IT8448432A0 - Sistema e medoto per intensificare il ciclo termoenergetico nei motori a propulsione mediante getto d'aria e relativi motori perfezionati - Google Patents

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

Info

Publication number
IT8448432A0
IT8448432A0 IT8448432A IT4843284A IT8448432A0 IT 8448432 A0 IT8448432 A0 IT 8448432A0 IT 8448432 A IT8448432 A IT 8448432A IT 4843284 A IT4843284 A IT 4843284A IT 8448432 A0 IT8448432 A0 IT 8448432A0
Authority
IT
Italy
Prior art keywords
engines
thermoenergy
intensifying
cycle
air jet
Prior art date
Application number
IT8448432A
Other languages
English (en)
Other versions
IT1177817B (it
IT8448432A1 (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
Publication of IT8448432A1 publication Critical patent/IT8448432A1/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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (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 (3)

Publication Number Publication Date
IT8448432A0 true IT8448432A0 (it) 1984-06-20
IT8448432A1 IT8448432A1 (it) 1985-12-20
IT1177817B 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 (11)

* 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
JP6031097B2 (ja) * 2011-06-17 2016-11-24 ゼネラル・エレクトリック・カンパニイ 航空機エンジン燃料システム及びその作動方法
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
CN118294150B (zh) * 2024-04-10 2025-10-17 集美大学 一种可实现强预冷的高焓压气机测试方法

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
EP0146624A4 (en) 1986-03-18
DK77385A (da) 1985-02-20
WO1985000199A1 (en) 1985-01-17
CA1235583A (en) 1988-04-26
IT1177817B (it) 1987-08-26
EP0146624B1 (en) 1989-03-15
IT8448432A1 (it) 1985-12-20
DE3477229D1 (en) 1989-04-20
DK77385D0 (da) 1985-02-20
BR8406943A (pt) 1985-06-04
EP0146624A1 (en) 1985-07-03
JPS60501616A (ja) 1985-09-26
AU3210384A (en) 1985-01-25

Similar Documents

Publication Publication Date Title
IT1204307B (it) Sistema di controllo di aria particolarmente per motori di aereo
IT8448432A0 (it) Sistema e medoto per intensificare il ciclo termoenergetico nei motori a propulsione mediante getto d'aria e relativi motori perfezionati
IT1180683B (it) Sistema di controllo elettronico per motori diesel
IT1146870B (it) Apparecchiatura e procedimento per il controllo di motori di propulsione
IT1176388B (it) Disposizione circuitale per l'accensione di motori termici
IT1190156B (it) Perfezionamenti nei collettori di scarico per motori di autoveicoli a piu' cilindri
IT1176626B (it) Sistema di propulsione ad elica per aeroplano
IT1150465B (it) Motore a turbine a gas e suo sistema di presa d'aria associato
FI934727A0 (fi) Propeller eller flaekt med justerbar stigvinkel
IT8721567A0 (it) Apparecchio e metodo per controllare i limiti di sfiancamento di motori a turbina
IT8103606A0 (it) Impianto per il raffreddamento dell'aria di alimentazione in motori endotermici sovraalimentati
GB2189055B (en) Apparatus and method for the flow control of flue gas to combustion air in a regenerative heating system
IT8449311A0 (it) Sensore per perdite d'aria calda erelativo metodo di impiego, in particolare per reattore d'aereo
IT1177168B (it) Dispositivo per il riconoscimento di combustioni detonanti nei motori termici
GB2186639B (en) Improvements in or relating to bladed structures for fluid flow propulsion engines
IT8922380A0 (it) Sistema sincrofasatore per turbomotore d'aeroplano
IT8347647A0 (it) Sistema di comando per l'attacco e il distacco di turbocompressori agas di scarico
IT1155952B (it) Sistema di alimentazione per motori diesel sovralimentati
IT1176384B (it) Disposizione circuitale per l'accensione di motori termici
IT1135845B (it) Iniettore-pompa per motori diesel
IT8368106A0 (it) Dispositivo di filtraggio per l aria di aspirazione di motori di aeromobili in particolare elicotteri
IT1173030B (it) Procedimento e sistema circuitale per la regolazione dell'assorbimento di energia di un motore a corrente alternata
IT1209024B (it) Sistema di carburazione nei motori metodo di perfezionamento al a ciclo otto.
IT8622586A0 (it) Apparecchio e metodo per impedire il rallentamento involontario di un motore funzionante di un aeromobile a piu' motori.
IT8360336V0 (it) Metodo di perfezionamento al sistema di carburazione nei motori a ciclo otto.

Legal Events

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

Effective date: 19921230