FR3052146B1 - Ensemble comprenant une turbomachine avec compresseur et son procede de fonctionnement - Google Patents

Ensemble comprenant une turbomachine avec compresseur et son procede de fonctionnement Download PDF

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Publication number
FR3052146B1
FR3052146B1 FR1754735A FR1754735A FR3052146B1 FR 3052146 B1 FR3052146 B1 FR 3052146B1 FR 1754735 A FR1754735 A FR 1754735A FR 1754735 A FR1754735 A FR 1754735A FR 3052146 B1 FR3052146 B1 FR 3052146B1
Authority
FR
France
Prior art keywords
compressor
turbomachine
assembly including
operating procedure
leakage current
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.)
Active
Application number
FR1754735A
Other languages
English (en)
Other versions
FR3052146A1 (fr
Inventor
Steffen Poggel
Sven Schmidt
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.)
Diehl Aerospace GmbH
Original Assignee
Diehl Aerospace 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 Diehl Aerospace GmbH filed Critical Diehl Aerospace GmbH
Publication of FR3052146A1 publication Critical patent/FR3052146A1/fr
Application granted granted Critical
Publication of FR3052146B1 publication Critical patent/FR3052146B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/203—Adaptations of gas-turbine plants for driving vehicles the vehicles being waterborne vessels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/601—Fluid transfer using an ejector or a jet pump
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel Cell (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne un ensemble (1) comprenant une turbomachine (2) avec un compresseur (3) présentant une sortie (7) et une conduite d'air de prélèvement (9) pouvant être parcourue par un courant de fuite, reliée à la sortie (7) du compresseur (3) par l'intermédiaire d'une vanne réglable (8) pour amener le courant de fuite à une unité. Ensemble caractérisé en ce que l'unité est réalisée sous la forme d'une pompe pouvant être entraînée par le courant de fuite, sous la forme d'une pompe à jet (10) ou d'un ventilateur. L'invention concerne en outre un procédé de fonctionnement de l'ensemble (1).
FR1754735A 2016-06-02 2017-05-30 Ensemble comprenant une turbomachine avec compresseur et son procede de fonctionnement Active FR3052146B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102016006764.0A DE102016006764B4 (de) 2016-06-02 2016-06-02 Anordnung, umfassend eine Turbomaschine und zugehöriges Betriebsverfahren

Publications (2)

Publication Number Publication Date
FR3052146A1 FR3052146A1 (fr) 2017-12-08
FR3052146B1 true FR3052146B1 (fr) 2020-10-30

Family

ID=60327522

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1754735A Active FR3052146B1 (fr) 2016-06-02 2017-05-30 Ensemble comprenant une turbomachine avec compresseur et son procede de fonctionnement

Country Status (5)

Country Link
US (1) US20170350317A1 (fr)
BR (1) BR102017010753A2 (fr)
CA (1) CA2967314A1 (fr)
DE (1) DE102016006764B4 (fr)
FR (1) FR3052146B1 (fr)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3454239A (en) 1967-04-05 1969-07-08 Peter J Frey Counterflow jet flap
US5137230A (en) 1991-06-04 1992-08-11 General Electric Company Aircraft gas turbine engine bleed air energy recovery apparatus
US6979508B2 (en) 2003-11-12 2005-12-27 Ener 1 Inc. Fuel cell with integrated feedback control
US9297316B2 (en) 2011-11-23 2016-03-29 General Electric Company Method and apparatus for optimizing the operation of a turbine system under flexible loads
US8967528B2 (en) 2012-01-24 2015-03-03 The Boeing Company Bleed air systems for use with aircrafts and related methods
DE102012002131B4 (de) 2012-02-03 2021-07-29 Airbus Operations Gmbh Notfallversorgungssystem für ein Verkehrsmittel, Verfahren zum Bereitstellen von elektrischer Leistung und zum Unterdrücken von Feuer und Verkehrsmittel mit einem Notfallversorgungssystem

Also Published As

Publication number Publication date
US20170350317A1 (en) 2017-12-07
DE102016006764B4 (de) 2024-06-27
FR3052146A1 (fr) 2017-12-08
CA2967314A1 (fr) 2017-12-02
DE102016006764A1 (de) 2017-12-07
BR102017010753A2 (pt) 2017-12-19

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