IT1177817B - Sistema e metodo per intensificare il ciclo termoenergetico nei motori a propulsione mediante getto d'aria e relativi motori perfezionati - Google Patents

Sistema e metodo per intensificare il ciclo termoenergetico nei motori a propulsione mediante getto d'aria e relativi motori perfezionati

Info

Publication number
IT1177817B
IT1177817B IT48432/84A IT4843284A IT1177817B IT 1177817 B IT1177817 B IT 1177817B IT 48432/84 A IT48432/84 A IT 48432/84A IT 4843284 A IT4843284 A IT 4843284A IT 1177817 B IT1177817 B IT 1177817B
Authority
IT
Italy
Prior art keywords
engines
intensifying
thermo
air jet
energy cycle
Prior art date
Application number
IT48432/84A
Other languages
English (en)
Other versions
IT8448432A0 (it
Inventor
Paul A Marius
Original Assignee
Paul A Marius
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 Paul A Marius filed Critical Paul A Marius
Publication of IT8448432A0 publication Critical patent/IT8448432A0/it
Application granted granted Critical
Publication of IT1177817B publication Critical patent/IT1177817B/it

Links

Classifications

    • 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
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • 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
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • 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
    • F23R3/34—Feeding into different combustion zones
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Means For Warming Up And Starting Carburetors (AREA)
  • Control Of Turbines (AREA)
  • Percussion Or Vibration Massage (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
IT48432/84A 1983-06-20 1984-06-20 Sistema e metodo per intensificare il ciclo termoenergetico nei motori a propulsione mediante getto d'aria e relativi motori perfezionati IT1177817B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US50565883A 1983-06-20 1983-06-20

Publications (2)

Publication Number Publication Date
IT8448432A0 IT8448432A0 (it) 1984-06-20
IT1177817B true IT1177817B (it) 1987-08-26

Family

ID=24011258

Family Applications (1)

Application Number Title Priority Date Filing Date
IT48432/84A IT1177817B (it) 1983-06-20 1984-06-20 Sistema e metodo per intensificare il ciclo termoenergetico nei motori a propulsione mediante getto d'aria e relativi motori perfezionati

Country Status (9)

Country Link
EP (1) EP0146624B1 (it)
JP (1) JPS60501616A (it)
AU (1) AU3210384A (it)
BR (1) BR8406943A (it)
CA (1) CA1235583A (it)
DE (1) DE3477229D1 (it)
DK (1) DK77385D0 (it)
IT (1) IT1177817B (it)
WO (1) WO1985000199A1 (it)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4858428A (en) * 1986-04-24 1989-08-22 Paul Marius A Advanced integrated propulsion system with total optimized cycle for gas turbines
US4916896A (en) * 1988-11-02 1990-04-17 Paul Marius A Multiple propulsion with quatro vectorial direction system
FR2670869B1 (fr) * 1990-12-19 1994-10-21 Snecma Chambre de combustion comportant deux enceintes successives.
JP2988109B2 (ja) * 1991-03-20 1999-12-06 株式会社日立製作所 回転電機用ロータシャフト及びそれを用いた回転電機
GB9418949D0 (en) * 1994-09-20 1994-11-09 Helliwell Brian J 90% thermal efficient gas turbine engine
DE19902437C5 (de) * 1999-01-22 2017-01-12 General Electric Technology Gmbh Verfahren und Vorrichtung zum schnellen Anfahren und zur schnellen Leistungssteigerung einer Gasturbinenanlage
JP2013543556A (ja) * 2010-09-30 2013-12-05 ゼネラル・エレクトリック・カンパニイ 航空機エンジンシステムおよびそれを動作させるための方法
CA2838561A1 (en) * 2011-06-17 2012-12-20 General Electric Company Aircraft engine fuel system and method of operating the same
US9709069B2 (en) 2013-10-22 2017-07-18 Dayspring Church Of God Apostolic Hybrid drive engine
JP7250304B2 (ja) * 2018-09-26 2023-04-03 国立大学法人室蘭工業大学 タービン駆動用ガスジェネレータの推進剤及びその製造方法

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2360130A (en) * 1941-03-26 1944-10-10 Armstrong Siddeley Motors Ltd High-speed propulsion plant
US2416389A (en) * 1942-06-17 1947-02-25 Armstrong Siddeley Motors Ltd Torque balancing of jet propulsion turbine plant
FR924012A (fr) * 1946-02-18 1947-07-24 Const Aeronautiques Du Ct Soc Perfectionnement apporté aux turbines à combustion
US2647368A (en) * 1949-05-09 1953-08-04 Hermann Oestrich Method and apparatus for internally cooling gas turbine blades with air, fuel, and water
DE846341C (de) * 1950-06-20 1952-08-11 Gustav Fillon Beschaufelung mit Innenkuehlung fuer Gasturbinen mit Verbrennung innerhalb der Schaufelkanaele
CH308992A (de) * 1951-05-16 1955-08-15 Power Jets Res & Dev Ltd Gasturbinenanlage.
US2970807A (en) * 1957-05-28 1961-02-07 Messerschmitt Ag Rotor blades for gas turbines
US3747339A (en) * 1961-11-13 1973-07-24 Texaco Inc Reaction propulsion engine and method of operation
DE1231959B (de) * 1963-06-28 1967-01-05 M A N Turbo G M B H Als Zweistromtriebwerk in Einwellenbauart ausgebildetes Hubstrahltriebwerk fuer Luftfahrzeuge
GB1039677A (en) * 1963-07-10 1966-08-17 Rolls Royce Combustion chamber for a gas turbine engine
US3740949A (en) * 1963-11-20 1973-06-26 Texaco Inc Fuel cooled ram air reaction propulsion engine
DE1261357B (de) * 1965-12-14 1968-02-15 Dornier Gmbh Gasturbinentriebwerk
US3486340A (en) * 1967-05-05 1969-12-30 Garrett Corp Gas turbine powerplant with means for cooling compressed air
US3600890A (en) * 1968-11-29 1971-08-24 United Aircraft Corp Turbine cooling construction
CH573571A5 (it) * 1974-01-11 1976-03-15 Sulzer Ag
US4054030A (en) * 1976-04-29 1977-10-18 General Motors Corporation Variable cycle gas turbine engine
US4118145A (en) * 1977-03-02 1978-10-03 Westinghouse Electric Corp. Water-cooled turbine blade
US4190398A (en) * 1977-06-03 1980-02-26 General Electric Company Gas turbine engine and means for cooling same
US4242045A (en) * 1979-06-01 1980-12-30 General Electric Company Trap seal for open circuit liquid cooled turbines

Also Published As

Publication number Publication date
JPS60501616A (ja) 1985-09-26
DK77385A (da) 1985-02-20
EP0146624A1 (en) 1985-07-03
AU3210384A (en) 1985-01-25
CA1235583A (en) 1988-04-26
DK77385D0 (da) 1985-02-20
WO1985000199A1 (en) 1985-01-17
EP0146624B1 (en) 1989-03-15
DE3477229D1 (en) 1989-04-20
IT8448432A0 (it) 1984-06-20
BR8406943A (pt) 1985-06-04
EP0146624A4 (en) 1986-03-18

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19921230