SU1332849A1 - The method of processing single-crystal turbine blades of nickel alloys - Google Patents

The method of processing single-crystal turbine blades of nickel alloys

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Publication number
SU1332849A1
SU1332849A1 SU3954843/02A SU3954843A SU1332849A1 SU 1332849 A1 SU1332849 A1 SU 1332849A1 SU 3954843/02 A SU3954843/02 A SU 3954843/02A SU 3954843 A SU3954843 A SU 3954843A SU 1332849 A1 SU1332849 A1 SU 1332849A1
Authority
SU
USSR - Soviet Union
Prior art keywords
turbine blades
nickel alloys
processing single
crystal turbine
heating
Prior art date
Application number
SU3954843/02A
Other languages
Russian (ru)
Inventor
Б.И. Чирков
В.А. Костышев
Т.В. Желнина
Original Assignee
Б.И. Чирков
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Б.И. Чирков filed Critical Б.И. Чирков
Priority to SU3954843/02A priority Critical patent/SU1332849A1/en
Application granted granted Critical
Publication of SU1332849A1 publication Critical patent/SU1332849A1/en

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  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

1. Способ обработки монокристаллических турбинных лопаток из никелевых сплавов, включающий нагрев, отличающийся тем, что, с целью повышения усталостной прочности, перед нагревом проводят поверхностную пластическую деформацию со степенью 5-25%, а нагрев ведут до 1200-1250°С с выдержкой 10-60 мин при этой температуре.2. Способ по п.1, отличающийся тем, что после нагрева осуществляют дополнительную поверхностную пластическую деформацию со степенью 1-3%.1. The method of processing single-crystal turbine blades of nickel alloys, including heating, characterized in that, in order to increase fatigue strength, surface plastic deformation is carried out with a degree of 5-25% before heating, and heating is carried out to 1200-1250 ° C with a holding 10 -60 min at this temperature. The method according to claim 1, characterized in that after heating, an additional surface plastic deformation is performed with a degree of 1-3%.

SU3954843/02A 1985-07-12 1985-07-12 The method of processing single-crystal turbine blades of nickel alloys SU1332849A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3954843/02A SU1332849A1 (en) 1985-07-12 1985-07-12 The method of processing single-crystal turbine blades of nickel alloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3954843/02A SU1332849A1 (en) 1985-07-12 1985-07-12 The method of processing single-crystal turbine blades of nickel alloys

Publications (1)

Publication Number Publication Date
SU1332849A1 true SU1332849A1 (en) 2006-01-27

Family

ID=60519498

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3954843/02A SU1332849A1 (en) 1985-07-12 1985-07-12 The method of processing single-crystal turbine blades of nickel alloys

Country Status (1)

Country Link
SU (1) SU1332849A1 (en)

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