Method for repairing an end plate of a turbomachine rotor

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12228045
APP PUB NO 20240110482A1
SERIAL NO

18264969

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Abstract

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A method for repairing an end plate of a turbomachine rotor, the end plate including a crown having at least two collar fastening holes and at least one balancing-weight fastening hole located between the two collar fastening holes, each collar fastening hole being equipped with a crimped nut, the crown having a damaged portion between two collar fastening holes, the method including the steps of removing the two crimped nuts located on either side of the damage; removing the damaged crown portion, for example by machining; putting in place a strip in the form of a crown portion closing off the removed crown portion, the strip having at least one balancing-weight fastening hole and two mounting holes; fastening the strip to the crown with two crimped nuts, which penetrate the mounting holes, by crimping each nut in a collar fastening hole.

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Patent Owner(s)

  • SAFRAN AIRCRAFT ENGINES

International Classification(s)

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  • 2022 Application Filing Year
  • B23P Class
  • 359 Applications Filed
  • 191 Patents Issued To-Date
  • 53.21 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances20222023202420250255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bot, Cédric Nicolas Moissy-Cramayel, FR 1 0
Lexilus, Jean-Hilaire Moissy-Cramayel, FR 2 0
Reghezza, Patrick Jean-Louis Moissy-Cramayel, FR 25 145

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Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges2170101 - 10010020030040050060070080090010001100120013001400150016001700180019002000210022002300

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