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    Combustion arrester test systems and methods

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    Name:
    US20180280747A1.pdf
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    3.206Mb
    Format:
    PDF
    Description:
    Patent
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    Type
    Patent
    Patent Status
    Published Application
    Authors
    Kwon, Eddie
    Damazo, Jason Scott
    Lacoste, Deanna
    Roberts, William Lafayette
    Assignee
    The Boeing Company
    King Abdullah University Of Science And Technology
    Date
    2018-10-04
    Submitted Date
    2017-03-28
    Permanent link to this record
    http://hdl.handle.net/10754/629828
    
    Metadata
    Show full item record
    Abstract
    Systems, kits, and methods for testing a combustion arrester are disclosed. Systems include an upstream chamber, a downstream chamber, and a combustion arrester between the upstream chamber and the downstream chamber. The upstream chamber includes an ignition port configured to receive an ignition source. And, the upstream chamber defines a convergent duct that converges toward the combustion arrester and terminates at the combustion arrester. The upstream chamber may include a hierarchical series of modular shell sections that define the convergent duct. The downstream chamber may include a series of modular shell sections.
    Application Number
    US20180280747A1
    EP3381520A1
    Additional Links
    https://patents.google.com/patent/US20180280747A1/en
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