DE1131467B - Composite engine for powering aircraft - Google Patents

Composite engine for powering aircraft

Info

Publication number
DE1131467B
DE1131467B DED30571A DED0030571A DE1131467B DE 1131467 B DE1131467 B DE 1131467B DE D30571 A DED30571 A DE D30571A DE D0030571 A DED0030571 A DE D0030571A DE 1131467 B DE1131467 B DE 1131467B
Authority
DE
Germany
Prior art keywords
composite engine
powering aircraft
powering
aircraft
composite
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.)
Granted
Application number
DED30571A
Other languages
German (de)
Other versions
DE1131467C2 (en
Inventor
Dipl-Ing Peter Duettmann
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
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 Daimler Benz AG filed Critical Daimler Benz AG
Priority to DE1959D0030571 priority Critical patent/DE1131467C2/de
Publication of DE1131467B publication Critical patent/DE1131467B/en
Application granted granted Critical
Publication of DE1131467C2 publication Critical patent/DE1131467C2/de
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • F02C3/305Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
    • 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
    • F02K3/02Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
    • 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
    • F02K3/08Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105Heating the by-pass flow
    • F02K3/11Heating the by-pass flow by means of burners or combustion chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/10Plants 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
    • F02K7/16Composite ram-jet/turbo-jet engines
DE1959D0030571 1959-04-30 1959-04-30 Expired DE1131467C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE1959D0030571 DE1131467C2 (en) 1959-04-30 1959-04-30

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1959D0030571 DE1131467C2 (en) 1959-04-30 1959-04-30

Publications (2)

Publication Number Publication Date
DE1131467B true DE1131467B (en) 1962-06-14
DE1131467C2 DE1131467C2 (en) 1963-01-03

Family

ID=7040554

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1959D0030571 Expired DE1131467C2 (en) 1959-04-30 1959-04-30

Country Status (1)

Country Link
DE (1) DE1131467C2 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1231064B (en) * 1962-12-17 1966-12-22 Rolls Royce Gas turbine jet engine plant for aircraft
DE1289364B (en) * 1964-08-04 1969-02-13 Rolls Royce Composite engine for powering aircraft
FR2653496A1 (en) * 1989-10-24 1991-04-26 Mtu Muenchen Gmbh Integrated turbo-statoreactor, equipping aircraft for sub and / or hypersonic flight.
US5165228A (en) * 1990-02-13 1992-11-24 Mtu Motoren-Und Turbinen-Union Munchen Gmbh Turboramjet engine
FR2910056A1 (en) * 2006-12-18 2008-06-20 Michel Aguilar Rotary wing-less vertical take-off and landing vehicle for transporting passengers by air, has rear wing whose variable incidence is set to generate lift force in take-off mode, and added to forces developed on front wings in cruise mode

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8900530D0 (en) * 1989-01-10 1989-03-08 Craig Alfred C Jet powered aircraft propulsion system

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH244761A (en) * 1945-08-14 1946-09-30 Escher Wyss Maschf Ag Jet engine for aircraft.
US2577919A (en) * 1947-07-22 1951-12-11 Snecma Association on flying machine of compressor-jet units with ramjet units
FR998659A (en) * 1949-09-30 1952-01-22 Rateau Soc An apparatus for controlling overload turbojet accessories
FR1006682A (en) * 1948-02-10 1952-04-25 Rateau Soc Overload processes for turbojets two-stream
GB701324A (en) * 1950-03-21 1953-12-23 Rateau Soc Improvements in jet or propeller turbine engines used for aircraft propulsion
GB704669A (en) * 1949-07-22 1954-02-24 Rateau Soc Improvements in jet propulsion engines
US2696078A (en) * 1952-08-30 1954-12-07 Waitzman Simon Jet propulsion apparatus having a combination ram-jet and turbojet engine
US2831627A (en) * 1954-01-15 1958-04-22 Westinghouse Electric Corp Axial flow compressor apparatus

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH244761A (en) * 1945-08-14 1946-09-30 Escher Wyss Maschf Ag Jet engine for aircraft.
US2577919A (en) * 1947-07-22 1951-12-11 Snecma Association on flying machine of compressor-jet units with ramjet units
FR1006682A (en) * 1948-02-10 1952-04-25 Rateau Soc Overload processes for turbojets two-stream
GB704669A (en) * 1949-07-22 1954-02-24 Rateau Soc Improvements in jet propulsion engines
FR998659A (en) * 1949-09-30 1952-01-22 Rateau Soc An apparatus for controlling overload turbojet accessories
GB701324A (en) * 1950-03-21 1953-12-23 Rateau Soc Improvements in jet or propeller turbine engines used for aircraft propulsion
US2696078A (en) * 1952-08-30 1954-12-07 Waitzman Simon Jet propulsion apparatus having a combination ram-jet and turbojet engine
US2831627A (en) * 1954-01-15 1958-04-22 Westinghouse Electric Corp Axial flow compressor apparatus

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1231064B (en) * 1962-12-17 1966-12-22 Rolls Royce Gas turbine jet engine plant for aircraft
DE1289364B (en) * 1964-08-04 1969-02-13 Rolls Royce Composite engine for powering aircraft
FR2653496A1 (en) * 1989-10-24 1991-04-26 Mtu Muenchen Gmbh Integrated turbo-statoreactor, equipping aircraft for sub and / or hypersonic flight.
US5165228A (en) * 1990-02-13 1992-11-24 Mtu Motoren-Und Turbinen-Union Munchen Gmbh Turboramjet engine
FR2910056A1 (en) * 2006-12-18 2008-06-20 Michel Aguilar Rotary wing-less vertical take-off and landing vehicle for transporting passengers by air, has rear wing whose variable incidence is set to generate lift force in take-off mode, and added to forces developed on front wings in cruise mode

Also Published As

Publication number Publication date
DE1131467C2 (en) 1963-01-03

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