DE3915697C1 - - Google Patents

Info

Publication number
DE3915697C1
DE3915697C1 DE3915697A DE3915697A DE3915697C1 DE 3915697 C1 DE3915697 C1 DE 3915697C1 DE 3915697 A DE3915697 A DE 3915697A DE 3915697 A DE3915697 A DE 3915697A DE 3915697 C1 DE3915697 C1 DE 3915697C1
Authority
DE
Germany
Prior art keywords
turbine
compressor
group
stages
stage
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.)
Expired - Fee Related
Application number
DE3915697A
Other languages
German (de)
English (en)
Inventor
Hans Dipl.-Ing. 8113 Kochel De Lifka
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.)
LIFKA, HANS, DIPL.-ING., 82431 KOCHEL, DE
Original Assignee
Messerschmitt Bolkow Blohm 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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Priority to DE3915697A priority Critical patent/DE3915697C1/de
Priority to FR9005920A priority patent/FR2646879B1/fr
Priority to GB9010788A priority patent/GB2235018B/en
Application granted granted Critical
Publication of DE3915697C1 publication Critical patent/DE3915697C1/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
    • 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
    • F02C3/36—Open cycles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/80—Application in supersonic vehicles excluding hypersonic vehicles or ram, scram or rocket propulsion
    • 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)
DE3915697A 1989-05-13 1989-05-13 Expired - Fee Related DE3915697C1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE3915697A DE3915697C1 (fr) 1989-05-13 1989-05-13
FR9005920A FR2646879B1 (fr) 1989-05-13 1990-05-11 Installation pour le refroidissement de gaz et la fourniture de puissance mecanique a des fins d'entrainement, notamment sur des engins volants hypersoniques
GB9010788A GB2235018B (en) 1989-05-13 1990-05-14 Device for air cooling and provision of mechanical power

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3915697A DE3915697C1 (fr) 1989-05-13 1989-05-13

Publications (1)

Publication Number Publication Date
DE3915697C1 true DE3915697C1 (fr) 1990-12-20

Family

ID=6380625

Family Applications (1)

Application Number Title Priority Date Filing Date
DE3915697A Expired - Fee Related DE3915697C1 (fr) 1989-05-13 1989-05-13

Country Status (3)

Country Link
DE (1) DE3915697C1 (fr)
FR (1) FR2646879B1 (fr)
GB (1) GB2235018B (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5443362A (en) * 1994-03-16 1995-08-22 The Hoover Company Air turbine
JP3981721B2 (ja) 2002-04-02 2007-09-26 独立行政法人 宇宙航空研究開発機構 単翼列多段タービン

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3002340A (en) * 1957-04-05 1961-10-03 United Aircraft Corp Rocket gas generator for turbofan engine
GB1392675A (en) * 1961-11-13 1975-04-30 Texaco Development Corp Reaction propulsion engine and method of operation

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2454738A (en) * 1944-01-31 1948-11-23 Power Jets Res And Development Internal-combustion turbine power plant
FR954272A (fr) * 1946-09-11 1949-12-21 Rolls Royce Perfectionnements aux turbines à gaz et à leurs organes de réglage
GB800661A (en) * 1955-06-23 1958-08-27 Plessey Co Ltd Improvements in or relating to air turbines
DE1085718B (de) * 1958-11-26 1960-07-21 Daimler Benz Ag Gasturbinentriebwerk
DE1406609A1 (de) * 1961-12-21 1968-10-31 Materiels Hispano Suiza S A So Anlage zur gleichzeitigen Erzeugung von Kuehlenergie und elektrischer Energie in schnell fliegenden Flugzeugen
GB1093151A (en) * 1964-04-29 1967-11-29 Hawker Siddeley Dynamics Ltd Improvements in or relating to air conditioning systems
FR2102467A5 (fr) * 1970-08-05 1972-04-07 Rylewski Eugeniusz
DE2121738A1 (de) * 1971-05-03 1972-11-09 Sontheimer, Georg, 7900 Ulm Gasturbine und Verfahren zum Betrieb derselben

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3002340A (en) * 1957-04-05 1961-10-03 United Aircraft Corp Rocket gas generator for turbofan engine
GB1392675A (en) * 1961-11-13 1975-04-30 Texaco Development Corp Reaction propulsion engine and method of operation

Also Published As

Publication number Publication date
GB2235018B (en) 1993-11-24
FR2646879A1 (fr) 1990-11-16
GB2235018A (en) 1991-02-20
FR2646879B1 (fr) 1993-10-29
GB9010788D0 (en) 1990-07-04

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Legal Events

Date Code Title Description
8100 Publication of the examined application without publication of unexamined application
D1 Grant (no unexamined application published) patent law 81
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: DEUTSCHE AEROSPACE AG, 8000 MUENCHEN, DE

8327 Change in the person/name/address of the patent owner

Owner name: LIFKA, HANS, DIPL.-ING., 82431 KOCHEL, DE

8339 Ceased/non-payment of the annual fee