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FR331292A - Continuous combustion turbo-engine - Google Patents

Continuous combustion turbo-engine

Info

Publication number
FR331292A
FR331292A FR331292DA FR331292A FR 331292 A FR331292 A FR 331292A FR 331292D A FR331292D A FR 331292DA FR 331292 A FR331292 A FR 331292A
Authority
FR
France
Prior art keywords
engine
continuous combustion
combustion turbo
turbo
continuous
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
Gaston-Charles-Emile De Bonnechose
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.)
GASTON CHARLES EMILE DE BONNEC
Original Assignee
GASTON CHARLES EMILE DE BONNEC
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 GASTON CHARLES EMILE DE BONNEC filed Critical GASTON CHARLES EMILE DE BONNEC
Application granted granted Critical
Publication of FR331292A publication Critical patent/FR331292A/en
Expired legal-status Critical Current

Links

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
    • 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
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/32—Inducing air flow by fluid jet, e.g. ejector action

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR331292D 1903-02-16 1903-02-16 Continuous combustion turbo-engine Expired FR331292A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR331292T 1903-02-16

Publications (1)

Publication Number Publication Date
FR331292A true FR331292A (en) 1903-09-03

Family

ID=1381013

Family Applications (1)

Application Number Title Priority Date Filing Date
FR331292D Expired FR331292A (en) 1903-02-16 1903-02-16 Continuous combustion turbo-engine

Country Status (1)

Country Link
FR (1) FR331292A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2546432A (en) * 1944-03-20 1951-03-27 Power Jets Res & Dev Ltd Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream
US2692480A (en) * 1948-05-07 1954-10-26 Onera (Off Nat Aerospatiale) Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines
US2881588A (en) * 1948-04-27 1959-04-14 Wilbur H Goss Injector and method for fuel injection
US3062482A (en) * 1952-08-25 1962-11-06 A V Roe Canada Ltd Gas turbine engined aircraft

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2546432A (en) * 1944-03-20 1951-03-27 Power Jets Res & Dev Ltd Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream
US2881588A (en) * 1948-04-27 1959-04-14 Wilbur H Goss Injector and method for fuel injection
US2692480A (en) * 1948-05-07 1954-10-26 Onera (Off Nat Aerospatiale) Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines
US3062482A (en) * 1952-08-25 1962-11-06 A V Roe Canada Ltd Gas turbine engined aircraft

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