FR2625261B1 - INVERTER OF TURBOREACTOR DRIVE WITH OBSTACLES LINKED TO THE PRIMARY HOOD - Google Patents

INVERTER OF TURBOREACTOR DRIVE WITH OBSTACLES LINKED TO THE PRIMARY HOOD

Info

Publication number
FR2625261B1
FR2625261B1 FR8717992A FR8717992A FR2625261B1 FR 2625261 B1 FR2625261 B1 FR 2625261B1 FR 8717992 A FR8717992 A FR 8717992A FR 8717992 A FR8717992 A FR 8717992A FR 2625261 B1 FR2625261 B1 FR 2625261B1
Authority
FR
France
Prior art keywords
obstacles
inverter
linked
primary hood
turboreactor
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 - Lifetime
Application number
FR8717992A
Other languages
French (fr)
Other versions
FR2625261A1 (en
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.)
Safran Transmission Systems SAS
Original Assignee
Hispano Suiza SA
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 Hispano Suiza SA filed Critical Hispano Suiza SA
Priority to FR8717992A priority Critical patent/FR2625261B1/en
Publication of FR2625261A1 publication Critical patent/FR2625261A1/en
Application granted granted Critical
Publication of FR2625261B1 publication Critical patent/FR2625261B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/64Reversing fan flow
    • F02K1/68Reversers mounted on the engine housing downstream of the fan exhaust section
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/64Reversing fan flow
    • F02K1/70Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing

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)
FR8717992A 1987-12-23 1987-12-23 INVERTER OF TURBOREACTOR DRIVE WITH OBSTACLES LINKED TO THE PRIMARY HOOD Expired - Lifetime FR2625261B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8717992A FR2625261B1 (en) 1987-12-23 1987-12-23 INVERTER OF TURBOREACTOR DRIVE WITH OBSTACLES LINKED TO THE PRIMARY HOOD

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8717992A FR2625261B1 (en) 1987-12-23 1987-12-23 INVERTER OF TURBOREACTOR DRIVE WITH OBSTACLES LINKED TO THE PRIMARY HOOD

Publications (2)

Publication Number Publication Date
FR2625261A1 FR2625261A1 (en) 1989-06-30
FR2625261B1 true FR2625261B1 (en) 1992-11-06

Family

ID=9358197

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8717992A Expired - Lifetime FR2625261B1 (en) 1987-12-23 1987-12-23 INVERTER OF TURBOREACTOR DRIVE WITH OBSTACLES LINKED TO THE PRIMARY HOOD

Country Status (1)

Country Link
FR (1) FR2625261B1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2676780B1 (en) * 1991-05-23 1993-08-13 Snecma PUSH INVERTER FOR VERY HIGH DILUTION TURBOSOUFFLANTE.
FR2712929B1 (en) * 1993-11-24 1995-12-29 Hispano Suiza Sa Dual flow turbojet thrust reverser.
FR2721977B1 (en) * 1994-06-30 1996-08-02 Hispano Suiza Sa DOUBLE-FLOW TURBOREACTOR DRIVE INVERTER WITH PRIMARY HOOD-RELATED OBSTACLES
FR2749041B1 (en) * 1996-05-23 1998-06-26 Hispano Suiza Sa DOUBLE FLOW TURBOREACTOR DRIVE INVERTER WITH PRIMARY HOOD OBSTACLES
FR2759418B1 (en) * 1997-02-13 1999-03-19 Snecma PUSH INVERTER FOR VERY HIGH DILUTION TURBOSOFFICE
FR2766522B1 (en) * 1997-07-24 1999-09-03 Hispano Suiza Sa TURBO BLOWER THRUST INVERTER WITH OBSTACLE WITH AXIAL GUIDANCE LINKED TO THE PRIMARY COVER
FR2866070B1 (en) 2004-02-05 2008-12-05 Snecma Moteurs TURBOREACTOR WITH HIGH DILUTION RATE

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2839891A (en) * 1953-11-27 1958-06-24 Boeing Co Thrust reversers for jet engines
US3280561A (en) * 1965-06-07 1966-10-25 Gen Electric Thrust reverser mechanism

Also Published As

Publication number Publication date
FR2625261A1 (en) 1989-06-30

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
ST Notification of lapse