FR1035814A - Perfectionnements apportés aux turbines à gaz - Google Patents

Perfectionnements apportés aux turbines à gaz

Info

Publication number
FR1035814A
FR1035814A FR1035814DA FR1035814A FR 1035814 A FR1035814 A FR 1035814A FR 1035814D A FR1035814D A FR 1035814DA FR 1035814 A FR1035814 A FR 1035814A
Authority
FR
France
Prior art keywords
gas turbines
turbines
gas
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR1035814A publication Critical patent/FR1035814A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • 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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/185—Liquid cooling
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/22—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants movable, e.g. to an inoperative position; adjustable, e.g. self-adjusting
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1035814D 1950-04-14 1951-04-10 Perfectionnements apportés aux turbines à gaz Expired FR1035814A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1035814X 1950-04-14

Publications (1)

Publication Number Publication Date
FR1035814A true FR1035814A (fr) 1953-08-31

Family

ID=10869480

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1035814D Expired FR1035814A (fr) 1950-04-14 1951-04-10 Perfectionnements apportés aux turbines à gaz

Country Status (1)

Country Link
FR (1) FR1035814A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2940252A (en) * 1956-02-07 1960-06-14 Boeing Co Gas stream thrust reaction propulsion engines with noise-suppression and thrust-reversing nozzle means
EP0315486A2 (fr) * 1987-11-05 1989-05-10 General Electric Company Structure de châssis pour un réacteur d'avion

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2940252A (en) * 1956-02-07 1960-06-14 Boeing Co Gas stream thrust reaction propulsion engines with noise-suppression and thrust-reversing nozzle means
EP0315486A2 (fr) * 1987-11-05 1989-05-10 General Electric Company Structure de châssis pour un réacteur d'avion
EP0315486A3 (en) * 1987-11-05 1990-01-17 General Electric Company Aircraft engine frame construction
US5020318A (en) * 1987-11-05 1991-06-04 General Electric Company Aircraft engine frame construction

Similar Documents

Publication Publication Date Title
FR1033849A (fr) Perfectionnements aux turbines à gaz
FR57426E (fr) Perfectionnements aux turbines à gaz
FR1029366A (fr) Turbine à gaz
FR1122205A (fr) Perfectionnements apportés aux turbines à gaz, notamment aux turbines axipètes
FR1062311A (fr) Perfectionnements aux turbines à gaz
FR1006338A (fr) Perfectionnements aux turbines à gaz
FR1059635A (fr) Perfectionnements aux turbines à gaz
FR1076479A (fr) Turbine à gaz
FR1114538A (fr) Perfectionnements aux turbines à gaz
FR1007743A (fr) Turbine à gaz
FR1035814A (fr) Perfectionnements apportés aux turbines à gaz
FR1058197A (fr) Perfectionnements apportés aux installations avec turbines à gaz
FR995175A (fr) Perfectionnements aux turbines à gaz
FR1066103A (fr) Perfectionnements apportés aux turbines à gaz
FR935236A (fr) Perfectionnements aux turbines à gaz
FR1025463A (fr) Perfectionnements apportés aux turbines axiales à gaz
FR1006585A (fr) Perfectionnements aux turbines à gaz
FR1062654A (fr) Perfectionnements aux turbines à gaz
FR1046175A (fr) Perfectionnements aux turbines à gaz
FR1110874A (fr) Perfectionnements aux turbines à gaz
FR1069330A (fr) Perfectionnements aux turbines à gaz
FR945342A (fr) Perfectionnements aux turbines à gaz
FR1018527A (fr) Perfectionnements apportés aux chaudières à gaz
FR1033951A (fr) Turbine à gaz
FR1043148A (fr) Perfectionnements apportés aux installations avec turbines à gaz