FR801190A - Dispositif de réglage de la combustion dans un foyer surcomprimé par turbosoufflante - Google Patents

Dispositif de réglage de la combustion dans un foyer surcomprimé par turbosoufflante

Info

Publication number
FR801190A
FR801190A FR801190DA FR801190A FR 801190 A FR801190 A FR 801190A FR 801190D A FR801190D A FR 801190DA FR 801190 A FR801190 A FR 801190A
Authority
FR
France
Prior art keywords
combustion
turbofan
adjustment device
combustion chamber
chamber supercharged
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
Application number
Other languages
English (en)
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.)
Rateau SA
Original Assignee
Rateau SA
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 Rateau SA filed Critical Rateau SA
Application granted granted Critical
Publication of FR801190A publication Critical patent/FR801190A/fr
Expired 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
    • 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
    • F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
FR801190D 1935-04-29 1935-04-29 Dispositif de réglage de la combustion dans un foyer surcomprimé par turbosoufflante Expired FR801190A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR801190T 1935-04-29

Publications (1)

Publication Number Publication Date
FR801190A true FR801190A (fr) 1936-07-29

Family

ID=9242454

Family Applications (1)

Application Number Title Priority Date Filing Date
FR801190D Expired FR801190A (fr) 1935-04-29 1935-04-29 Dispositif de réglage de la combustion dans un foyer surcomprimé par turbosoufflante

Country Status (1)

Country Link
FR (1) FR801190A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000065201A1 (fr) * 1999-04-27 2000-11-02 Pratt & Whitney Canada Corp. Refroidissement de turbine haute pression pour moteur a turbine a gaz

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000065201A1 (fr) * 1999-04-27 2000-11-02 Pratt & Whitney Canada Corp. Refroidissement de turbine haute pression pour moteur a turbine a gaz
US6227801B1 (en) 1999-04-27 2001-05-08 Pratt & Whitney Canada Corp. Turbine engine having improved high pressure turbine cooling

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