Title:
How to produce the reinforcing member for protection of the front tip of a shuttlecock
Document Type and Number:
Japanese Patent JP6189295
Kind Code:
B2
Abstract:
A method of making a reinforcement for reinforcing a leading edge of a blade, the method including depositing a metal coating on the leading edge by thermal spraying in compression. A blade, for example a blade for a turbine engine, a helicopter, or a propeller, can have the leading edge protected by such a reinforcement.
Inventors:
Lodon Paul, Dudon
Allanto, Antonio Cremildo
Allanto, Antonio Cremildo
Application Number:
JP2014524434A
Publication Date:
August 30, 2017
Filing Date:
August 09, 2012
Export Citation:
Assignee:
Saffron Aircraft Engines
International Classes:
C23C4/12; B05D1/08; B05D7/00; B05D7/24; B64C11/26; B64C27/473; C23C4/06; C23C24/04; F01D5/28; F01D25/00; F02C7/00
Domestic Patent References:
| JP2005273015A | ||||
| JP2011117446A | ||||
| JP62165506A | ||||
| JP62113802A | ||||
| JP4032546A | ||||
| JP2230902A | ||||
| JP2006124830A |
Foreign References:
| WO2013021141A1 | ||||
| US20020197152 |
Attorney, Agent or Firm:
Kawaguchi International Patent Office