wherein the cap mounted to the panel covers at least two of the outlet openings so that the air emitted from the at least two outlet openings is received into the cavity of the cap before being emitted from the cap through the at least one slot to form an air curtain associated with the row of seats below.

19. The vehicle of claim 18 , wherein a first end of the cap defines an inlet opening, and
the air curtain system further comprises a rail that that defines a channel through which airflow is directed from a ventilation system of the vehicle, wherein the rail is coupled to the first end of the cap and the channel is fluidly connected to the inlet opening to supply the airflow into the cavity of the cap prior to the airflow being emitted from the cap through the at least one slot to form the air curtain.

20. The vehicle of claim 18 , wherein the at least one slot defines an air curtain axis that is generally parallel to a row axis of the row of seats, and the at least one slot is positioned in front of the row of seats along a longitudinal axis of the internal cabin.

Assignees

• Boeing Co

Inventors

• Vandyke Bryce Avery
• Maben Douglas Dean
• Collins Jonathan William
• Wu Tateh
• Pedersen Anders Michael
• Cordero Edmund Fidelino P

Classifications

• B64D2013/003

  Cabin ventilation nozzles · CPC title

• B60J9/04

  Air curtains (in general F24F) · CPC title

• B64D13/00 Primary

  Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space · CPC title

• B64D13/06 Primary

  the air being conditioned (pressurising B64D13/02) · CPC title

• B64D11/00

  Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title