RU2015129034A - AUXILIARY GASKET IN COMPACT EXECUTION FOR TURBOMACHINE HOUSING - Google Patents

AUXILIARY GASKET IN COMPACT EXECUTION FOR TURBOMACHINE HOUSING Download PDF

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Publication number
RU2015129034A
RU2015129034A RU2015129034A RU2015129034A RU2015129034A RU 2015129034 A RU2015129034 A RU 2015129034A RU 2015129034 A RU2015129034 A RU 2015129034A RU 2015129034 A RU2015129034 A RU 2015129034A RU 2015129034 A RU2015129034 A RU 2015129034A
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RU
Russia
Prior art keywords
housing
sealing element
sealing
fastening
chamfer
Prior art date
Application number
RU2015129034A
Other languages
Russian (ru)
Inventor
Ян ВОЙЛЕ
Original Assignee
Сименс Акциенгезелльшафт
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.)
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Publication date
Application filed by Сименс Акциенгезелльшафт filed Critical Сименс Акциенгезелльшафт
Publication of RU2015129034A publication Critical patent/RU2015129034A/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/086Sealings especially adapted for liquid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/003Preventing or minimising internal leakage of working-fluid, e.g. between stages by packing rings; Mechanical seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/083Sealings especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/002Sealings comprising at least two sealings in succession
    • F16J15/004Sealings comprising at least two sealings in succession forming of recuperation chamber for the leaking fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/02Sealings between relatively-stationary surfaces
    • F16J15/06Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/062Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces characterised by the geometry of the seat
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/40Use of a multiplicity of similar components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/60Fluid transfer
    • F05D2260/602Drainage
    • F05D2260/6022Drainage of leakage having past a seal

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Claims (31)

