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EP0972945A3 - Gear driven compressor - Google Patents

Gear driven compressor Download PDF

Info

Publication number
EP0972945A3
EP0972945A3 EP99113317A EP99113317A EP0972945A3 EP 0972945 A3 EP0972945 A3 EP 0972945A3 EP 99113317 A EP99113317 A EP 99113317A EP 99113317 A EP99113317 A EP 99113317A EP 0972945 A3 EP0972945 A3 EP 0972945A3
Authority
EP
European Patent Office
Prior art keywords
gas
jacket
compressor stage
gas cooler
pipe
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
EP99113317A
Other languages
German (de)
French (fr)
Other versions
EP0972945B1 (en
EP0972945A2 (en
Inventor
Heiko Dr. Ing. Sandstede
Anton Castor
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Atlas Copco Energas GmbH
Original Assignee
Atlas Copco Energas GmbH
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 Atlas Copco Energas GmbH filed Critical Atlas Copco Energas GmbH
Publication of EP0972945A2 publication Critical patent/EP0972945A2/en
Publication of EP0972945A3 publication Critical patent/EP0972945A3/en
Application granted granted Critical
Publication of EP0972945B1 publication Critical patent/EP0972945B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F9/026—Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
    • F04D25/163—Combinations of two or more pumps ; Producing two or more separate gas flows driven by a common gearing arrangement
    • 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
    • F04D29/58—Cooling; Heating; Diminishing heat transfer
    • F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/16—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation
    • F28D7/163—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation with conduit assemblies having a particular shape, e.g. square or annular; with assemblies of conduits having different geometrical features; with multiple groups of conduits connected in series or parallel and arranged inside common casing
    • F28D7/1638—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation with conduit assemblies having a particular shape, e.g. square or annular; with assemblies of conduits having different geometrical features; with multiple groups of conduits connected in series or parallel and arranged inside common casing with particular pattern of flow or the heat exchange medium flowing inside the conduits assemblies, e.g. change of flow direction from one conduit assembly to another one
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings

Landscapes

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

Abstract

Gegenstand der Erfindung ist eine Getriebe-Turbokompressoranlage mit einer Antriebsmaschine (1), mindestens einer radialen Verdichterstufe (2) und mindestens einem Gaskühler (3) zur Zwischenkühlung oder Nachkühlung des verdichteten Gasstromes. Die Antriebsmaschine (1), die Verdichterstufe (2) und der Gaskühler (3) sind in einem gemeinsamen Maschinengestell angeordnet. Der Gaskühler (3) besteht aus einem liegend angeordneten zylindrischen Mantel (8) und einem Rohrbündel aus parallelen, von einer Kühlflüssigkeit durchströmbaren Rohren und ist durch eine Rohrleitung (4) mit mindestens einer Verdichterstufe (2) verbunden. Der zylindrische Mantel (8) des Gaskühlers weist eine Gaseintrittsöffnung und eine Gasaustrittsöffnung auf, die in einem fest vorgegebenen Abstand zueinander nahe den Rohrböden angeordnet sind. Erfindungsgemäß ist zumindest ein Abschnitt des Mantels (8) von einem Außenmantel (11) umgeben, wobei der Außenmantel (11) und der die Rohre umschließende Mantel (8) einen gasdurchströmten Ringraum begrenzen. An den Außenmantel (11) ist zumindest ein Rohrstutzen (13) für den Gaseintritt oder Gasaustritt angeschlossen, dessen Position variabel nach Maßgabe der den Gaskühler (3) mit einer Verdichterstufe (2) verbindenden Rohrleitung (4) festlegbar ist.

Figure 00000001
The invention relates to a geared turbo compressor system with a drive machine (1), at least one radial compressor stage (2) and at least one gas cooler (3) for intermediate cooling or aftercooling of the compressed gas stream. The drive machine (1), the compressor stage (2) and the gas cooler (3) are arranged in a common machine frame. The gas cooler (3) consists of a cylindrical jacket (8) arranged horizontally and a tube bundle made of parallel tubes through which a cooling liquid can flow and is connected by a pipe (4) to at least one compressor stage (2). The cylindrical jacket (8) of the gas cooler has a gas inlet opening and a gas outlet opening which are arranged at a fixed predetermined distance from one another near the tube sheets. According to the invention, at least a section of the jacket (8) is surrounded by an outer jacket (11), the outer jacket (11) and the jacket (8) surrounding the pipes delimiting an annular space through which gas flows. At least one pipe socket (13) for the gas inlet or gas outlet is connected to the outer jacket (11), the position of which can be variably determined in accordance with the pipe (4) connecting the gas cooler (3) to a compressor stage (2).
Figure 00000001
EP99113317A 1998-07-17 1999-07-09 Gear driven compressor Expired - Lifetime EP0972945B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19832222 1998-07-17
DE19832222A DE19832222A1 (en) 1998-07-17 1998-07-17 Gas cooler for installation in a gearbox turbo compressor system

Publications (3)

Publication Number Publication Date
EP0972945A2 EP0972945A2 (en) 2000-01-19
EP0972945A3 true EP0972945A3 (en) 2002-03-06
EP0972945B1 EP0972945B1 (en) 2005-03-02

Family

ID=7874435

Family Applications (1)

Application Number Title Priority Date Filing Date
EP99113317A Expired - Lifetime EP0972945B1 (en) 1998-07-17 1999-07-09 Gear driven compressor

Country Status (3)

Country Link
EP (1) EP0972945B1 (en)
JP (1) JP3524437B2 (en)
DE (2) DE19832222A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007020145A1 (en) * 2006-05-23 2007-11-29 Bayer Materialscience Ag Apparatus for cooling gases (quench) to form a corrosive condensate
DE102009039751B4 (en) * 2009-09-02 2011-05-12 Atlas Copco Energas Gmbh Compressed gas cooler, in particular for compressors

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3937276A (en) * 1974-05-21 1976-02-10 Gordon Smith & Co., Inc. Aftercooler for air compressor
US4010016A (en) * 1975-05-27 1977-03-01 Ingersoll-Rand Company Gas compressor
EP0770782A1 (en) * 1995-10-25 1997-05-02 Ishikawajima-Harima Heavy Industries Co., Ltd. Turbo compressor

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3061810U (en) 1999-03-03 1999-09-24 誠一 丹 Distilled water cooling device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3937276A (en) * 1974-05-21 1976-02-10 Gordon Smith & Co., Inc. Aftercooler for air compressor
US4010016A (en) * 1975-05-27 1977-03-01 Ingersoll-Rand Company Gas compressor
EP0770782A1 (en) * 1995-10-25 1997-05-02 Ishikawajima-Harima Heavy Industries Co., Ltd. Turbo compressor

Also Published As

Publication number Publication date
JP3524437B2 (en) 2004-05-10
DE19832222A1 (en) 2000-01-20
JP2000045946A (en) 2000-02-15
EP0972945B1 (en) 2005-03-02
EP0972945A2 (en) 2000-01-19
DE59911677D1 (en) 2005-04-07

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