[go: up one dir, main page]

UA27751C2 - Turbo-compressor - Google Patents

Turbo-compressor

Info

Publication number
UA27751C2
UA27751C2 UA93003255A UA93003255A UA27751C2 UA 27751 C2 UA27751 C2 UA 27751C2 UA 93003255 A UA93003255 A UA 93003255A UA 93003255 A UA93003255 A UA 93003255A UA 27751 C2 UA27751 C2 UA 27751C2
Authority
UA
Ukraine
Prior art keywords
compressor
turbo
diffuser
relates
stage compressor
Prior art date
Application number
UA93003255A
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Йоахім Котцур
Йоахим КОТЦУР
Франц-Арно Ріхтер
Франц-Арно Рихтер
Любомир Тураньський
Любомир Тураньский
Original Assignee
Гхх Борзіг Турбомашінен Гмбх
ГХХ Борзиг Турбомашинен ГмбХ
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 Гхх Борзіг Турбомашінен Гмбх, ГХХ Борзиг Турбомашинен ГмбХ filed Critical Гхх Борзіг Турбомашінен Гмбх
Publication of UA27751C2 publication Critical patent/UA27751C2/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/10—Centrifugal pumps for compressing or evacuating
    • F04D17/12—Multi-stage pumps
    • F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44—Fluid-guiding means, e.g. diffusers
    • F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • F04D29/444—Bladed diffusers

Landscapes

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

Abstract

The invention relates to one- or multi-stage compressor with radial design, after the working wheel of which diffuser is placed, with guide blades. The invention can be used in main gas pipelines.
UA93003255A 1992-09-19 1993-09-17 Turbo-compressor UA27751C2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4231452A DE4231452C2 (en) 1992-09-19 1992-09-19 Turbo compressor with an outlet housing for the opposite direction of rotation

Publications (1)

Publication Number Publication Date
UA27751C2 true UA27751C2 (en) 2000-10-16

Family

ID=6468386

Family Applications (1)

Application Number Title Priority Date Filing Date
UA93003255A UA27751C2 (en) 1992-09-19 1993-09-17 Turbo-compressor

Country Status (3)

Country Link
DE (1) DE4231452C2 (en)
RU (1) RU2082021C1 (en)
UA (1) UA27751C2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19654840C2 (en) * 1996-12-23 2001-12-13 Mannesmann Ag Multi-stage turbo compressor
FR2958967B1 (en) * 2010-04-14 2013-03-15 Turbomeca METHOD FOR ADJUSTING TURBOMACHINE AIR FLOW WITH CENTRIFUGAL COMPRESSOR AND DIFFUSER THEREFOR
RU2469214C2 (en) * 2010-07-14 2012-12-10 Общество с ограниченной ответственностью "ТурбоЗАР" Diffuser
JP5010722B2 (en) * 2010-08-31 2012-08-29 三菱重工業株式会社 Centrifugal compressor diffuser and centrifugal compressor provided with the same
RU2631848C1 (en) * 2016-11-22 2017-09-26 федеральное государственное бюджетное образовательное учреждение высшего образования "Национальный исследовательский университет "МЭИ" (ФГБОУ ВО "НИУ "МЭИ") Diffuser

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3333035C2 (en) * 1983-09-13 1987-01-08 Proizvodstvennoe ob"edinenie "Nevskij zavod" imeni V.I. Lenina, Leningrad Centrifugal compressor

Also Published As

Publication number Publication date
RU2082021C1 (en) 1997-06-20
DE4231452C2 (en) 1994-11-03
DE4231452A1 (en) 1994-03-24

Similar Documents

Publication Publication Date Title
UA32572C2 (en) Multi-stage drive multi-shaft turbo-compressor
MX154244A (en) IMPROVEMENTS TO DIFFUSER FOR CENTRIFUGAL TURBOMACHINES, FOR EXAMPLE GAS COMPRESSORS
EP1227217A3 (en) Gas turbine
AU2001261936A1 (en) Blade for axial flow fan
GB1510402A (en) Gas compressor
UA27751C2 (en) Turbo-compressor
PE20020825A1 (en) COMPRESSION APPARATUS
GB2234295B (en) Gas turbine engine compressor assembly
FR2361528A1 (en) RADIAL INLET GAS TURBINE ROTOR WHEEL
SE8503224L (en) centrifugal
DE69002358D1 (en) SCREW COMPRESSOR AND ITS OPERATING PROCEDURE.
EA199800673A1 (en) SPIRAL PRESSURE PIPE
GB1469666A (en) Air compressor assembly
ATE39549T1 (en) LIQUID RING COMPRESSORS.
JPS6487900A (en) Blower
JPS5434161A (en) Turbo refrigerator
AU2003238992A1 (en) A turbine and a component
GB583664A (en) Improvements in and relating to centrifugal compressors
GB701560A (en) Improvements relating to centrifugal compressors
GB871098A (en) Improvements in axial-flow bladed rotor wheels
FR2298021A1 (en) Stator for a multistage radial compressor - has bladed diffuser held on fixed blading stage supports connected together
CA2430448A1 (en) Process gas extraction device for an axial compressor, having a high degree of adaptability to changes in the operating characteristics of the compressor
BR0005338A (en) Process and apparatus for the production of enriched air
IT1024055B (en) Stator for a multistage radial compressor - has bladed diffuser held on fixed blading stage supports connected together
RU98118382A (en) MULTI-STAGE AXIAL COMPRESSOR OF THE AIRCRAFT ENGINE