SU689051A1 - METHOD OF MANUFACTURING DETAILS OF TYPE OF TURBINE BLADES - Google Patents

METHOD OF MANUFACTURING DETAILS OF TYPE OF TURBINE BLADES

Info

Publication number
SU689051A1
SU689051A1 SU2181029/27A SU2181029A SU689051A1 SU 689051 A1 SU689051 A1 SU 689051A1 SU 2181029/27 A SU2181029/27 A SU 2181029/27A SU 2181029 A SU2181029 A SU 2181029A SU 689051 A1 SU689051 A1 SU 689051A1
Authority
SU
USSR - Soviet Union
Prior art keywords
turbine blades
type
manufacturing details
force
value
Prior art date
Application number
SU2181029/27A
Other languages
Russian (ru)
Inventor
В.И. Шашорин
И.Р. Хаймович
Ю.Н. Краснов
А.И. Хотилин
Original Assignee
В.И. Шашорин
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 В.И. Шашорин filed Critical В.И. Шашорин
Priority to SU2181029/27A priority Critical patent/SU689051A1/en
Application granted granted Critical
Publication of SU689051A1 publication Critical patent/SU689051A1/en

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  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Способ изготовления деталей типа турбинных лопаток путем нагрева заготовки и приложения к ней деформирующего усилия, отличающийся тем, что, с целью повышения точности обработки и снижения трудоемкости процесса, после снятия с полученной детали деформирующего усилия к ней прикладывают дополнительное усилие и выдерживают деталь с ее охлаждением, при этом величину дополнительного усилия устанавливают больше величины усилий, возникающих от термических напряжений при охлаждении детали.A method of manufacturing parts such as turbine blades by heating the workpiece and applying a deforming force to it, characterized in that, in order to improve processing accuracy and reduce the laboriousness of the process, after removing the deforming force from the received part, additional force is applied to it and the part is maintained with cooling at the same time, the value of the additional force is set larger than the value of the forces arising from thermal stresses during cooling of the part.

SU2181029/27A 1975-10-13 1975-10-13 METHOD OF MANUFACTURING DETAILS OF TYPE OF TURBINE BLADES SU689051A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2181029/27A SU689051A1 (en) 1975-10-13 1975-10-13 METHOD OF MANUFACTURING DETAILS OF TYPE OF TURBINE BLADES

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2181029/27A SU689051A1 (en) 1975-10-13 1975-10-13 METHOD OF MANUFACTURING DETAILS OF TYPE OF TURBINE BLADES

Publications (1)

Publication Number Publication Date
SU689051A1 true SU689051A1 (en) 2005-03-20

Family

ID=60522894

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2181029/27A SU689051A1 (en) 1975-10-13 1975-10-13 METHOD OF MANUFACTURING DETAILS OF TYPE OF TURBINE BLADES

Country Status (1)

Country Link
SU (1) SU689051A1 (en)

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