Aspirators for evacuation assemblies

Patent metadata

Field	Value
Publication number	US-11143208-B2
Application number	US-201916399469-A
Country	US
Kind code	B2
Filing date	Apr 30, 2019
Priority date	Dec 17, 2018
Publication date	Oct 12, 2021
Grant date	Oct 12, 2021

Abstract

An aspirator for an evacuation assembly includes a duct defining a flow axis with an upstream portion and a downstream portion, a vane spanning the upstream portion of the duct, and a nozzle. The nozzle has an outlet, is supported by the vane, and is positioned within the upstream portion of the duct. The outlet is laterally offset from the flow axis and is axially overlapped by the vane to limit resistance to a primary gas flow entering the duct through the outlet of the nozzle. Evacuation assemblies are also described.

First claim

What is claimed is:

1. An aspirator for an evacuation assembly, comprising:
a duct defining a flow axis with an upstream portion and a downstream portion;
a vane spanning the upstream portion of the duct, the vane having a u-shaped profile including a base segment and first and second edge segments, wherein the first edge segment extends laterally from the base segment and towards an inlet of the duct and is oriented obliquely toward the flow axis and the second edge segment extends laterally from the base segment on a side of the flow axis opposite the first edge segment and is oriented obliquely toward the flow axis; and
a nozzle with an outlet supported by the vane and positioned within the upstream portion of the duct, wherein the outlet of the nozzle is laterally offset from the flow axis.

2. The aspirator as recited in claim 1 , wherein the nozzle is a converging-diverging type nozzle.

3. The aspirator as recited in claim 1 , wherein the nozzle is a first nozzle and the aspirator further includes a second nozzle, the second nozzle arranged on a side of the flow axis opposite the first nozzle.

4. The aspirator as recited in claim 1 , wherein the aspirator has no more than two nozzles.

5. The aspirator as recited in claim 1 , further comprising a manifold coupling the nozzle to the vane.

6. The aspirator as recited in claim 3 , wherein the manifold has a first tine portion and a second tine portion located on a side of the flow axis axially opposite the first tine portion.

7. The aspirator as recited in claim 6 , wherein the manifold has a bident shape with arcuate segments coupling the first and second tine portions to a stem portion, the stem portion seated in the vane.

8. The aspirator as recited in claim 6 , wherein the first nozzle is seated within the first tine portion, wherein the second nozzle is seated with the second tine portion.

9. The aspirator as recited in claim 1 , further comprising a union for connecting a compressed gas source to the nozzle, wherein the union is arranged upstream of the upstream portion of the duct, and wherein union is arranged along the flow axis defined by the duct.

10. The aspirator as recited in claim 1 , further comprising a pressurized gas source connected to the nozzle.

11. The aspirator as recited in claim 1 , wherein the upstream portion of the duct has a flow area with a rectangular shape, wherein the downstream portion of the duct has a flow area with a round shape, and wherein the duct further comprises a transition portion coupling the downstream portion to the upstream portion, the transition portion transitioning from a flow area with rectangular shape on an upstream end to a flow area with a round shape on the downstream end of the transition portion.

12. The aspirator as recited in claim 11 , wherein the outlet is located upstream of the transition portion of the duct.

13. The aspirator as recited in claim 1 , further comprising an inflatable body connected to the downstream portion of the duct and in fluid communication with the upstream portion of the duct.

14. The aspirator as recited in claim 1 , further comprising at least one of an aircraft evacuation slide, a life raft, and a pontoon connected to the downstream portion of the duct and in fluid communication through downstream portion of the duct with the upstream portion of the duct.

15. The aspirator as recited in claim 1 , wherein the vane divides an entrance into the upstream portion of the duct into a first secondary air inlet and a second secondary air inlet.

16. The aspirator as recited in claim 1 , wherein the nozzle is coupled to the base segment of the vane, the edge segments bounding a first secondary gas inlet and second secondary gas inlet into the upstream portion of the duct.

17. The aspirator as recited in claim 1 , wherein the upstream portion of the duct has a height of 4.8 inches (12.2 centimeters), wherein the upstream portion of the duct has a width of 5.6 inches (14.2 centimeters), wherein the downstream portion of the duct has a diameter of 4 inches (10.2 centimeters), and wherein the aspirator has an axial length of 17 inches (43.2 centimeters).

18. An evacuation assembly, comprising:
an aspirator as recited in claim 1 ;
a manifold coupling the nozzle to the vane and having a first tine portion and a second tine portion located on a side of the flow axis axially opposite the first tine portion;
a pressurized gas source connected to the nozzle; and
an inflatable body selected from a group includes an aircraft evacuation slide, a life raft, and a pontoon connected to the outlet portion of the duct and in fluid communication through downstream portion with the upstream portion of the duct.

19. The evacuation assembly as recited in claim 18 , wherein the vane divides a secondary inlet located on the upstream portion of the duct into a first secondary air inlet and a second secondary air inlet, wherein the vane has a u-shaped profile with a base portion and opposed leg portions, the nozzle connected to the base portion of the vane, the leg portions bounding an inlet of the upstream portion of the duct.

20. The evacuation assembly as recited in claim 18 , wherein the nozzle is a converging-diverging nozzle, wherein the nozzle is first nozzle and further comprising a second nozzle, the second nozzle arranged on a side of the flow axis opposite the first nozzle, and wherein the aspirator has no more than two nozzles.

Assignees

• Goodrich Corp

Inventors

• Kuppan Skandan Berikai

Classifications

• B64D25/14 Primary

  Inflatable escape chutes · CPC title

• F04F5/466 Primary

  with a plurality of nozzles arranged in parallel · CPC title

• F04F5/16

  displacing elastic fluids · CPC title

• F04F5/46

  Arrangements of nozzles · CPC title

• F04F5/463

  with provisions for mixing · CPC title