FR2099597B3 - - Google Patents

Info

Publication number
FR2099597B3
FR2099597B3 FR7046318A FR7046318A FR2099597B3 FR 2099597 B3 FR2099597 B3 FR 2099597B3 FR 7046318 A FR7046318 A FR 7046318A FR 7046318 A FR7046318 A FR 7046318A FR 2099597 B3 FR2099597 B3 FR 2099597B3
Authority
FR
France
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
FR7046318A
Other languages
French (fr)
Other versions
FR2099597A7 (de
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.)
MTU Aero Engines GmbH
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2099597A7 publication Critical patent/FR2099597A7/fr
Application granted granted Critical
Publication of FR2099597B3 publication Critical patent/FR2099597B3/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/004—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector
    • 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
    • F02K3/06—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 with front fan
    • 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
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/328—Application in turbines in gas turbines providing direct vertical lift

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
FR7046318A 1970-07-25 1970-12-22 Expired FR2099597B3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19702037049 DE2037049A1 (de) 1970-07-25 1970-07-25 Mehr Wellen Turbinenstrahltriebwerk

Publications (2)

Publication Number Publication Date
FR2099597A7 FR2099597A7 (de) 1972-03-17
FR2099597B3 true FR2099597B3 (de) 1973-04-27

Family

ID=5777928

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7046318A Expired FR2099597B3 (de) 1970-07-25 1970-12-22

Country Status (3)

Country Link
DE (1) DE2037049A1 (de)
FR (1) FR2099597B3 (de)
GB (1) GB1351000A (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4713935A (en) * 1986-04-08 1987-12-22 Rolls-Royce Inc. Vectorable nozzles for aircraft
DE4426195C2 (de) * 1994-07-23 1998-02-05 Daimler Benz Aerospace Ag Schubdüse in Rechteckbauweise für Strahltriebwerke
DE10033653A1 (de) * 2000-06-16 2002-03-07 Sandor Nagy Kombinationsantrieb
DE10126632A1 (de) * 2000-08-08 2002-09-12 Sandor Nagy Kombinationsantrieb
DE602004028297D1 (de) 2004-12-01 2010-09-02 United Technologies Corp Umfangsbrennkammer für spitzenturbinenmotor
EP1825116A2 (de) 2004-12-01 2007-08-29 United Technologies Corporation Ejektor-kühlung des aussengehäuses eines tip-turbinen-triebwerks
EP1828547B1 (de) 2004-12-01 2011-11-30 United Technologies Corporation Turbofantriebwerk mit einer Mehrzahl von einzeln steuerbaren Einlassleitschaufeln und zugehöriges Steuerverfahren
US8561383B2 (en) 2004-12-01 2013-10-22 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
WO2006059972A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
DE602004031470D1 (de) * 2004-12-01 2011-03-31 United Technologies Corp Übergangskanal mit mitteln zur strömungsvektorbeeinflussung bei einer gasturbine
WO2006059986A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
US7937927B2 (en) 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
EP1831521B1 (de) 2004-12-01 2008-08-20 United Technologies Corporation Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren
EP1828683B1 (de) 2004-12-01 2013-04-10 United Technologies Corporation Brennkammer für turbinenmotor
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
CN105134407B (zh) * 2015-08-20 2017-08-01 南京航空航天大学 具有垂直起降功能的喉道偏移式气动矢量喷管及控制方法

Also Published As

Publication number Publication date
FR2099597A7 (de) 1972-03-17
GB1351000A (en) 1974-04-24
DE2037049A1 (de) 1972-02-03

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Legal Events

Date Code Title Description
ST Notification of lapse