Systems and methods for regulators for inflation systems for evacuation assemblies
US-2024300655-A1 · Sep 12, 2024 · US
US10457407B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10457407-B2 |
| Application number | US-201715466550-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 22, 2017 |
| Priority date | Mar 22, 2017 |
| Publication date | Oct 29, 2019 |
| Grant date | Oct 29, 2019 |
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An evacuation assembly of an aircraft includes an evacuation slide and a sheet coupled to the evacuation slide. The sheet may be deployable in a wind curtain configuration and a canopy configuration. In the wind curtain configuration, the sheet may extend, as a substantially vertical panel, longitudinally along opposing lateral sides of the evacuation slide. In the canopy configuration the sheet may extend over at least a portion of a top side of the evacuation slide. In the canopy configuration, the sheet may include a first portion that is the substantially vertical panel that extends longitudinally along the opposing lateral sides of the evacuation slide and a second portion that extends over the top side of the evacuation slide. The second portion of the curtain may in a furled, collapsed form in the wind curtain configuration and may be configured to unfurl in the canopy configuration.
Opening claim text (preview).
What is claimed is: 1. An evacuation assembly of an aircraft, the evacuation assembly comprising: an evacuation slide; and a sheet coupled to the evacuation slide, wherein the sheet is deployable in a wind curtain configuration and a canopy configuration, wherein the sheet comprises a first portion and a second portion; wherein in the wind curtain configuration: the first portion of the sheet is a substantially vertical panel that extends along one lateral side of two opposing lateral sides of the evacuation slide; the second portion of the sheet is in a furled form that extends along a top edge of the first portion of the sheet that is the substantially vertical panel at the lateral side of the evacuation slide; wherein in the canopy configuration: the second portion is unfurled to extend over a top side of the evacuation slide. 2. The evacuation assembly of claim 1 , wherein in the wind curtain configuration the furled form of the second portion of the sheet is disposed along only the one lateral side of the two opposing lateral sides of the evacuation slide, wherein in the canopy configuration the second portion is unfurled to extend over the top side of the evacuation slide to the other of the two opposing lateral sides of the evacuation slide. 3. The evacuation assembly of claim 1 , wherein in the wind curtain configuration the sheet as the substantially vertical panel is configured to disrupt air flow over the top side of the evacuation slide to produce negative lift in response to air flowing across the evacuation slide in a width direction, wherein the width direction is perpendicular to a longitudinal axis of the evacuation slide. 4. The evacuation assembly of claim 1 , wherein in the wind curtain configuration the furled form of the second portion of the sheet is housed within an enclosure. 5. The evacuation assembly of claim 1 , wherein the second portion of the sheet is unitary with the first portion of the sheet. 6. The evacuation assembly of claim 1 , wherein the second portion of the sheet is separate from the first portion of the sheet. 7. The evacuation assembly of claim 1 , further comprising pillars extending substantially vertically from the opposing lateral sides of the evacuation slide, wherein in the wind curtain configuration the sheet, as the substantially vertical panel, is coupled to the pillars. 8. The evacuation assembly of claim 7 , wherein in the canopy configuration the sheet is detached from the pillars as the substantially vertical panel. 9. The evacuation assembly of claim 1 , wherein: the evacuation assembly comprises a support; and in the canopy configuration, the support is coupled to and extends between the top side of the evacuation slide and the sheet. 10. The evacuation assembly of claim 9 , wherein the support is disposed in a middle section between the two opposing lateral sides of the evacuation slide. 11. The evacuation assembly of claim 10 , wherein in the canopy configuration the sheet is coupled to the support. 12. An evacuation assembly of an aircraft, the evacuation assembly comprising: an evacuation slide; and a sheet coupled to the evacuation slide, the sheet comprising a first portion and a second portion, wherein: the sheet is deployable in a wind curtain configuration and a canopy configuration; in the wind curtain configuration the first portion of the sheet extends, as a substantially vertical panel, longitudinally along opposing lateral sides of the evacuation slide and the second portion is in a furled form; and in the canopy configuration the first portion of the sheet remains as the substantially vertical panel extending longitudinally along the opposing lateral sides of the evacuation slide and the second portion of the sheet is unfurled from a top edge of the substantially vertical panel to extend over the top side of the evacuation slide. 13. A method of using an evacuation assembly of an aircraft, the method comprising: inflating an evacuation slide such that the evacuation slide is in slide mode, wherein in the slide mode a sheet is coupled to the evacuation slide in a wind curtain configuration; detaching the evacuation slide from the aircraft such that the evacuation slide is in raft mode; and configuring the sheet in a canopy configuration, wherein configuring the sheet in the canopy configuration comprises unfurling a second portion of the sheet from a top edge of a first portion of the sheet that forms a substantially vertical panel and extending the second portion of the sheet over a top side of the evacuation slide. 14. The method of claim 13 , wherein configuring the sheet in the canopy configuration is performed in response to the evacuation slide being in the raft mode. 15. The method of claim 13 , wherein configuring the sheet in the canopy configuration is performed after detaching the evacuation slide from the aircraft.
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