Turbine engine with a flow splitter having a profile with inclined serrations

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United States of America Patent

PATENT NO 11629664
APP PUB NO 20200400069A1
SERIAL NO

16969630

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Abstract

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An airflow profile structure having a leading and/or trailing edge profiled with a serrated profile. The serrated profile has a succession of teeth and depressions, characterized in that, along the leading and/or trailing edge, from a first location to a second location, the teeth of the serrated profile are individually inclined towards the second location.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINES75015 PARIS

International Classification(s)

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  • 2019 Application Filing Year
  • F02K Class
  • 432 Applications Filed
  • 280 Patents Issued To-Date
  • 64.82 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances2019202020212022202320240255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Fiack, Matthieu Moissy-Cramayel, FR 4 3
Gea, Aguilera Fernando Moissy-Cramayel, FR 10 7
Gruber, Mathieu Simon Paul Moissy-Cramayel, FR 16 50

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Patent Citation Ranking

  • 0 Citation Count
  • F02K Class
  • 0 % this patent is cited more than
  • 2 Age
Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges3136001 - 10020406080100120140160180200220240260280300320340

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