DE3770617D1 - Abgasstutzen fuer eine gasturbine mit einem lochdiffusor. - Google Patents

Abgasstutzen fuer eine gasturbine mit einem lochdiffusor.

Info

Publication number
DE3770617D1
DE3770617D1 DE8787118618T DE3770617T DE3770617D1 DE 3770617 D1 DE3770617 D1 DE 3770617D1 DE 8787118618 T DE8787118618 T DE 8787118618T DE 3770617 T DE3770617 T DE 3770617T DE 3770617 D1 DE3770617 D1 DE 3770617D1
Authority
DE
Germany
Prior art keywords
gas turbine
exhaust manifold
hole diffuser
diffuser
hole
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.)
Expired - Fee Related
Application number
DE8787118618T
Other languages
English (en)
Inventor
Jacques Rigault
Pierre Bonnet
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.)
Alstom Holdings SA
Original Assignee
Vibrachoc SAS
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 Vibrachoc SAS filed Critical Vibrachoc SAS
Application granted granted Critical
Publication of DE3770617D1 publication Critical patent/DE3770617D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
    • F15D1/00—Influencing flow of fluids
    • F15D1/02—Influencing flow of fluids in pipes or conduits
    • F15D1/04—Arrangements of guide vanes in pipe elbows or duct bends; Construction of pipe conduit elements for elbows with respect to flow, e.g. for reducing losses of flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2200/00—Mathematical features
    • F05D2200/20—Special functions
    • F05D2200/23—Logarithm
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/19—Two-dimensional machined; miscellaneous
    • F05D2250/191—Two-dimensional machined; miscellaneous perforated

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
  • Lasers (AREA)
  • Jet Pumps And Other Pumps (AREA)
DE8787118618T 1986-12-18 1987-12-15 Abgasstutzen fuer eine gasturbine mit einem lochdiffusor. Expired - Fee Related DE3770617D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8617760A FR2612250B1 (fr) 1986-12-18 1986-12-18 Dispositif d'echappement d'une turbine a gaz, comportant un diffuseur de jets

Publications (1)

Publication Number Publication Date
DE3770617D1 true DE3770617D1 (de) 1991-07-11

Family

ID=9342054

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8787118618T Expired - Fee Related DE3770617D1 (de) 1986-12-18 1987-12-15 Abgasstutzen fuer eine gasturbine mit einem lochdiffusor.

Country Status (9)

Country Link
US (1) US4748805A (de)
EP (1) EP0276448B1 (de)
JP (1) JPH0681904B2 (de)
CN (1) CN1007442B (de)
BR (1) BR8706890A (de)
CA (1) CA1279580C (de)
DE (1) DE3770617D1 (de)
FR (1) FR2612250B1 (de)
IN (1) IN170768B (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2261474B (en) * 1991-10-23 1994-06-22 Ruston Gas Turbines Ltd Gas turbine exhaust system
US5569196A (en) * 1992-07-21 1996-10-29 Advanced Cardiovascular Systems, Inc. Trackable intravascular catheter
DE4422700A1 (de) * 1994-06-29 1996-01-04 Abb Management Ag Diffusor für Turbomaschine
US5632142A (en) * 1995-02-15 1997-05-27 Surette; Robert G. Stationary gas turbine power system and related method
US6851514B2 (en) * 2002-04-15 2005-02-08 Air Handling Engineering Ltd. Outlet silencer and heat recovery structures for gas turbine
US7648564B2 (en) * 2006-06-21 2010-01-19 General Electric Company Air bypass system for gas turbine inlet
US7707818B2 (en) * 2008-02-11 2010-05-04 General Electric Company Exhaust stacks and power generation systems for increasing gas turbine power output
US8511984B2 (en) * 2009-10-16 2013-08-20 General Electric Company Gas turbine engine exhaust diffuser and collector
US20110236201A1 (en) * 2010-03-23 2011-09-29 Sumedhkumar Vyankatesh Shende Method and apparatus for radial exhaust gas turbine
CN101893021B (zh) * 2010-08-01 2012-09-26 王政玉 一种产生有序流的装置
JP5951187B2 (ja) * 2011-03-29 2016-07-13 三菱重工業株式会社 タービン排気構造及びガスタービン
ITFI20120221A1 (it) * 2012-10-22 2014-04-23 Nuovo Pignone Srl "exhaust gas collector and gas turbine"
US20140348647A1 (en) * 2013-05-24 2014-11-27 Solar Turbines Incorporated Exhaust diffuser for a gas turbine engine exhaust system
US11162424B2 (en) * 2013-10-11 2021-11-02 Reaction Engines Ltd Heat exchangers
GB2600759A (en) * 2020-11-10 2022-05-11 Reaction Engines Ltd Guiding array

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3185252A (en) * 1957-07-29 1965-05-25 C W Lemmerman Inc Jet engine noise attenuator
US3195678A (en) * 1962-02-23 1965-07-20 Industrial Acoustics Co Aerodynamic coupling for jet noise suppressors
FR2059877A5 (de) * 1970-07-30 1971-06-04 Prvni Brnenska Strojirna
US3688865A (en) * 1970-11-17 1972-09-05 Cloyd D Smith Jet engine noise suppressor
US3692140A (en) * 1971-04-05 1972-09-19 Cloyd D Smith Exhaust noise suppressor for gas turbine
US4180141A (en) * 1975-11-24 1979-12-25 Judd Frederick V H Distributor for gas turbine silencers
US4244441A (en) * 1979-07-31 1981-01-13 The Garrett Corporation Broad band acoustic attenuator

Also Published As

Publication number Publication date
FR2612250B1 (fr) 1991-04-05
CN1007442B (zh) 1990-04-04
US4748805A (en) 1988-06-07
BR8706890A (pt) 1988-07-26
CA1279580C (fr) 1991-01-29
JPS63219825A (ja) 1988-09-13
EP0276448B1 (de) 1991-06-05
EP0276448A1 (de) 1988-08-03
CN87101162A (zh) 1988-06-29
JPH0681904B2 (ja) 1994-10-19
FR2612250A1 (fr) 1988-09-16
IN170768B (de) 1992-05-16

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Legal Events

Date Code Title Description
8327 Change in the person/name/address of the patent owner

Owner name: GEC ALSTHOM S.A., PARIS, FR

8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee