GB2293359B - Jet Engine with Thrust Reversal - Google Patents

Jet Engine with Thrust Reversal

Info

Publication number
GB2293359B
GB2293359B GB9518811A GB9518811A GB2293359B GB 2293359 B GB2293359 B GB 2293359B GB 9518811 A GB9518811 A GB 9518811A GB 9518811 A GB9518811 A GB 9518811A GB 2293359 B GB2293359 B GB 2293359B
Authority
GB
United Kingdom
Prior art keywords
jet engine
thrust reversal
reversal
thrust
jet
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
GB9518811A
Other versions
GB9518811D0 (en
GB2293359A (en
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 GB9518811D0 publication Critical patent/GB9518811D0/en
Publication of GB2293359A publication Critical patent/GB2293359A/en
Application granted granted Critical
Publication of GB2293359B publication Critical patent/GB2293359B/en
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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB9518811A 1994-09-22 1995-09-14 Jet Engine with Thrust Reversal Expired - Fee Related GB2293359B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19944433759 DE4433759C1 (en) 1994-09-22 1994-09-22 Jet engine with thrust reverser

Publications (3)

Publication Number Publication Date
GB9518811D0 GB9518811D0 (en) 1995-11-15
GB2293359A GB2293359A (en) 1996-03-27
GB2293359B true GB2293359B (en) 1998-02-18

Family

ID=6528840

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9518811A Expired - Fee Related GB2293359B (en) 1994-09-22 1995-09-14 Jet Engine with Thrust Reversal

Country Status (3)

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

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19642393A1 (en) 1996-10-14 1998-04-16 Mtu Muenchen Gmbh Turbo jet engine with a flower mixer
FR2914954B1 (en) * 2007-04-13 2012-12-07 Snecma DOUBLE FLOW TURBOREACTOR COMPRISING A PUSH INVERTER.

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938335A (en) * 1958-04-14 1960-05-31 Boeing Co Noise suppressor and thrust reverser
GB838038A (en) * 1957-08-20 1960-06-22 Boeing Co Improvements in jet engines
GB859993A (en) * 1958-06-20 1961-01-25 Boeing Co Retractable noise suppressor for jet propulsion engines
GB1190039A (en) * 1967-10-13 1970-04-29 British Aircraft Corp Ltd Thrust Reversing Mechanism for Aircraft Gas Turbine Engines
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
US5079915A (en) * 1989-03-08 1992-01-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Heat protective lining for a passage in a turbojet engine

Family Cites Families (3)

* 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
US3302404A (en) * 1965-06-30 1967-02-07 Gen Electric Lightweight thrust reverser
BE756228R (en) * 1970-03-02 1971-03-01 Gen Electric

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
GB848679A (en) * 1958-04-14 1960-09-21 Boeing Co Noise suppressor and thrust reverser for aircraft jet engines
GB859993A (en) * 1958-06-20 1961-01-25 Boeing Co Retractable noise suppressor for jet propulsion engines
GB1190039A (en) * 1967-10-13 1970-04-29 British Aircraft Corp Ltd Thrust Reversing Mechanism for Aircraft Gas Turbine Engines
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
US5079915A (en) * 1989-03-08 1992-01-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Heat protective lining for a passage in a turbojet engine

Also Published As

Publication number Publication date
FR2724978A1 (en) 1996-03-29
GB9518811D0 (en) 1995-11-15
FR2724978B1 (en) 1998-04-30
DE4433759C1 (en) 1996-02-08
GB2293359A (en) 1996-03-27

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19990914