FIELD: process engineering.
SUBSTANCE: invention relates to machine building, particularly, to turbo machine flow section seals operated at higher temperatures and high-frequency oscillations. Proposed method comprises sintering preset size and shape rods from run-in material powders. Aforesaid run-in material represents a mechanical mix of allow powder containing the following components, in wt %: Cr - 10.0 to 18.0%, Mo - 0.8 to 3.7%, Fe or Ti or Cu or combination thereof making the rest, or allow containing: Cr - 18% to 34%; Al - 3% to 16%; Y - 0.2% to 0.7%; Ni making the rest, or alloy containing: Cr - 18% to 34%; Al - 3% to 16%; Y - 0.2% to 0.7%; Ni making the rest. With particle size varying from 15 mcm to 180 mcm, with powders of hexagonal boron nitride with particle size less than 1 mcm in amount of 1.0-1.5% of total mix amount and calcium fluoride CaF2 with particle size of 1 mcm to 25 mcm in amount of 6.0-8.0% of total amount of mix. Note here that sintering is carried out at 1100-1200°C in vacuum or one of the following media ammonia, mix of argon with ammonia, mix of hydrogen with nitrogen, mix of hydrogen, argon and nitrogen.
EFFECT: higher run-in properties, mechanical strength and wear resistance.
11 cl, 1 ex
Title | Year | Author | Number |
---|---|---|---|
TURBINE WORN-IN SEAL ELEMENT | 2011 |
|
RU2484924C2 |
METHOD OF MAKING TURBO MACHINE CONFORMABLE SEAL | 2011 |
|
RU2478454C1 |
METHOD OF MAKING TURBO MACHINE CONFORMABLE SEAL ELEMENT WITH REINFORCED SHELL | 2011 |
|
RU2484925C2 |
METHOD OF MAKING TURBO MACHINE CONFORMABLE SEAL | 2011 |
|
RU2507033C2 |
METHOD OF FABRICATING REINFORCED ELEMENT OF TURBINE RUN-IN SEAL | 2011 |
|
RU2457067C1 |
METHOD OF FABRICATING TURBINE RUN-IN CELLULAR SEAL | 2011 |
|
RU2457066C1 |
METHOD OF FABRICATING TURBINE RUN-IN ALIGNED-STRUCTURE SEAL | 2011 |
|
RU2457071C1 |
METHOD OF FABRICATING TURBINE RUN-IN SEAL WITH MULTILAYER SHELL | 2011 |
|
RU2461449C1 |
METHOD OF FABRICATING TURBINE RUN-IN COLUMNAR-STRUCTURE SEAL | 2011 |
|
RU2461448C1 |
LABYRINTH SHROUD SEAL FOR STEAM TURBINE | 2011 |
|
RU2499144C2 |
Authors
Dates
2012-07-27—Published
2011-05-03—Filed