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RU2001109680A - TURBOCHARGER - Google Patents

TURBOCHARGER

Info

Publication number
RU2001109680A
RU2001109680A RU2001109680/06A RU2001109680A RU2001109680A RU 2001109680 A RU2001109680 A RU 2001109680A RU 2001109680/06 A RU2001109680/06 A RU 2001109680/06A RU 2001109680 A RU2001109680 A RU 2001109680A RU 2001109680 A RU2001109680 A RU 2001109680A
Authority
RU
Russia
Prior art keywords
sealing rings
turbocharger
cavity
radial channels
bearing housing
Prior art date
Application number
RU2001109680/06A
Other languages
Russian (ru)
Other versions
RU2202052C2 (en
Inventor
Евгений Николаевич Огородников
Original Assignee
Евгений Николаевич Огородников
Filing date
Publication date
Application filed by Евгений Николаевич Огородников filed Critical Евгений Николаевич Огородников
Priority to RU2001109680/06A priority Critical patent/RU2202052C2/en
Priority claimed from RU2001109680/06A external-priority patent/RU2202052C2/en
Publication of RU2001109680A publication Critical patent/RU2001109680A/en
Application granted granted Critical
Publication of RU2202052C2 publication Critical patent/RU2202052C2/en

Links

Claims (1)

Турбокомпрессор наддува двигателя внутреннего сгорания, содержащий корпуса компрессора и турбины, корпус подшипника с ротором, установленный на валу ротора маслоотражатель с уплотнительными кольцами, отличающийся тем, что уплотнительные кольца снабжены радиальными каналами, соединяющими полости канавок уплотнительных колец с полостью корпуса подшипника, причем радиальные каналы соединены между собой кольцевой канавкой.A turbocharger for boosting an internal combustion engine, comprising a compressor housing and a turbine, a bearing housing with a rotor, an oil deflector with sealing rings mounted on the rotor shaft, characterized in that the sealing rings are provided with radial channels connecting the cavity of the grooves of the sealing rings with the cavity of the bearing housing, the radial channels being connected between each other an annular groove.
RU2001109680/06A 2001-04-10 2001-04-10 Turbocompressor RU2202052C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001109680/06A RU2202052C2 (en) 2001-04-10 2001-04-10 Turbocompressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001109680/06A RU2202052C2 (en) 2001-04-10 2001-04-10 Turbocompressor

Publications (2)

Publication Number Publication Date
RU2001109680A true RU2001109680A (en) 2003-02-27
RU2202052C2 RU2202052C2 (en) 2003-04-10

Family

ID=20248296

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001109680/06A RU2202052C2 (en) 2001-04-10 2001-04-10 Turbocompressor

Country Status (1)

Country Link
RU (1) RU2202052C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2517952C1 (en) * 2013-04-26 2014-06-10 Александр Алексеевич Семенов Turbo compressor with controlled supercharge
RU209972U1 (en) * 2021-10-12 2022-03-24 Денис Сергеевич Агафонов Hybrid turbocharger

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2032838C1 (en) * 1991-11-13 1995-04-10 Юрий Вяйнович Гявгянен Torbo-compressor
RU2147084C1 (en) * 1998-04-21 2000-03-27 Уфимский государственный авиационный технический университет Turbine compressor plant
RU2173410C2 (en) * 1999-10-15 2001-09-10 Открытое акционерное общество "Авиадвигатель" Heated swivel guide apparatus of compressor
RU2167353C1 (en) * 1999-11-30 2001-05-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" Method of sealing ring installation between body and shaft

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