DE1131467B - Verbundtriebwerk zum Antrieb von Flugzeugen - Google Patents

Verbundtriebwerk zum Antrieb von Flugzeugen

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
engine
ramjet
air
volume
aircraft
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)
English (en)
Other versions
DE1131467C2 (sl
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 DED30571A priority Critical patent/DE1131467B/de
Publication of DE1131467B publication Critical patent/DE1131467B/de
Application granted granted Critical
Publication of DE1131467C2 publication Critical patent/DE1131467C2/de
Granted legal-status Critical Current

Links

Classifications

    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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
    • F02C3/20—Gas-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
    • F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • F02C3/305—Increasing 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
    • 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
    • F02K3/02—Plants 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
    • F02K3/04—Plants 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
    • F02K3/075—Plants 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
    • 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
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DED30571A 1959-04-30 1959-04-30 Verbundtriebwerk zum Antrieb von Flugzeugen Granted DE1131467B (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DED30571A DE1131467B (de) 1959-04-30 1959-04-30 Verbundtriebwerk zum Antrieb von Flugzeugen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DED30571A DE1131467B (de) 1959-04-30 1959-04-30 Verbundtriebwerk zum Antrieb von Flugzeugen

Publications (2)

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

Family

ID=7040554

Family Applications (1)

Application Number Title Priority Date Filing Date
DED30571A Granted DE1131467B (de) 1959-04-30 1959-04-30 Verbundtriebwerk zum Antrieb von Flugzeugen

Country Status (1)

Country Link
DE (1) DE1131467B (sl)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1231064B (de) * 1962-12-17 1966-12-22 Rolls Royce Gasturbinenstrahltriebwerksanlage fuer Flugzeuge
DE1289364B (de) * 1964-08-04 1969-02-13 Rolls Royce Verbundtriebwerk zum Antrieb von Flugzeugen
FR2653496A1 (fr) * 1989-10-24 1991-04-26 Mtu Muenchen Gmbh Turbo-statoreacteur integre, equipant des avions pour vol sub et/ou hypersonique.
US5165228A (en) * 1990-02-13 1992-11-24 Mtu Motoren-Und Turbinen-Union Munchen Gmbh Turboramjet engine
FR2910056A1 (fr) * 2006-12-18 2008-06-20 Michel Aguilar Turbomachine a compresseur volumique rotatif
FR3052493A1 (fr) * 2016-06-14 2017-12-15 Guillaume Thomas Pelcot Reacteur combine et les moyens de permutation entre ses deux modes de fonctionnement
CN111692013A (zh) * 2020-07-03 2020-09-22 南京航空航天大学 一种轴对称内并联涡轮基旋转爆震冲压组合发动机及控制方法

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 (de) * 1945-08-14 1946-09-30 Escher Wyss Maschf Ag Düsentriebwerk für Flugzeuge.
US2577919A (en) * 1947-07-22 1951-12-11 Snecma Association on flying machine of compressor-jet units with ramjet units
FR998659A (fr) * 1949-09-30 1952-01-22 Rateau Soc Dispositif de commande des accessoires de surcharge des turboréacteurs
FR1006682A (fr) * 1948-02-10 1952-04-25 Rateau Soc Procédés de surcharge pour les turbo-réacteurs à deux flux
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 (de) * 1945-08-14 1946-09-30 Escher Wyss Maschf Ag Düsentriebwerk für Flugzeuge.
US2577919A (en) * 1947-07-22 1951-12-11 Snecma Association on flying machine of compressor-jet units with ramjet units
FR1006682A (fr) * 1948-02-10 1952-04-25 Rateau Soc Procédés de surcharge pour les turbo-réacteurs à deux flux
GB704669A (en) * 1949-07-22 1954-02-24 Rateau Soc Improvements in jet propulsion engines
FR998659A (fr) * 1949-09-30 1952-01-22 Rateau Soc Dispositif de commande des accessoires de surcharge des turboréacteurs
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 (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1231064B (de) * 1962-12-17 1966-12-22 Rolls Royce Gasturbinenstrahltriebwerksanlage fuer Flugzeuge
DE1289364B (de) * 1964-08-04 1969-02-13 Rolls Royce Verbundtriebwerk zum Antrieb von Flugzeugen
FR2653496A1 (fr) * 1989-10-24 1991-04-26 Mtu Muenchen Gmbh Turbo-statoreacteur integre, equipant des avions pour vol sub et/ou hypersonique.
US5165228A (en) * 1990-02-13 1992-11-24 Mtu Motoren-Und Turbinen-Union Munchen Gmbh Turboramjet engine
FR2910056A1 (fr) * 2006-12-18 2008-06-20 Michel Aguilar Turbomachine a compresseur volumique rotatif
FR3052493A1 (fr) * 2016-06-14 2017-12-15 Guillaume Thomas Pelcot Reacteur combine et les moyens de permutation entre ses deux modes de fonctionnement
CN111692013A (zh) * 2020-07-03 2020-09-22 南京航空航天大学 一种轴对称内并联涡轮基旋转爆震冲压组合发动机及控制方法

Also Published As

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

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