Three dimensional pinched airflow nozzle and methods for use thereof

Patent metadata

Field	Value
Publication number	US-10633097-B2
Application number	US-201615222566-A
Country	US
Kind code	B2
Filing date	Jul 28, 2016
Priority date	Jul 28, 2016
Publication date	Apr 28, 2020
Grant date	Apr 28, 2020

Abstract

Apparatus and methods for providing a desired volumetric conditioned airflow rate and for reducing noise level, airflow recirculation and airflow separation are disclosed. An example apparatus includes a nozzle housing having a pair of opposing sidewalls and a front and back wall that define an airflow passage. The airflow passage has a centerline extending between the inlet and the outlet and has a plurality of cross-sections taken perpendicular to the centerline that collectively define a smooth contour along a length of the airflow passage. The cross-sections each have a thickness between the front and back wall that is greater at side edges than at the centerline. The thickness of the cross-sections decreases along a length of at least a first portion of the nozzle housing. A width of each of the cross-sections between the sidewalls increases along the length of at least the first portion of the nozzle housing.

First claim

What is claimed is:

1. An apparatus, comprising:
a nozzle housing having an inlet at a first end and an outlet at a second end, wherein the nozzle housing has a pair of opposing sidewalls and has a front wall and a back wall each extending between the pair of opposing sidewalls;
an airflow passage defined by the pair of opposing sidewalls, the front wall and the back wall, wherein the airflow passage has a centerline extending between the inlet and the outlet and has a plurality of cross-sections taken perpendicular to the centerline that collectively define a smooth contour along a length of the airflow passage;
wherein each of the plurality of cross-sections has a thickness between the front wall and the back wall that is greater at side edges of both the front wall and the back wall than at the centerline, wherein the thickness of each of the plurality of cross-sections both at the side edges of the front wall and the back wall and at the centerline decreases along a length of at least a first portion of the nozzle housing from the inlet toward the outlet, wherein a width of each of the plurality of cross-sections between the pair of opposing sidewalls increases along the length of at least the first portion of the nozzle housing from the inlet toward the outlet; and
a second portion of the nozzle housing coupled to the first portion of the nozzle housing, wherein the inlet is coupled to the first portion of the nozzle housing and the outlet is coupled to the second portion of the nozzle housing, wherein both a shape of the smooth contour and an area of each of the plurality of cross-sections along a length of the second portion of the nozzle housing remains constant and the pair of opposing sidewalls that form the airflow passage are rounded and wherein each of the plurality of cross-sections along a length of the second portion of the nozzle housing has a thickness between the front wall and the back wall that is greater at the side edges of both the front wall and the back wall than at the centerline and has a constant width, and wherein the second portion of the nozzle housing includes at least two bent segments such that a centerline of the air flow passage in each of the at least two bent segments is angled relative to the centerline of the airflow passage in a straight segment of the second portion of the nozzle housing.

2. The apparatus of claim 1 , wherein the inlet is coupled to a first end of the first portion of the nozzle housing and the outlet is coupled to a second end of the first portion of the nozzle housing.

3. The apparatus of claim 1 , wherein the front wall and the back wall of the second portion of the nozzle housing are arranged symmetrically with respect to each other about a plane.

4. The apparatus of claim 1 , wherein the second portion of the nozzle has a smooth and rounded transition between the straight segment to a first bent segment of the at least two bent segments.

5. The apparatus of claim 1 , further comprising:
a nozzle extension coupled to the outlet of the nozzle housing and defining a portion of the airflow passage, the nozzle extension having an inlet defining a first area and having an outlet defining a second area that is the same as the first area.

6. The apparatus of claim 5 , wherein the outlet of the nozzle extension has a rectangular shape.

7. The apparatus of claim 5 , wherein a thickness of the inlet of the nozzle extension at the centerline is less than a thickness of the outlet of the nozzle extension, and the thickness of the airflow passage between the front wall and the back wall of the nozzle housing is greater at the side edges of both the front wall and the back wall at the inlet of the nozzle extension than the thickness of the outlet of the nozzle extension.

8. The apparatus of claim 1 , wherein the inlet of the nozzle housing has a circular shape.

9. The apparatus of claim 1 , wherein a length of the nozzle housing between the first end and the second end ranges from 8 inches to 17 inches.

10. The apparatus of claim 8 , wherein the inlet of the nozzle housing has a diameter of 2.5 inches.

11. The apparatus of claim 1 , wherein the nozzle housing is configured to be coupled to a component of an air distribution system.

12. The apparatus of claim 11 , where in the component of the air distribution system is a supply duct.

13. The apparatus of claim 1 , wherein the nozzle housing is injection molded as a single unitary piece.

14. The apparatus of claim 1 , wherein the nozzle housing is injection molded in several segments that are joined together via ultrasonic welding, laser welding, or an adhesive.

15. The apparatus of claim 1 , wherein the nozzle housing is fabricated via 3D printing.

16. The apparatus of claim 1 , wherein the nozzle housing is configured to have two-dimensional flow patterns at the outlet such that airflow velocity vectors in each plane perpendicular to a cross-section at the outlet of the nozzle are parallel to each other.

17. The apparatus of claim 6 , wherein the nozzle extension is configured to provide a uniform velocity distribution of airflow exiting the outlet of the nozzle extension.

18. The apparatus of claim 6 , wherein the nozzle extension is configured to mate with a vent in an aircraft cabin.

19. A method for using a nozzle apparatus, the method comprising:
flowing air through an inlet of an nozzle housing and into an airflow passage, wherein the nozzle apparatus comprises (a) the nozzle housing having the inlet at a first end and an outlet at a second end, wherein the nozzle housing has a pair of opposing sidewalls and has a front wall and a back wall each extending between the pair of opposing sidewalls, (b) the airflow passage that is defined by the pair of opposing sidewalls, the front wall and the back wall, wherein the airflow passage has a centerline extending between the inlet and the outlet and has a plurality of cross-sections taken perpendicular to the centerline that collectively define a smooth contour along a length of the airflow passage, (c) wherein each of the plurality of cross-sections has a thickness between the front wall and the back wall that is greater at side edges of both the front wall and the back wall than at the centerline, wherein the thickness of each of the plurality of cross-sections both at the side edges of the front wall and the back wall and at the centerline decreases along a length of at least a first portion of the nozzle housing from the inlet toward the outlet, wherein a width of each of the plurality of cross-sections between the pair of opposing sidewalls increases along the length of at least the first portion of the nozzle housing from the inlet toward the outlet and (d) a second portion of the nozzle housing coupled to the first portion of the nozzle housing, wherein the inlet is coupled to the first portion of the nozzle housing and the outlet is coupled to the second portion of the nozzle housing, wherein both a shape of the smooth contour and an area of each of the plurality of cross-sections along a length of the second portion of the nozzle housing remains constant and the pair of opposing sidewalls that form the airflow passage are rounded and wherein each of the plurality of cross-sections along a length of the second portion of the nozzle housing has a thickness between the front wall and the back wall that is greater at the side edges of both the front wall and the back wall than at the centerline and has a constant width, and wherein the second portion of the nozzle housing includes at least two bent

Assignees

• Boeing Co

Inventors

• Al-Alusi Thamir R

Classifications

• B60H1/3407 Primary

  providing an air stream in a fixed direction, e.g. using a grid or porous panel · CPC title

• B64D2013/003

  Cabin ventilation nozzles · CPC title

• B64D2013/0625

  comprising means for distribution effusion of conditioned air in the cabin · CPC title

• B64D13/00 Primary

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

• B05B1/005

  Nozzles or other outlets specially adapted for discharging one or more gases · CPC title