DE1131467C2 - - Google Patents

Info

Publication number
DE1131467C2
DE1131467C2 DE1959D0030571 DED0030571A DE1131467C2 DE 1131467 C2 DE1131467 C2 DE 1131467C2 DE 1959D0030571 DE1959D0030571 DE 1959D0030571 DE D0030571 A DED0030571 A DE D0030571A DE 1131467 C2 DE1131467 C2 DE 1131467C2
Authority
DE
Germany
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.)
Expired
Application number
DE1959D0030571
Other languages
German (de)
Other versions
DE1131467B (de
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 filed Critical
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 DE1131467B (de) 1962-06-14
DE1131467C2 true DE1131467C2 (zh) 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 (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990008255A1 (en) * 1989-01-10 1990-07-26 Alfred Cowie Craig Controlling the flow ratio in a multiflow jet engine

Families Citing this family (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
GB1008322A (en) * 1964-08-04 1965-10-27 Rolls Royce Gas turbine engine
DE3935313C1 (zh) * 1989-10-24 1991-06-06 Mtu Muenchen Gmbh
DE4004416C2 (de) * 1990-02-13 1993-10-14 Mtu Muenchen Gmbh Turbo-Staustrahltriebwerk mit Absperreinrichtung für variablen Umschaltbetrieb
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

Family Cites Families (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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990008255A1 (en) * 1989-01-10 1990-07-26 Alfred Cowie Craig Controlling the flow ratio in a multiflow jet engine

Also Published As

Publication number Publication date
DE1131467B (de) 1962-06-14

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