Title:
ターボ機械部品、ブランクおよび最終部品の製造方法
Document Type and Number:
Japanese Patent JP6871860
Kind Code:
B2
Abstract:
The manufacture of a metal turbomachine part, comprising steps consisting of melting a titanium-aluminium intermetallic compound by plasma torch in a ring mould, extracting therefrom an ingot, as cast, in a state cooled from molten, cutting the ingot into at least one blank with an external shape that is simpler than the more complex one of said part to be manufactured, and machining the blank in order to obtain the part with said more complex external shape.
More Like This:
Inventors:
Martin, Guillaume
Marcillon, Celine Jeanne
Minur-Panijon, Marie
Marcillon, Celine Jeanne
Minur-Panijon, Marie
Application Number:
JP2017548026A
Publication Date:
May 19, 2021
Filing Date:
March 04, 2016
Export Citation:
Assignee:
Saffron Aircraft Engines
International Classes:
B22D11/041; B22D11/00; B22D11/12; B22D21/06; C22C14/00; C22C21/00; C22F1/04; C22F1/18; F01D5/28; F01D25/00
Domestic Patent References:
| JP2003533594A | ||||
| JP2005508758A | ||||
| JP2013209750A |
Foreign References:
| WO2014057222A1 |
Attorney, Agent or Firm:
Kawaguchi International Patent Office
Previous Patent: 亜鉛ジアクリレート誘導体および過酸化物を含む組成物を含んでいるタイ...
Next Patent: 血管内温度管理カテーテルおよび／または熱交換パッドのための熱交換器...
Next Patent: 血管内温度管理カテーテルおよび／または熱交換パッドのための熱交換器...