SU416442A1 - - Google Patents

Info

Publication number
SU416442A1
SU416442A1 SU1726380A SU1726380A SU416442A1 SU 416442 A1 SU416442 A1 SU 416442A1 SU 1726380 A SU1726380 A SU 1726380A SU 1726380 A SU1726380 A SU 1726380A SU 416442 A1 SU416442 A1 SU 416442A1
Authority
SU
USSR - Soviet Union
Prior art keywords
nozzle
turbomachine
longitudinal
radial
flows
Prior art date
Application number
SU1726380A
Other languages
English (en)
Russian (ru)
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 filed Critical
Priority to SU1726380A priority Critical patent/SU416442A1/ru
Application granted granted Critical
Publication of SU416442A1 publication Critical patent/SU416442A1/ru

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
SU1726380A 1971-12-13 1971-12-13 SU416442A1 (enrdf_load_stackoverflow)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1726380A SU416442A1 (enrdf_load_stackoverflow) 1971-12-13 1971-12-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1726380A SU416442A1 (enrdf_load_stackoverflow) 1971-12-13 1971-12-13

Publications (1)

Publication Number Publication Date
SU416442A1 true SU416442A1 (enrdf_load_stackoverflow) 1974-02-25

Family

ID=20496655

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1726380A SU416442A1 (enrdf_load_stackoverflow) 1971-12-13 1971-12-13

Country Status (1)

Country Link
SU (1) SU416442A1 (enrdf_load_stackoverflow)

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