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US Patent 10465706 Adjustable-trim centrifugal compressor for a turbocharger

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Date Filed
March 1, 2017
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Date of Patent
November 5, 2019
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Patent Applicant
Honeywell
Honeywell
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Patent Application Number
15446054
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Patent Citations Received
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US Patent 11946480 Centrifugal compressor
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US Patent 11525451 Compressor inlet adjustment mechanism
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US Patent 11591926 Turbocharger including a switchable trim compressor and ported shroud
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US Patent 11260978 Valve for aircraft environmental control system conduit
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US Patent 11300043 Internal combustion engine comprising a turbocharger with variability at the compressor inlet
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US Patent 11401948 Turbocharger compressor with inlet-adjustment mechanism having pivoting blades forming adjustable uninterrupted blade ring
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US Patent 11415149 Compressor inlet arrangement
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US Patent 11885343 Centrifugal compressor
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Patent Inventor Names
Stephane Doise
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Hani Mohtar
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Stephane Pees
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Alain Lombard
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
10465706
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Patent Primary Examiner
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Patrick D Maines
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