RU2000111664A - GAS TURBINE ENGINE COMPRESSOR ROTOR - Google Patents

GAS TURBINE ENGINE COMPRESSOR ROTOR

Info

Publication number
RU2000111664A
RU2000111664A RU2000111664/06A RU2000111664A RU2000111664A RU 2000111664 A RU2000111664 A RU 2000111664A RU 2000111664/06 A RU2000111664/06 A RU 2000111664/06A RU 2000111664 A RU2000111664 A RU 2000111664A RU 2000111664 A RU2000111664 A RU 2000111664A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine engine
compressor rotor
engine compressor
annular lock
Prior art date
Application number
RU2000111664/06A
Other languages
Russian (ru)
Other versions
RU2186258C2 (en
Inventor
Анатолий Иванович Тункин
Николай Афанасьевич Аликин
Валерий Алексеевич Кузнецов
Original Assignee
Открытое акционерное общество "Авиадвигатель"
Filing date
Publication date
Application filed by Открытое акционерное общество "Авиадвигатель" filed Critical Открытое акционерное общество "Авиадвигатель"
Priority to RU2000111664A priority Critical patent/RU2186258C2/en
Priority claimed from RU2000111664A external-priority patent/RU2186258C2/en
Publication of RU2000111664A publication Critical patent/RU2000111664A/en
Application granted granted Critical
Publication of RU2186258C2 publication Critical patent/RU2186258C2/en

Links

Claims (1)

Ротор компрессора газотурбинного двигателя, включающий рабочие колеса и лабиринтный диск, установленные на валу с помощью прямоугольных шлиц и зафиксированные в осевом направлении гайкой и кольцевым замком, отличающийся тем, что кольцевой замок выполнен с осевыми выступами, ограниченными в окружном направлении выступами прямоугольных шлиц, а в радиальном направлении - ступицей лабиринтного диска.The compressor rotor of a gas turbine engine, including impellers and a labyrinth disk mounted on a shaft using rectangular slots and axially fixed with a nut and an annular lock, characterized in that the annular lock is made with axial protrusions, rectangular protrusions bounded in the circumferential direction, and in radial direction - the hub of the labyrinth disk.
RU2000111664A 2000-05-10 2000-05-10 Compressor rotor of gas turbine engine RU2186258C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2000111664A RU2186258C2 (en) 2000-05-10 2000-05-10 Compressor rotor of gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2000111664A RU2186258C2 (en) 2000-05-10 2000-05-10 Compressor rotor of gas turbine engine

Publications (2)

Publication Number Publication Date
RU2000111664A true RU2000111664A (en) 2002-04-20
RU2186258C2 RU2186258C2 (en) 2002-07-27

Family

ID=20234433

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2000111664A RU2186258C2 (en) 2000-05-10 2000-05-10 Compressor rotor of gas turbine engine

Country Status (1)

Country Link
RU (1) RU2186258C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2606295C1 (en) * 2015-08-14 2017-01-10 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Gas turbine engine compressor rotor

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