1. Корпус (1) турбомашины (10) с горшком (2) корпуса и с крышкой (8) корпуса, установленной по общей опорной поверхности (6) на горшке корпуса, а также с установленной по общей опорной поверхности (6) прокладкой (3) для уплотнения общей опорной поверхности (6) с первым уплотнительным элементом (4) и со вторым уплотнительным элементом (5), установленным с радиальным смещением относительно первого уплотнительного элемента (4), причем первый и второй уплотнительные элементы (4, 5) установлены также с аксиальным смещением относительно друг друга,1. The casing (1) of the turbomachine (10) with the pot (2) of the casing and with the cover (8) of the casing installed along the common supporting surface (6) on the casing and also with the gasket (3) installed along the common supporting surface (6) ) for sealing a common abutment surface (6) with a first sealing element (4) and with a second sealing element (5) mounted radially offset relative to the first sealing element (4), the first and second sealing elements (4, 5) being also installed with axial displacement relative to each other, отличающийся тем, чтоcharacterized in that корпус (1) включает в себя контроль (13) промежуточного пространства, отслеживающий для прокладки (3) контрольное пространство (26), образованное по общей опорной поверхности (16) радиально между первым и вторым уплотнительными элементами (4, 5).the housing (1) includes a control (13) of the intermediate space, tracking for the gasket (3) the control space (26) formed radially between the first and second sealing elements (4, 5) along a common supporting surface (16). 2. Корпус (1) по п. 1,2. The housing (1) according to claim 1, отличающийся тем, чтоcharacterized in that первый уплотнительный элемент (4) установлен в первом креплении (14) уплотнительного элемента, а второй уплотнительный элемент (5) - во втором креплении (15) второго уплотнительного элемента, причем первое и второе крепления (14, 15) уплотнительных элементов выполнены в крышке (8) корпуса.the first sealing element (4) is installed in the first fastening (14) of the sealing element, and the second sealing element (5) in the second fastening (15) of the second sealing element, the first and second fastening (14, 15) of the sealing elements are made in the cover ( 8) housing. 3. Корпус (1) по п. 2,3. The housing (1) according to claim 2, отличающийся тем, чтоcharacterized in that первое и/или второе крепление (14, 15) уплотнительного элемента выполнены в виде фаски/фасок на крышке (8) корпуса или что первое крепление (14) уплотнительного элемента выполнено в виде окружной фаски, а второе крепление (15) уплотнительного элемента в виде окружного прямоугольного паза или окружного прямоугольного углубления на крышке (8) корпуса.the first and / or second fastening (14, 15) of the sealing element is made in the form of a chamfer / chamfer on the cover (8) of the housing or that the first fastening (14) of the sealing element is made in the form of a circumferential chamfer, and the second fastening (15) of the sealing element in the form circumferential rectangular groove or circumferential rectangular recess on the cover (8) of the housing. 4. Корпус (1) по п. 1,4. The housing (1) according to claim 1, отличающийся тем, чтоcharacterized in that уплотнительными элементами (4, 5) являются круглые кольца и/или уплотнительные манжеты (Cupseals).the sealing elements (4, 5) are round rings and / or sealing cups (Cupseals). 5. Корпус (1) по п. 1,5. The housing (1) according to claim 1, отличающийся тем, чтоcharacterized in that первый уплотнительный элемент (4) установлен радиально за пределами второго уплотнительного элемента (5), и первый уплотнительный элемент (1) является круглым кольцом, а второй уплотнительный элемент (5) - уплотнительной манжетой (Cupseal) (5) или профильным уплотнением.the first sealing element (4) is mounted radially outside the second sealing element (5), and the first sealing element (1) is a circular ring, and the second sealing element (5) is a sealing cup (Cupseal) (5) or profile seal. 6. Корпус (1) по п. 1,6. The housing (1) according to claim 1, отличающийся тем, чтоcharacterized in that контроль (13) промежуточного пространства включает выполненную на горшке (2) корпуса окружную фаску (27), ограничивающую контрольное пространство (26), которая выполнена на горшке (2) корпуса таким образом, чтобы она радиально и аксиально была расположена по общей опорной поверхности (6) между первым и вторым уплотнительными элементами (4, 5).the control (13) of the intermediate space includes a circumferential chamfer (27) made on the body pot (2), bounding the control space (26), which is made on the body pot (2) so that it is radially and axially located on a common supporting surface ( 6) between the first and second sealing elements (4, 5). 7. Корпус (1) по п. 6,7. The housing (1) according to claim 6, отличающийся тем, чтоcharacterized in that контроль (13) промежуточного пространства включает заканчивающееся в контрольном пространстве (26) в области фаски (27) высверленное отверстие (28), причем высверленное отверстие (28) выполнено перпендикулярно фаске (27).control (13) of the intermediate space includes a drilled hole (28) ending in the control space (26) in the chamfer region (27), and the drilled hole (28) is perpendicular to the chamfer (27). 8. Корпус (1) по п. 1,8. The housing (1) according to claim 1, отличающийся тем, чтоcharacterized in that контроль (13) промежуточного пространства включает выполненную на наружной окружающей поверхности (17) горшка (2) корпуса, в частности, отфрезерованную резьбовую поверхность (7) для привинчивания к горшку (2) корпуса соединительного элемента для контроля (13) промежуточного пространства.the control (13) of the intermediate space includes a housing pot (2) made on the outer surrounding surface (17), in particular, a milled threaded surface (7) for screwing the connecting element element to the pot (2) for controlling the intermediate space (13). 9. Корпус (1) по п. 1,9. The housing (1) according to claim 1, отличающийся установленной в горшке (2) корпуса спиральной вставкой (7), имеющей общую радиальную опорную поверхность (31) с горшком (2) корпуса и крышкой (8) корпуса.characterized by a spiral insert (7) installed in the body pot (2) of the housing, having a common radial abutment surface (31) with the body pot (2) and the housing cover (8). 10. Корпус (1) по п. 9,10. The housing (1) according to claim 9, отличающийся тем, чтоcharacterized in that один (5) из двух уплотнительных элементов (4, 5), в частности, радиально внутренний уплотнительный элемент (5) из двух уплотнительных элементов (4, 5), установлен на наружной окружающей поверхности (21) спиральной вставки (7).one (5) of two sealing elements (4, 5), in particular, a radially inner sealing element (5) of two sealing elements (4, 5), is installed on the outer surrounding surface (21) of the spiral insert (7). 11. Корпус (1) по одному из пп. 1-10,11. The housing (1) according to one of paragraphs. 1-10, используемый в компрессоре (10), в частности, в одновальном или приводном турбокомпрессоре (10), кроме того, в частности, для использования диоксида углерода, в расширителе или в турбине.used in the compressor (10), in particular in a single-shaft or drive turbocharger (10), in addition, in particular, for the use of carbon dioxide, in an expander or in a turbine.
RU2015129034A 2012-12-17 2013-12-17 AUXILIARY GASKET IN COMPACT EXECUTION FOR TURBOMACHINE HOUSING RU2015129034A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102012223462.4 2012-12-17
DE102012223462A DE102012223462B3 (en) 2012-12-17 2012-12-17 Housing of fluid flow machine e.g. compressor, has seal that is arranged to seal the common contact surface in which the sealing elements are arranged, and sealing elements that are arranged axially relative to each other
PCT/EP2013/076875 WO2014095843A1 (en) 2012-12-17 2013-12-17 Compact backup seal for a turbomachine housing

