RU2016146883A3 - - Google Patents

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Publication number
RU2016146883A3
RU2016146883A3 RU2016146883A RU2016146883A RU2016146883A3 RU 2016146883 A3 RU2016146883 A3 RU 2016146883A3 RU 2016146883 A RU2016146883 A RU 2016146883A RU 2016146883 A RU2016146883 A RU 2016146883A RU 2016146883 A3 RU2016146883 A3 RU 2016146883A3
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RU
Russia
Application number
RU2016146883A
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Russian (ru)
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RU2662755C2 (en
RU2016146883A (en
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Priority to RU2016146883A priority Critical patent/RU2662755C2/en
Publication of RU2016146883A publication Critical patent/RU2016146883A/en
Publication of RU2016146883A3 publication Critical patent/RU2016146883A3/ru
Application granted granted Critical
Publication of RU2662755C2 publication Critical patent/RU2662755C2/en

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RU2016146883A 2016-11-29 2016-11-29 Place of mounting of working blades of booster rotors and compressor of aviation engines of fifth generation; booster rotor and rotor of high pressure compressor of first generation aviation engine, with working blades, fixed with help of swallowtail type locks in ring grooves of these devices; method of assembling place of mounting working blades of booster rotors and compressor RU2662755C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2016146883A RU2662755C2 (en) 2016-11-29 2016-11-29 Place of mounting of working blades of booster rotors and compressor of aviation engines of fifth generation; booster rotor and rotor of high pressure compressor of first generation aviation engine, with working blades, fixed with help of swallowtail type locks in ring grooves of these devices; method of assembling place of mounting working blades of booster rotors and compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2016146883A RU2662755C2 (en) 2016-11-29 2016-11-29 Place of mounting of working blades of booster rotors and compressor of aviation engines of fifth generation; booster rotor and rotor of high pressure compressor of first generation aviation engine, with working blades, fixed with help of swallowtail type locks in ring grooves of these devices; method of assembling place of mounting working blades of booster rotors and compressor

Publications (3)

Publication Number Publication Date
RU2016146883A RU2016146883A (en) 2018-05-29
RU2016146883A3 true RU2016146883A3 (en) 2018-05-29
RU2662755C2 RU2662755C2 (en) 2018-07-30

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ID=62557568

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016146883A RU2662755C2 (en) 2016-11-29 2016-11-29 Place of mounting of working blades of booster rotors and compressor of aviation engines of fifth generation; booster rotor and rotor of high pressure compressor of first generation aviation engine, with working blades, fixed with help of swallowtail type locks in ring grooves of these devices; method of assembling place of mounting working blades of booster rotors and compressor

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RU (1) RU2662755C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2740442C2 (en) * 2019-06-27 2021-01-14 федеральное государственное автономное образовательное учреждение высшего образования "Самарский национальный исследовательский университет имени академика С.П. Королёва" Axle compressor blisk and rotor of low-pressure compressor of aircraft gas turbine engine
CN117346635B (en) * 2023-12-06 2024-03-12 成都格瑞特高压容器有限责任公司 Outer diameter measuring device and measuring method for cylindrical gas cylinder

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU641129A1 (en) * 1976-03-03 1979-01-05 Куйбышевский Ордена Трудового Красного Знамени Авиационный Институт Имени Академика С.П.Королева Turbomachine blade
US5518369A (en) * 1994-12-15 1996-05-21 Pratt & Whitney Canada Inc. Gas turbine blade retention
FR2945074B1 (en) * 2009-04-29 2011-06-03 Snecma REINFORCED BLOW OF BREATHING BLADE
RU2570087C1 (en) * 2014-08-22 2015-12-10 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Impeller of rotor of gas turbine engine with dampening of vibration oscillations

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Publication number Publication date
RU2662755C2 (en) 2018-07-30
RU2016146883A (en) 2018-05-29

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Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20181130

NF4A Reinstatement of patent

Effective date: 20210713