RU92004337A - EXHAUST SYSTEM FOR EXHAUST GASES - Google Patents

EXHAUST SYSTEM FOR EXHAUST GASES

Info

Publication number
RU92004337A
RU92004337A RU92004337/06A RU92004337A RU92004337A RU 92004337 A RU92004337 A RU 92004337A RU 92004337/06 A RU92004337/06 A RU 92004337/06A RU 92004337 A RU92004337 A RU 92004337A RU 92004337 A RU92004337 A RU 92004337A
Authority
RU
Russia
Prior art keywords
pipe
exhaust
outlet pipe
valve
junction
Prior art date
Application number
RU92004337/06A
Other languages
Russian (ru)
Other versions
RU2094619C1 (en
Inventor
Р.К. Филип
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 NL9101782A external-priority patent/NL9101782A/en
Application filed filed Critical
Publication of RU92004337A publication Critical patent/RU92004337A/en
Application granted granted Critical
Publication of RU2094619C1 publication Critical patent/RU2094619C1/en

Links

Claims (1)

Использование: в выпускных системах для выхлопных газов газовых турбин или подобных установок. Сущность изобретения: один конец выпускной трубы соединен с газовой турбиной или подобной установкой, а другой конец - с теплообменником. Отводная труба, расположенная поперек выпускной трубы, соединена с последней. Рядом с местом соединения отводной трубы с выпускной трубой предусмотрен клапан, выполненный с возможностью поворота между первым положением, в котором он закрывает конец отводной трубы, соединяющий ее с выпускной трубой, и вторым положением, в котором выпускная труба закрывается ниже по потоку от места соединения отводной трубы с выпускной трубой. Кроме того, предусмотрена по крайней мере одна направляющая лопатка, которая во втором положении клапана расположена вверх по потоку относительно клапана и по крайней мере частично внутри выпускной трубы и занимает область от верхней по потоку кромки вниз по потоку в направлении отводной трубы. Направляющая лопатка выполнена с возможностью регулировки вплоть до положения внутри отводной трубы, обеспечивая регулировку клапана в пределах от второго положения до первого положения.Usage: in exhaust systems for exhaust gases of gas turbines or similar installations. The inventive one end of the exhaust pipe is connected to a gas turbine or similar installation, and the other end with a heat exchanger. A branch pipe located across the discharge pipe is connected to the latter. Near the junction of the bypass pipe with the outlet pipe, a valve is provided that is rotatable between the first position in which it closes the end of the outlet pipe connecting it to the outlet pipe and the second position in which the outlet pipe closes downstream from the junction of the outlet pipe pipes with exhaust pipe. In addition, at least one guide vane is provided, which in the second position of the valve is located upstream of the valve and at least partially inside the exhaust pipe and occupies an area from the upstream edge downstream in the direction of the discharge pipe. The guide vane is configured to be adjusted up to a position within the outlet pipe, providing valve adjustment ranging from a second position to a first position.
RU9292004337A 1991-10-24 1992-10-23 Exhaust gas outlet system RU2094619C1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NL9101782A NL9101782A (en) 1991-10-24 1991-10-24 EXHAUST SYSTEM FOR COMBUSTION GASES.
NL9101782 1991-10-24

Publications (2)

Publication Number Publication Date
RU92004337A true RU92004337A (en) 1994-12-30
RU2094619C1 RU2094619C1 (en) 1997-10-27

Family

ID=19859843

Family Applications (1)

Application Number Title Priority Date Filing Date
RU9292004337A RU2094619C1 (en) 1991-10-24 1992-10-23 Exhaust gas outlet system

Country Status (8)

Country Link
US (1) US5503221A (en)
EP (1) EP0538918B1 (en)
AT (1) ATE130907T1 (en)
CA (1) CA2078159C (en)
DE (1) DE69206383T2 (en)
ES (1) ES2082352T3 (en)
NL (1) NL9101782A (en)
RU (1) RU2094619C1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4226525C1 (en) * 1992-08-11 1993-08-19 Stober + Morlock Waermekraft Gmbh, 4350 Recklinghausen, De
DE19541890A1 (en) * 1995-11-10 1997-05-15 Asea Brown Boveri Gas turbine group
US6257155B1 (en) * 2000-10-16 2001-07-10 Alstom Power N.V. Curved blade by-pass damper with flow control
EP2224101A1 (en) * 2009-02-27 2010-09-01 Siemens Aktiengesellschaft Gas turbine
US20110154680A1 (en) * 2009-12-30 2011-06-30 Daewoo Electronics Corporation Dryer having circulation apparatus and control method thereof
EP3006683B1 (en) * 2014-10-08 2017-08-02 Ansaldo Energia Switzerland AG Diverting system

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2227666A (en) * 1936-12-10 1941-01-07 Bbc Brown Boveri & Cie Starting up system for heat producing and consuming plants
US2713245A (en) * 1952-11-24 1955-07-19 Austin Motor Co Ltd Internal combustion turbine power plants with regenerative exhaust treatment system
DE1035977B (en) * 1954-05-25 1958-08-07 Napier & Son Ltd Two-way valve for a hot gas line connected downstream of the gas turbine of a gas generator designed as a gas turbine system
US2945346A (en) * 1954-10-04 1960-07-19 Republic Aviat Corp Reverse thrust brake
GB901538A (en) * 1959-05-22 1962-07-18 Rolls Royce Improved fluid flow control valve
US3270775A (en) * 1963-04-09 1966-09-06 Gen Electric Diverter valve assembly
US3220775A (en) * 1964-05-27 1965-11-30 Gar Wood Ind Inc Wheel and tire trim construction
US3805884A (en) * 1973-01-08 1974-04-23 Vogt H Machine Co Inc Damper means for controlling the flow of gas to a heat exchanger
US3837411A (en) * 1973-11-21 1974-09-24 Gen Electric Diverter valve for a gas turbine with an augmenter
DE3206626A1 (en) * 1982-02-24 1983-09-01 Kraftwerk Union AG, 4330 Mülheim EXHAUST CHANNEL FOR GAS TURBINES
US4753392A (en) * 1984-11-02 1988-06-28 United Technologies Corporation Two dimensional gas turbine engine exhaust nozzle
US4760960A (en) * 1987-05-22 1988-08-02 United Technologies Corporation Linkage for area controlled, thrust vectoring vane cascade
US4821507A (en) * 1987-05-29 1989-04-18 Bachmann Industries, Inc. Gas flow diverter
DE3831062A1 (en) * 1988-09-13 1990-03-15 Stober & Morlock DEVICE BEHIND A GAS TURBINE
GB8913735D0 (en) * 1989-06-15 1989-08-02 Grovag Grossventiltech Isolators
GB9020297D0 (en) * 1990-09-17 1990-10-31 Grovag Grossventiltech Diverter valves
US5186205A (en) * 1991-04-29 1993-02-16 Bachmann Industries, Inc. Valves for use in controlling the flow of a gas stream through ducts of large cross sectional areas

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