RU2000112277A - DEVICE FOR FIXING A TURBO MACHINE DEFLECTOR - Google Patents

DEVICE FOR FIXING A TURBO MACHINE DEFLECTOR

Info

Publication number
RU2000112277A
RU2000112277A RU2000112277/06A RU2000112277A RU2000112277A RU 2000112277 A RU2000112277 A RU 2000112277A RU 2000112277/06 A RU2000112277/06 A RU 2000112277/06A RU 2000112277 A RU2000112277 A RU 2000112277A RU 2000112277 A RU2000112277 A RU 2000112277A
Authority
RU
Russia
Prior art keywords
fixing
deflector
turbo machine
disk
machine deflector
Prior art date
Application number
RU2000112277/06A
Other languages
Russian (ru)
Other versions
RU2204723C2 (en
Inventor
Владимир Константинович Сычев
Владимир Михайлович Язев
Сергей Иванович Фадеев
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 RU2000112277/06A priority Critical patent/RU2204723C2/en
Priority claimed from RU2000112277/06A external-priority patent/RU2204723C2/en
Publication of RU2000112277A publication Critical patent/RU2000112277A/en
Application granted granted Critical
Publication of RU2204723C2 publication Critical patent/RU2204723C2/en

Links

Claims (1)

Устройство для фиксации дефлектора диска турбомашины, включающее элементы осевой фиксации в виде выступов на поверхности обода дефлектора, размещенных в канавке на ободе диска, а также элемент окружной фиксации дефлектора относительно диска, отличающееся тем, что канавка выполнена с плавным переходом от торцовой к радиальной поверхностям, а элемент окружной фиксации дефлектора выполнен в виде зигзагообразной детали.A device for fixing a disk deflector of a turbomachine, including axial locking elements in the form of protrusions on the surface of the deflector rim placed in a groove on the disk rim, as well as an element of circumferential fixing of the deflector relative to the disk, characterized in that the groove is made with a smooth transition from the end to the radial surfaces, and the circumferential fixation element of the deflector is made in the form of a zigzag part.
RU2000112277/06A 2000-05-15 2000-05-15 Turbomachine disk deflector fixing device RU2204723C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2000112277/06A RU2204723C2 (en) 2000-05-15 2000-05-15 Turbomachine disk deflector fixing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2000112277/06A RU2204723C2 (en) 2000-05-15 2000-05-15 Turbomachine disk deflector fixing device

Publications (2)

Publication Number Publication Date
RU2000112277A true RU2000112277A (en) 2002-04-27
RU2204723C2 RU2204723C2 (en) 2003-05-20

Family

ID=20234708

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2000112277/06A RU2204723C2 (en) 2000-05-15 2000-05-15 Turbomachine disk deflector fixing device

Country Status (1)

Country Link
RU (1) RU2204723C2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2907497B1 (en) * 2006-10-24 2009-01-23 Snecma Sa BALANCING SYSTEM FOR TURBOMACHINE ROTOR
FR2907498B1 (en) * 2006-10-24 2009-01-23 Snecma Sa BALANCING SYSTEM FOR TURBOMACHINE ROTOR
RU2525985C1 (en) * 2013-04-11 2014-08-20 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Gas turbine engine rotor
RU2534672C1 (en) * 2013-11-25 2014-12-10 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) High-temperature turbine rotor

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