Dual configuration wind curtain for evacuation assembly

US10457407B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10457407-B2
Application numberUS-201715466550-A
CountryUS
Kind codeB2
Filing dateMar 22, 2017
Priority dateMar 22, 2017
Publication dateOct 29, 2019
Grant dateOct 29, 2019

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

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.

First claim

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.

Assignees

Inventors

Classifications

  • B64D25/14Primary

    Inflatable escape chutes · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US10457407B2 cover?
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 shee…
Who is the assignee on this patent?
Goodrich Corp
What technology area does this patent fall under?
Primary CPC classification B64D25/14. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Oct 29 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).