FR924012A - Improvement made to combustion turbines - Google Patents

Improvement made to 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
improvement made
combustion turbines
turbines
combustion
improvement
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
Priority to FR924012T priority Critical
Application granted granted Critical
Publication of FR924012A publication Critical patent/FR924012A/en
Application status is Expired legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/182Transpiration cooling
    • F01D5/183Blade walls being porous
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
FR924012D 1946-02-18 1946-02-18 Improvement made to combustion turbines Expired FR924012A (en)

Priority Applications (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 Improvement made to 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 Oberflaechenkuehlung
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 Oberflaechenkuehlung
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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