FR2724978B1 - Reacteur a inversion de poussee, reduisant la distance a l'atterrissage d'avions - Google Patents

Reacteur a inversion de poussee, reduisant la distance a l'atterrissage d'avions

Info

Publication number
FR2724978B1
FR2724978B1 FR9510176A FR9510176A FR2724978B1 FR 2724978 B1 FR2724978 B1 FR 2724978B1 FR 9510176 A FR9510176 A FR 9510176A FR 9510176 A FR9510176 A FR 9510176A FR 2724978 B1 FR2724978 B1 FR 2724978B1
Authority
FR
France
Prior art keywords
reverse thrust
landing distance
airplane landing
reactor
reducing
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
FR9510176A
Other languages
English (en)
Other versions
FR2724978A1 (fr
Inventor
Peter Tracksdorf
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 FR2724978A1 publication Critical patent/FR2724978A1/fr
Application granted granted Critical
Publication of FR2724978B1 publication Critical patent/FR2724978B1/fr
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
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR9510176A 1994-09-22 1995-08-29 Reacteur a inversion de poussee, reduisant la distance a l'atterrissage d'avions Expired - Fee Related FR2724978B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19944433759 DE4433759C1 (de) 1994-09-22 1994-09-22 Strahltriebwerk mit Schubumkehr

Publications (2)

Publication Number Publication Date
FR2724978A1 FR2724978A1 (fr) 1996-03-29
FR2724978B1 true FR2724978B1 (fr) 1998-04-30

Family

ID=6528840

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9510176A Expired - Fee Related FR2724978B1 (fr) 1994-09-22 1995-08-29 Reacteur a inversion de poussee, reduisant la distance a l'atterrissage d'avions

Country Status (3)

Country Link
DE (1) DE4433759C1 (fr)
FR (1) FR2724978B1 (fr)
GB (1) GB2293359B (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19642393A1 (de) 1996-10-14 1998-04-16 Mtu Muenchen Gmbh Turbostrahltriebwerk mit einem Blütenmischer
FR2914954B1 (fr) * 2007-04-13 2012-12-07 Snecma Turboreacteur a double flux comportant un inverseur de poussee.

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2952124A (en) * 1957-07-29 1960-09-13 Boeing Co Plug type noise suppressor and thrust reverser
GB838038A (en) * 1957-08-20 1960-06-22 Boeing Co Improvements in jet engines
US2938335A (en) * 1958-04-14 1960-05-31 Boeing Co Noise suppressor and thrust reverser
GB859993A (en) * 1958-06-20 1961-01-25 Boeing Co Retractable noise suppressor for jet propulsion engines
US3302404A (en) * 1965-06-30 1967-02-07 Gen Electric Lightweight thrust reverser
GB1190039A (en) * 1967-10-13 1970-04-29 British Aircraft Corp Ltd Thrust Reversing Mechanism for Aircraft Gas Turbine Engines
BE756228R (fr) * 1970-03-02 1971-03-01 Gen Electric
US3829020A (en) * 1973-06-13 1974-08-13 Boeing Co Translating sleeve variable area nozzle and thrust reverser
US3837411A (en) * 1973-11-21 1974-09-24 Gen Electric Diverter valve for a gas turbine with an augmenter
US4074859A (en) * 1976-11-10 1978-02-21 The United States Of America As Represented By The Secretary Of The Air Force Deformable plug for an aircraft engine exhaust nozzle
FR2644209B1 (fr) * 1989-03-08 1991-05-03 Snecma Chemise de protection thermique pour canal chaud de turboreacteur

Also Published As

Publication number Publication date
GB2293359B (en) 1998-02-18
GB2293359A (en) 1996-03-27
FR2724978A1 (fr) 1996-03-29
DE4433759C1 (de) 1996-02-08
GB9518811D0 (en) 1995-11-15

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Legal Events

Date Code Title Description
ST Notification of lapse