RU94009834A - GAS-INFLATABLE TURBINE WITH RADIAL FLOW PASSAGE - Google Patents

GAS-INFLATABLE TURBINE WITH RADIAL FLOW PASSAGE

Info

Publication number
RU94009834A
RU94009834A RU94009834/06A RU94009834A RU94009834A RU 94009834 A RU94009834 A RU 94009834A RU 94009834/06 A RU94009834/06 A RU 94009834/06A RU 94009834 A RU94009834 A RU 94009834A RU 94009834 A RU94009834 A RU 94009834A
Authority
RU
Russia
Prior art keywords
rotary shaft
gas
flow passage
radial flow
guide vanes
Prior art date
Application number
RU94009834/06A
Other languages
Russian (ru)
Other versions
RU2125164C1 (en
Inventor
Бэтс Йозеф
Цендер Марсель
Original Assignee
АББ Менеджмэнт АГ
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
Priority claimed from DE4309636A external-priority patent/DE4309636C2/en
Application filed by АББ Менеджмэнт АГ filed Critical АББ Менеджмэнт АГ
Publication of RU94009834A publication Critical patent/RU94009834A/en
Application granted granted Critical
Publication of RU2125164C1 publication Critical patent/RU2125164C1/en

Links

Claims (1)

Газонагнетательная турбина с аксиальным прохождением потока содержит ряд отдельно устанавливаемых направляющих лопаток, выполненных с возможностью вращения при помощи поворотного вала, установленного на подшипниках в корпусе. Хорда направляющих лопаток меньше, чем наибольший диаметр соответствующего поворотного вала. Если рассматривать в осевом направлении, профиль каждой направляющей лопатки находится полностью внутри радиально внешнего контура соответствующего поворотного вала. Таким образом, появляется возможность выполнить как монолит направляющую лопатку с соответствующим поворотным валом и качающийся рычаг. Созданная таким образом конструктивная единица может помещаться в корпус и выниматься из него.The gas injection turbine with axial flow contains a series of separately mounted guide vanes, made rotatable by means of a rotary shaft mounted on bearings in the housing. The chord of the guide vanes is smaller than the largest diameter of the corresponding rotary shaft. When viewed in the axial direction, the profile of each guide vane is completely inside the radially outer contour of the respective rotary shaft. Thus, it is possible to perform as a monolith guide vanes with the corresponding rotary shaft and swing arm. The structural unit thus created can be placed in the housing and removed from it.
RU94009834A 1993-03-25 1994-03-24 Gas delivery radial flow turbine RU2125164C1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4309636A DE4309636C2 (en) 1993-03-25 1993-03-25 Radially flow-through turbocharger turbine
DEP4309636.0 1993-03-25

Publications (2)

Publication Number Publication Date
RU94009834A true RU94009834A (en) 1995-11-20
RU2125164C1 RU2125164C1 (en) 1999-01-20

Family

ID=6483776

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94009834A RU2125164C1 (en) 1993-03-25 1994-03-24 Gas delivery radial flow turbine

Country Status (9)

Country Link
US (1) US5518365A (en)
JP (1) JPH06299860A (en)
KR (1) KR100289549B1 (en)
CN (1) CN1034967C (en)
CZ (1) CZ286599B6 (en)
DE (1) DE4309636C2 (en)
GB (1) GB2276424B (en)
PL (1) PL173354B1 (en)
RU (1) RU2125164C1 (en)

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JP4885118B2 (en) * 2007-12-21 2012-02-29 三菱重工業株式会社 Variable displacement exhaust turbocharger with variable nozzle mechanism
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JP5764962B2 (en) * 2011-02-16 2015-08-19 株式会社Ihi Turbocharger
CN102261344B (en) * 2011-08-31 2013-12-04 无锡杰尔压缩机有限公司 Synchronous regulating device of high-speed centrifugal fan outlet guide vane
RU2621450C2 (en) * 2012-06-19 2017-06-06 Вольво Ластвагнар Аб Device for controlling gas stream, after-treatment system of exhaust gases and propulsion system for means of transport
CN105570196B (en) * 2014-10-31 2019-09-06 特灵国际有限公司 Activate the link mechanism of entry guide vane
DE102017118795A1 (en) * 2017-08-17 2019-02-21 Ihi Charging Systems International Gmbh Adjustable distributor for a turbine, turbine for an exhaust gas turbocharger and turbocharger
US10811884B2 (en) * 2018-03-16 2020-10-20 Uop Llc Consolidation and use of power recovered from a turbine in a process unit
FR3079870B1 (en) * 2018-04-06 2020-03-20 Safran Aircraft Engines DEVICE FOR CONTROLLING AN ANNULAR ROW OF VARIABLE TIMING BLADES FOR AN AIRCRAFT ENGINE
EP3929407A1 (en) * 2020-06-23 2021-12-29 ABB Schweiz AG Modular nozzle ring for a turbine stage of a flow engine
JP2023077852A (en) * 2021-11-25 2023-06-06 株式会社豊田自動織機 Fluid machine for fuel battery
KR20230129756A (en) 2022-03-02 2023-09-11 주식회사 명진아이노리 Clip for rope that doubles as a handle

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