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FR924012A - Further development of combustion turbines - Google Patents

Further development of combustion turbines

Info

Publication number
FR924012A
FR924012A FR924012DA FR924012A FR 924012 A FR924012 A FR 924012A FR 924012D A FR924012D A FR 924012DA FR 924012 A FR924012 A FR 924012A
Authority
FR
France
Prior art keywords
further development
combustion turbines
turbines
combustion
development
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
French (fr)
Inventor
Leon Beaussart
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.)
CONST AERONAUTIQUES DU CT SOC
Original Assignee
CONST AERONAUTIQUES DU CT SOC
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 CONST AERONAUTIQUES DU CT SOC filed Critical CONST AERONAUTIQUES DU CT SOC
Application granted granted Critical
Publication of FR924012A publication Critical patent/FR924012A/en
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
    • F01D5/12—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
    • F01D5/182—Transpiration cooling
    • F01D5/183—Blade walls being porous
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
FR924012D 1946-02-18 1946-02-18 Further development of combustion turbines Expired FR924012A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR924012T 1946-02-18

Publications (1)

Publication Number Publication Date
FR924012A true FR924012A (en) 1947-07-24

Family

ID=9439102

Family Applications (1)

Application Number Title Priority Date Filing Date
FR924012D Expired FR924012A (en) 1946-02-18 1946-02-18 Further development of combustion turbines

Country Status (1)

Country Link
FR (1) FR924012A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1021644B (en) * 1955-05-18 1957-12-27 Messerschmitt Ag Blade for gas turbines with surface cooling
DE1028388B (en) * 1954-11-25 1958-04-17 Power Jets Res & Dev Ltd Turbine blade
US2970807A (en) * 1957-05-28 1961-02-07 Messerschmitt Ag Rotor blades for gas turbines
US3011760A (en) * 1953-10-20 1961-12-05 Ernst R G Eckert Transpiration cooled turbine blade manufactured from wires
US3836283A (en) * 1972-05-08 1974-09-17 Nat Aerospace Lab Construction of axial-flow turbine blades
EP0146624A1 (en) * 1983-06-20 1985-07-03 Marius A Paul Process of intensification of the thermoenergetical cycle and air jet propulsion engines.
US5122033A (en) * 1990-11-16 1992-06-16 Paul Marius A Turbine blade unit
US5177954A (en) * 1984-10-10 1993-01-12 Paul Marius A Gas turbine engine with cooled turbine blades

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3011760A (en) * 1953-10-20 1961-12-05 Ernst R G Eckert Transpiration cooled turbine blade manufactured from wires
DE1028388B (en) * 1954-11-25 1958-04-17 Power Jets Res & Dev Ltd Turbine blade
DE1021644B (en) * 1955-05-18 1957-12-27 Messerschmitt Ag Blade for gas turbines with surface cooling
US2970807A (en) * 1957-05-28 1961-02-07 Messerschmitt Ag Rotor blades for gas turbines
US3836283A (en) * 1972-05-08 1974-09-17 Nat Aerospace Lab Construction of axial-flow turbine blades
EP0146624A1 (en) * 1983-06-20 1985-07-03 Marius A Paul Process of intensification of the thermoenergetical cycle and air jet propulsion engines.
EP0146624A4 (en) * 1983-06-20 1986-03-18 Marius A Paul Process of intensification of the thermoenergetical cycle and air jet propulsion engines.
US5177954A (en) * 1984-10-10 1993-01-12 Paul Marius A Gas turbine engine with cooled turbine blades
US5122033A (en) * 1990-11-16 1992-06-16 Paul Marius A Turbine blade unit

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