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SU552410A1 - Turbocharger - Google Patents

Turbocharger

Info

Publication number
SU552410A1
SU552410A1 SU2187257A SU2187257A SU552410A1 SU 552410 A1 SU552410 A1 SU 552410A1 SU 2187257 A SU2187257 A SU 2187257A SU 2187257 A SU2187257 A SU 2187257A SU 552410 A1 SU552410 A1 SU 552410A1
Authority
SU
USSR - Soviet Union
Prior art keywords
turbocharger
mass
limits
larger
result
Prior art date
Application number
SU2187257A
Other languages
Russian (ru)
Inventor
Вячеслав Александрович Кочетов
Юрий Борисович Моргулис
Герман Митрофанович Поветкин
Original Assignee
Предприятие П/Я А-1697
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 Предприятие П/Я А-1697 filed Critical Предприятие П/Я А-1697
Priority to SU2187257A priority Critical patent/SU552410A1/en
Application granted granted Critical
Publication of SU552410A1 publication Critical patent/SU552410A1/en

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Supercharger (AREA)

Description

 сков подшипниковой втулки коэффициент демпфировани  со стороны, имеющей большую массу колеса турбины, больше, чем со стороны крыльчатки компрессора, имеющей меньшую массу, и за счет этого расшир ютс  границы устойчивой работы подшипников ротора турбокомпрессора.For example, in the bearing sleeve, the damping coefficient on the side with a large mass of turbine wheel is larger than that of the compressor impeller, which has a smaller mass, and as a result, the limits of stable operation of the rotor bearings of the turbo compressor expand.

Claims (1)

1. Патент США № 3811741, кл. 308-122, 1974.1. US patent No. 3811741, CL. 308-122,1974. V///; /////////,V ///; /////////, trtr /.4,-i/.4 .-i // IffIff
SU2187257A 1975-10-31 1975-10-31 Turbocharger SU552410A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2187257A SU552410A1 (en) 1975-10-31 1975-10-31 Turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2187257A SU552410A1 (en) 1975-10-31 1975-10-31 Turbocharger

Publications (1)

Publication Number Publication Date
SU552410A1 true SU552410A1 (en) 1977-03-30

Family

ID=20636568

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2187257A SU552410A1 (en) 1975-10-31 1975-10-31 Turbocharger

Country Status (1)

Country Link
SU (1) SU552410A1 (en)

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