Systems and methods for regulators for inflation systems for evacuation assemblies
US-2024300655-A1 · Sep 12, 2024 · US
US10384789B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10384789-B2 |
| Application number | US-201615356822-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 21, 2016 |
| Priority date | Nov 21, 2016 |
| Publication date | Aug 20, 2019 |
| Grant date | Aug 20, 2019 |
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An aspirator assembly for an inflatable device may have an inner housing disposed about an axis with an outlet formed through the inner housing. An outer housing may also be disposed about the axis with a surface of the outer housing covering the outlet. The outer housing may be translatable relative to the inner housing to expose the outlet in response to a gas pressure within the aspirator assembly being above a threshold.
Opening claim text (preview).
What is claimed is: 1. An aspirator and pressure relief valve assembly for an inflatable device, comprising: an inner housing disposed about an axis and having an outlet formed through a radially outer surface of the inner housing; and an outer housing translatable along the radially outer surface of the inner housing and disposed about the axis with a surface of the outer housing covering the outlet, wherein the outer housing is configured to translate relative to the inner housing to expose the outlet to an ambient environment in response to a gas pressure within the aspirator and pressure relief valve assembly being above a threshold. 2. The aspirator and pressure relief valve assembly of claim 1 , further comprising a flap coupled to the inner housing and configured to open and close in response to the gas pressure within the aspirator and pressure relief valve assembly. 3. The aspirator and pressure relief valve assembly of claim 1 , wherein the outer housing is fixed relative to the inflatable device. 4. The aspirator and pressure relief valve assembly of claim 3 , wherein the inner housing is configured to translate axially relative to the outer housing and the inflatable device in response to the gas pressure within the aspirator and pressure relief valve assembly. 5. The aspirator and pressure relief valve assembly of claim 1 , further comprising a spring assembly configured to bias the inner housing and the outer housing into a closed position. 6. The aspirator and pressure relief valve assembly of claim 5 , further comprising a face seal disposed between the inner housing and the outer housing. 7. The aspirator and pressure relief valve assembly of claim 5 , wherein the spring assembly further comprises: a pin extending through a wall of the inner housing; an end cap coupled to the pin; and a spring retained on the pin between the end cap and the wall of the inner housing. 8. The aspirator and pressure relief valve assembly of claim 5 , wherein a spring constant of the spring assembly is selected to urge the inner housing and the outer housing into the closed position in response to the gas pressure within the aspirator and pressure relief valve assembly dropping below the threshold. 9. An evacuation slide assembly, comprising: a slide; an aspirator and pressure relief valve assembly comprising: an outer housing coupled to the slide; an inner housing slideably engaged with the outer housing and an outlet formed through a radially outer surface of the inner housing, the outlet covered by the outer housing in a closed position, wherein the inner housing is configured to translate along the outer housing to expose the outlet to an ambient environment; and a charged tank in fluid communication with an inlet of the inner housing. 10. The evacuation slide assembly of claim 9 , wherein the inner housing is configured to translate relative to the outer housing in response to a gas pressure within the aspirator and pressure relief valve assembly being above a threshold. 11. The evacuation slide assembly of claim 9 , further comprising a flap coupled to the inner housing and configured to open in response to a pressurized gas from the charged tank. 12. The evacuation slide assembly of claim 9 , further comprising a spring assembly configured to bias the inner housing and the outer housing into a closed position. 13. The evacuation slide assembly of claim 12 , further comprising a face seal disposed between the inner housing and the outer housing. 14. The evacuation slide assembly of claim 12 , wherein the spring assembly further comprises: a pin extending through a wall of the inner housing; an end cap coupled to the pin; and a spring retained on the pin between the end cap and the wall of the inner housing. 15. The evacuation slide assembly of claim 14 , wherein a spring constant of the spring is selected to urge the inner housing and the outer housing into the closed position in response to a gas pressure within the aspirator and pressure relief valve assembly dropping below a threshold. 16. An aircraft having an evacuation slide assembly comprising: a housing; a panel covering the housing; a slide retained within the housing; an aspirator and pressure relief valve assembly coupled to the slide and comprising: an outer housing coupled to the slide; an inner housing slideably coupled to the outer housing and having an outlet formed through a radially outer surface of the inner housing, the outlet covered by the outer housing in a closed position, wherein the inner housing is configured to translate along the outer housing to expose the outlet to an ambient environment; and a charged tank in fluid communication with an inlet of the inner housing. 17. The aircraft having an evacuation slide assembly of claim 16 , wherein the inner housing is configured to translate relative to the outer housing in response to a gas pressure within the aspirator and pressure relief valve assembly being above a threshold. 18. The aircraft having an evacuation slide assembly of claim 16 , further comprising a flap coupled to the inner housing and configured to open in response to a pressurized gas from the charged tank. 19. The aircraft having an evacuation slide assembly of claim 16 , further comprising a spring assembly configured to bias the inner housing and the outer housing into the closed position. 20. The aircraft having an evacuation slide assembly of claim 19 , wherein the spring assembly further comprises: a pin extending through a wall of the inner housing; an end cap coupled to the pin; and a spring retained on the pin between the end cap and the wall of the inner housing.
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