Method of making turbine blades
United States Patent 3228095
US Patent References:
High-temperature stainless steel
- - 2447897
Heat-resisting nickel base alloys
- - 2977222
Method of making turbine blades and the like
- - 2987806
High temperature heat and creep resistant alloy
- - 3047381
Creep-resistant nickel-chromiumcobalt alloy
- - 3107999
High-temperature stainless steel
- - 2447897
Heat-resisting nickel base alloys
- - 2977222
Method of making turbine blades and the like
- - 2987806
High temperature heat and creep resistant alloy
- - 3047381
Creep-resistant nickel-chromiumcobalt alloy
- - 3107999
Inventors:
Raymond, Bird Jack
Wilson, Hall Douglas
Anthony, Denton David
Wilson, Hall Douglas
Anthony, Denton David
Publication Date:
01/11/1966
View Patent Images:
Export Citation:
Assignee:
Rolls, Royce
Primary Class:
Other Classes:
148/428, 29/527.500, 148/442
International Classes:
B21K3/04; B23P15/02; C22C19/00; B21K3/00
US Patent References:
| 3110587 | Nickel-chromium base alloy |
Foreign References:
| CA548777A |