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FR2887225B1 - Nacelle d'aeronef, et aeronef muni d'au moins une telle nacelle - Google Patents

Nacelle d'aeronef, et aeronef muni d'au moins une telle nacelle

Info

Publication number
FR2887225B1
FR2887225B1 FR0551689A FR0551689A FR2887225B1 FR 2887225 B1 FR2887225 B1 FR 2887225B1 FR 0551689 A FR0551689 A FR 0551689A FR 0551689 A FR0551689 A FR 0551689A FR 2887225 B1 FR2887225 B1 FR 2887225B1
Authority
FR
France
Prior art keywords
nacelle
aircraft
aircraft equipped
aircraft nacelle
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
FR0551689A
Other languages
English (en)
Other versions
FR2887225A1 (fr
Inventor
Eric Delmas
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0551689A priority Critical patent/FR2887225B1/fr
Publication of FR2887225A1 publication Critical patent/FR2887225A1/fr
Application granted granted Critical
Publication of FR2887225B1 publication Critical patent/FR2887225B1/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
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • 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
    • F02K1/58—Reversers mounted on the inner cone or the nozzle housing or the fuselage
    • 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
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)
FR0551689A 2005-06-21 2005-06-21 Nacelle d'aeronef, et aeronef muni d'au moins une telle nacelle Expired - Fee Related FR2887225B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0551689A FR2887225B1 (fr) 2005-06-21 2005-06-21 Nacelle d'aeronef, et aeronef muni d'au moins une telle nacelle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0551689A FR2887225B1 (fr) 2005-06-21 2005-06-21 Nacelle d'aeronef, et aeronef muni d'au moins une telle nacelle

Publications (2)

Publication Number Publication Date
FR2887225A1 FR2887225A1 (fr) 2006-12-22
FR2887225B1 true FR2887225B1 (fr) 2008-09-19

Family

ID=35788352

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0551689A Expired - Fee Related FR2887225B1 (fr) 2005-06-21 2005-06-21 Nacelle d'aeronef, et aeronef muni d'au moins une telle nacelle

Country Status (1)

Country Link
FR (1) FR2887225B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7673442B2 (en) 2006-11-14 2010-03-09 General Electric Company Turbofan engine cowl assembly
FR2935354B1 (fr) 2008-09-02 2011-04-01 Airbus France Nacelle pour moteur a double flux
FR2927310B1 (fr) * 2008-02-13 2010-07-30 Aircelle Sa Systeme de commande pour nacelle de turboreacteur
FR2933143B1 (fr) 2008-06-26 2011-06-10 Airbus France Nacelle pour aeronef comportant des moyens inverseurs de poussee et aeronef comportant au moins une telle nacelle
FR2933144B1 (fr) 2008-06-26 2012-08-17 Airbus France Nacelle pour aeronef comportant des moyens inverseurs de poussee et aeronef comportant au moins une telle nacelle
FR2935444B1 (fr) 2008-09-02 2010-09-10 Airbus France Inverseur de poussee et nacelle pour aeronef muni d'au moins un tel inverseur
FR2966432B1 (fr) * 2010-10-26 2013-08-30 Airbus Operations Sas Capot d'aeronef incorporant des moyens pour limiter les phenomenes d'ecope de type magnetique
FR3085727A1 (fr) * 2018-09-06 2020-03-13 Airbus Operations Turboreacteur comportant une nacelle equipee d'un systeme inverseur comportant des portes interieures et des volets exterieurs
FR3091691A1 (fr) 2019-01-14 2020-07-17 Airbus Operations NACELLE D’UN TURBOREACTEUR COMPORTANT UNE porte d’inversion ET UN SYSTEME D’AIDE AU DEPLOIEMENT De la porte d’inversion
CN111520252A (zh) * 2020-05-26 2020-08-11 浙江科技学院 一种航空发动机反推组件

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2798362A (en) * 1954-03-01 1957-07-09 Armstrong Siddeley Motors Ltd Means for slowing down an aircraft, particularly during landing, when powered by a turbo-jet
DE1054848B (de) * 1956-04-27 1959-04-09 Armstrong Siddeley Motors Ltd Vorrichtung zur Schubumkehr bei einem Strahltriebwerk eines Flugzeugs
GB1127828A (en) * 1966-06-29 1968-09-18 Rolls Royce Fan thrust reverser for jet propulsion plant
US3612401A (en) * 1970-01-29 1971-10-12 Rohr Corp Thrust-reversing apparatus for turbofan jet engine
US3815357A (en) * 1971-01-28 1974-06-11 Rohr Industries Inc Thrust reversing apparatus
RU2044912C1 (ru) * 1992-11-02 1995-09-27 Акционерное общество открытого типа "Авиадвигатель" Реверсивное устройство

Also Published As

Publication number Publication date
FR2887225A1 (fr) 2006-12-22

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Legal Events

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Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

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Year of fee payment: 12

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Effective date: 20210206