SU674487A1 - Лопатка турбомашины - Google Patents

Лопатка турбомашины

Info

Publication number
SU674487A1
SU674487A1 SU2577283/06A SU2577283A SU674487A1 SU 674487 A1 SU674487 A1 SU 674487A1 SU 2577283/06 A SU2577283/06 A SU 2577283/06A SU 2577283 A SU2577283 A SU 2577283A SU 674487 A1 SU674487 A1 SU 674487A1
Authority
SU
USSR - Soviet Union
Prior art keywords
turbomachine
blade
Prior art date
Application number
SU2577283/06A
Other languages
English (en)
Inventor
В.А. Яковлев
Е.П. Денисова
Г.К. Тананин
Ф.В. Шухов
Original Assignee
В.А. Яковлев
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.А. Яковлев filed Critical В.А. Яковлев
Priority to SU2577283/06A priority Critical patent/SU674487A1/ru
Application granted granted Critical
Publication of SU674487A1 publication Critical patent/SU674487A1/ru

Links

SU2577283/06A 1978-02-06 1978-02-06 Лопатка турбомашины SU674487A1 (ru)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2577283/06A SU674487A1 (ru) 1978-02-06 1978-02-06 Лопатка турбомашины

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2577283/06A SU674487A1 (ru) 1978-02-06 1978-02-06 Лопатка турбомашины

Publications (1)

Publication Number Publication Date
SU674487A1 true SU674487A1 (ru) 1995-02-20

Family

ID=60516778

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2577283/06A SU674487A1 (ru) 1978-02-06 1978-02-06 Лопатка турбомашины

Country Status (1)

Country Link
SU (1) SU674487A1 (ru)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112032105A (zh) * 2020-11-05 2020-12-04 中国航发上海商用航空发动机制造有限责任公司 转子叶尖间隙控制方法及利用该方法制造的转子叶片

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112032105A (zh) * 2020-11-05 2020-12-04 中国航发上海商用航空发动机制造有限责任公司 转子叶尖间隙控制方法及利用该方法制造的转子叶片
US12055048B2 (en) 2020-11-05 2024-08-06 Aecc Shanghai Commercial Aircraft Engine Manufacturing Co., Ltd. Method for rotor blade tip clearance control and rotor blade manufactured by the method

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