Protective coating for titanium alloy blades for turbine and turbo-compressor rotors
Номер патента: GB1479855A
Опубликовано: 13-07-1977
Автор(ы):
Принадлежит: Statni Vyzkumny Ustav Materialu
Опубликовано: 13-07-1977
Автор(ы):
Принадлежит: Statni Vyzkumny Ustav Materialu
Реферат: 1479855 Protective coating STATNI VYZKUMNY USTAV MATERIALU 23 April 1976 [23 April 1975] 16902/75 Heading C7A A protective coating for use on titanium or Tialloy-based blades containing at least one of Al, Su, Mo, V, Fe, Cr or Zr in turbine or other engine applications consists of a beta-phase stabilized Ti alloy containing:- Ti Bal, not less than 65% impurities, such as 0À2% oxygen, 0À1% nitrogen, 0À03% hydrogen and 0À05% C, must be less than 1%. The coating may be cast, hot or cold worked and attached to the component by brazing, soldering, welding &c. or may be attached by a powder metallurgy technique.
Protective coating and component of gas turbine with such coating
Номер патента: RU2631552C2. Автор: Син-Хай ЛИ. Владелец: СИМЕНС АКЦИЕНГЕЗЕЛЛЬШАФТ. Дата публикации: 2017-09-25.