FR1088309A - Improvement in turbo-machines, particularly intended for aerodyne thrusters - Google Patents

Improvement in turbo-machines, particularly intended for aerodyne thrusters

Info

Publication number
FR1088309A
FR1088309A FR1088309DA FR1088309A FR 1088309 A FR1088309 A FR 1088309A FR 1088309D A FR1088309D A FR 1088309DA FR 1088309 A FR1088309 A FR 1088309A
Authority
FR
France
Prior art keywords
aerodyne
thrusters
turbo
machines
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
Michel-Robert Garnier
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR1088309A publication Critical patent/FR1088309A/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
    • F02C7/22—Fuel supply systems
    • F02C7/236—Fuel delivery systems comprising two or more pumps
    • F02C7/2365—Fuel delivery systems comprising two or more pumps comprising an air supply system for the atomisation of 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
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
FR1088309D 1953-08-18 1953-08-18 Improvement in turbo-machines, particularly intended for aerodyne thrusters Expired FR1088309A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1088309T 1953-08-18

Publications (1)

Publication Number Publication Date
FR1088309A true FR1088309A (en) 1955-03-07

Family

ID=9613793

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1088309D Expired FR1088309A (en) 1953-08-18 1953-08-18 Improvement in turbo-machines, particularly intended for aerodyne thrusters

Country Status (1)

Country Link
FR (1) FR1088309A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2927427A (en) * 1955-05-10 1960-03-08 Onera (Off Nat Aerospatiale) Continuous flow thermal machines and in particular in ram-jets and turbojets
US2958196A (en) * 1959-01-02 1960-11-01 Gen Electric Flame igniter for gas turbine combustor
DE1123163B (en) * 1958-05-23 1962-02-01 Gen Electric Recoil engine with afterburners

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2927427A (en) * 1955-05-10 1960-03-08 Onera (Off Nat Aerospatiale) Continuous flow thermal machines and in particular in ram-jets and turbojets
DE1123163B (en) * 1958-05-23 1962-02-01 Gen Electric Recoil engine with afterburners
US2958196A (en) * 1959-01-02 1960-11-01 Gen Electric Flame igniter for gas turbine combustor

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