DE3906580A1 - Leichtes turbinenstrahltriebwerk nach dem baukastenprinzip - Google Patents

Leichtes turbinenstrahltriebwerk nach dem baukastenprinzip

Info

Publication number
DE3906580A1
DE3906580A1 DE3906580A DE3906580A DE3906580A1 DE 3906580 A1 DE3906580 A1 DE 3906580A1 DE 3906580 A DE3906580 A DE 3906580A DE 3906580 A DE3906580 A DE 3906580A DE 3906580 A1 DE3906580 A1 DE 3906580A1
Authority
DE
Germany
Prior art keywords
stage
engine according
turbine
jet engine
turbine jet
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Withdrawn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
DE3906580A
Other languages
German (de)
English (en)
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 DE3906580A1 publication Critical patent/DE3906580A1/de
Withdrawn legal-status Critical Current

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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18Lubricating arrangements
    • 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
    • F01D3/00Machines or engines with axial-thrust balancing effected by working-fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06Gas-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
    • F02C3/067Gas-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/12Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
    • 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

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)
DE3906580A 1988-04-11 1989-03-02 Leichtes turbinenstrahltriebwerk nach dem baukastenprinzip Withdrawn DE3906580A1 (de)

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
DE3906580A1 true DE3906580A1 (de) 1989-10-19

Family

ID=11301439

Family Applications (1)

Application Number Title Priority Date Filing Date
DE3906580A Withdrawn DE3906580A1 (de) 1988-04-11 1989-03-02 Leichtes turbinenstrahltriebwerk nach dem baukastenprinzip

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
DE19852768A1 (de) * 1998-11-16 2000-05-18 Bmw Rolls Royce Gmbh Kleingasturbine mit einer Radial- oder Slinger-Brennkammer

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE1025642B1 (fr) * 2017-10-16 2019-05-15 Safran Aero Boosters S.A. Carter de compresseur avec reservoir d'huile pour turbomachine

Family Cites Families (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 (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

Also Published As

Publication number Publication date
IT1219194B (it) 1990-05-03
IL89449A0 (en) 1989-09-10
IT8867322A0 (it) 1988-04-11
FR2629872A1 (fr) 1989-10-13

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Legal Events

Date Code Title Description
8139 Disposal/non-payment of the annual fee