FR2629872A1 - Turboreacteur leger modulaire - Google Patents

Turboreacteur leger modulaire Download PDF

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Publication number
FR2629872A1
FR2629872A1 FR8904626A FR8904626A FR2629872A1 FR 2629872 A1 FR2629872 A1 FR 2629872A1 FR 8904626 A FR8904626 A FR 8904626A FR 8904626 A FR8904626 A FR 8904626A FR 2629872 A1 FR2629872 A1 FR 2629872A1
Authority
FR
France
Prior art keywords
compressor
engine according
turbojet engine
stage
air
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.)
Withdrawn
Application number
FR8904626A
Other languages
English (en)
French (fr)
Inventor
Claudio Peretti
Paolo Bellezza
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.)
ARIS SpA
Original Assignee
ARIS SpA
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 ARIS SpA filed Critical ARIS SpA
Publication of FR2629872A1 publication Critical patent/FR2629872A1/fr
Withdrawn legal-status Critical Current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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • 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
    • F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR8904626A 1988-04-11 1989-04-07 Turboreacteur leger modulaire Withdrawn FR2629872A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT67322/88A IT1219194B (it) 1988-04-11 1988-04-11 Turboreattore leggero modulare

Publications (1)

Publication Number Publication Date
FR2629872A1 true FR2629872A1 (fr) 1989-10-13

Family

ID=11301439

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8904626A Withdrawn FR2629872A1 (fr) 1988-04-11 1989-04-07 Turboreacteur leger modulaire

Country Status (4)

Country Link
DE (1) DE3906580A1 (it)
FR (1) FR2629872A1 (it)
IL (1) IL89449A0 (it)
IT (1) IT1219194B (it)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019076519A1 (fr) * 2017-10-16 2019-04-25 Safran Aero Boosters Sa Carter extérieur de turbo-compresseur avec réservoir d'huile intégré

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19852768A1 (de) * 1998-11-16 2000-05-18 Bmw Rolls Royce Gmbh Kleingasturbine mit einer Radial- oder Slinger-Brennkammer

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2880573A (en) * 1952-08-27 1959-04-07 Gen Motors Corp Afterburner fuel injection system
GB1020145A (en) * 1964-12-07 1966-02-16 Rolls Royce Power plant e.g. for jet propulsion of aircraft
GB1039677A (en) * 1963-07-10 1966-08-17 Rolls Royce Combustion chamber for a gas turbine engine
US3552873A (en) * 1969-01-10 1971-01-05 John N Ghougasian Supersonic jet engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2880573A (en) * 1952-08-27 1959-04-07 Gen Motors Corp Afterburner fuel injection system
GB1039677A (en) * 1963-07-10 1966-08-17 Rolls Royce Combustion chamber for a gas turbine engine
GB1020145A (en) * 1964-12-07 1966-02-16 Rolls Royce Power plant e.g. for jet propulsion of aircraft
US3552873A (en) * 1969-01-10 1971-01-05 John N Ghougasian Supersonic jet engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019076519A1 (fr) * 2017-10-16 2019-04-25 Safran Aero Boosters Sa Carter extérieur de turbo-compresseur avec réservoir d'huile intégré
BE1025642B1 (fr) * 2017-10-16 2019-05-15 Safran Aero Boosters S.A. Carter de compresseur avec reservoir d'huile pour turbomachine
US11506068B2 (en) 2017-10-16 2022-11-22 Safran Aero Boosters Sa Compressor casing with oil tank for a turbine engine

Also Published As

Publication number Publication date
IT1219194B (it) 1990-05-03
IL89449A0 (en) 1989-09-10
IT8867322A0 (it) 1988-04-11
DE3906580A1 (de) 1989-10-19

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Legal Events

Date Code Title Description
ST Notification of lapse