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US Patent 10557415 Turbo-engine including two separate ventilation flows

Patent 10557415 was granted and assigned to Safran on February, 2020 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Current Assignee
Safran
Safran
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Date Filed
April 1, 2016
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Date of Patent
February 11, 2020
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Patent Applicant
Safran
Safran
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Patent Application Number
15088525
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Patent Citations Received
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US Patent 11480063 Gas turbine engine with inlet pre-swirl features
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US Patent 11655768 High fan up speed engine
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US Patent 11767790 Object direction mechanism for turbofan engine
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US Patent 11788465 Bleed flow assembly for a gas turbine engine
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US Patent 12085019 Object direction mechanism for turbofan engine
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US Patent 12116929 Bleed flow assembly for a gas turbine engine
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Patent Inventor Names
Jean-Christophe Duffet
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Gilles Alain Charier
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Tewfik Boudebiza
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Augustin Marc Michel Curlier
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
10557415
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Patent Primary Examiner
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William H Rodríguez
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