Publications (1)

Publication Number Publication Date
RU2015129034A true RU2015129034A (en) 2017-01-25

Family

ID=48794828

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015129034A RU2015129034A (en) 2012-12-17 2013-12-17 AUXILIARY GASKET IN COMPACT EXECUTION FOR TURBOMACHINE HOUSING

Country Status (5)

Country Link
EP (1) EP2906785A1 (en)
CN (1) CN104884742A (en)
DE (1) DE102012223462B3 (en)
RU (1) RU2015129034A (en)
WO (1) WO2014095843A1 (en)

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DE102014203466B4 (en) * 2014-02-26 2017-03-30 Siemens Aktiengesellschaft Housing of a fluid energy machine
EP3594506A1 (en) 2018-07-12 2020-01-15 Siemens Aktiengesellschaft Contour ring for a compressor
DE102018215280B4 (en) 2018-09-07 2023-03-16 Volkswagen Aktiengesellschaft Arrangement of a fluid-carrying element directly or indirectly on a housing of a compressor
DE102018128255A1 (en) * 2018-11-12 2020-05-14 Ebm-Papst Landshut Gmbh Blower device

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US3144035A (en) * 1963-02-01 1964-08-11 Nat Res Corp High vacuum system
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CH662865A5 (en) * 1984-03-19 1987-10-30 Sulzer Ag POT HOUSING FOR A CENTRIFUGAL PUMP.
DE4127300A1 (en) * 1991-06-15 1993-02-25 Albrecht Dipl Ing Kayser COMBINED SLIDE AND SPIRAL GROOVE AXIAL SHAFT SEAL
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DE102009012038B4 (en) * 2009-03-10 2014-10-30 Siemens Aktiengesellschaft Shaft seal for a turbomachine
DE102009058411A1 (en) * 2009-12-16 2011-06-22 BorgWarner Inc., Mich. turbocharger
WO2011076704A1 (en) * 2009-12-22 2011-06-30 Basf Se Sealing assembly for a process gas turbo-compressor
CN201771836U (en) * 2010-07-07 2011-03-23 上海连成(集团)有限公司 Novel pump housing sealing structure

Also Published As

Publication number Publication date
CN104884742A (en) 2015-09-02
EP2906785A1 (en) 2015-08-19
WO2014095843A1 (en) 2014-06-26
DE102012223462B3 (en) 2013-08-08

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Effective date: 20161219