BRPI1007811A2 - nacela de turborreator, e, turborreator - Google Patents

nacela de turborreator, e, turborreator

Info

Publication number
BRPI1007811A2
BRPI1007811A2 BRPI1007811A BRPI1007811A BRPI1007811A2 BR PI1007811 A2 BRPI1007811 A2 BR PI1007811A2 BR PI1007811 A BRPI1007811 A BR PI1007811A BR PI1007811 A BRPI1007811 A BR PI1007811A BR PI1007811 A2 BRPI1007811 A2 BR PI1007811A2
Authority
BR
Brazil
Prior art keywords
turborreator
nacelle
turborreator nacelle
Prior art date
Application number
BRPI1007811A
Other languages
English (en)
Inventor
Hervé Jean Albert Mouton
Thomas Alain Christian Vincent
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BRPI1007811A2 publication Critical patent/BRPI1007811A2/pt

Links

Classifications

    • 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
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BRPI1007811A 2009-02-24 2010-02-04 nacela de turborreator, e, turborreator BRPI1007811A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0951154A FR2942457B1 (fr) 2009-02-24 2009-02-24 Nacelle de turboreacteur a structure d'entree d'air amovible
PCT/FR2010/050175 WO2010097532A1 (fr) 2009-02-24 2010-02-04 Nacelle de turboreacteur a structure d'entree d'air amovible

Publications (1)

Publication Number Publication Date
BRPI1007811A2 true BRPI1007811A2 (pt) 2016-02-23

Family

ID=41061300

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1007811A BRPI1007811A2 (pt) 2009-02-24 2010-02-04 nacela de turborreator, e, turborreator

Country Status (9)

Country Link
US (1) US8899255B2 (pt)
EP (1) EP2401202A1 (pt)
JP (1) JP2012518738A (pt)
CN (1) CN102333697A (pt)
BR (1) BRPI1007811A2 (pt)
CA (1) CA2752533A1 (pt)
FR (1) FR2942457B1 (pt)
RU (1) RU2011139140A (pt)
WO (1) WO2010097532A1 (pt)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2972224B1 (fr) * 2011-03-04 2018-04-20 Safran Aircraft Engines Tuyere avec noyau aval presentant une forte courbure
DE102011103163A1 (de) 2011-06-01 2012-12-06 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinentriebwerk mit teleskopartigem Lufteinlass der Triebwerksverkleidung
EP2750972B1 (en) * 2011-09-02 2017-08-02 The Boeing Company Motion restrictor system for an aircraft engine
FR3001713B1 (fr) * 2013-02-05 2016-07-15 Astrium Sas Dispositif de retenue d'un reservoir dans un aeronef
FR3001714B1 (fr) * 2013-02-05 2016-08-26 Astrium Sas Dispositif de support et de maintien de reservoirs cryogeniques
CN104691741B (zh) * 2013-12-06 2017-11-10 中国航发商用航空发动机有限责任公司 航空发动机短舱
US10040560B2 (en) * 2015-09-30 2018-08-07 The Boeing Company Trailing edge core compartment vent for an aircraft engine
US10428763B2 (en) * 2016-04-01 2019-10-01 Rohr, Inc. Controlling a relative position at an interface between translating structures of an aircraft nacelle
US20170283081A1 (en) * 2016-04-05 2017-10-05 Rohr, Inc. Securing a translating fanlet for an aircraft propulsion system nacelle
US10837362B2 (en) 2016-10-12 2020-11-17 General Electric Company Inlet cowl for a turbine engine
FR3086643B1 (fr) * 2018-09-28 2021-05-28 Safran Nacelles Nacelle pour aeronef et entree d'air associee
US11390393B2 (en) * 2019-06-04 2022-07-19 Rohr, Inc. Nacelle with a translatable inlet for an aircraft propulsion system
FR3101854B1 (fr) * 2019-10-15 2024-05-31 Inst Superieur De L Aeronautique Et De L Espace Nacelle de turbomachine
US11866189B2 (en) * 2020-03-26 2024-01-09 Hartwell Corporation Latching system with movable anti-shear mechanism
US12420938B2 (en) 2023-05-01 2025-09-23 Rohr, Inc. Misalignment latch for an aircraft system

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2599037A (en) * 1947-07-26 1952-06-03 Boeing Co Quick-dismountable cowling
GB1353678A (en) * 1971-09-15 1974-05-22 Rolls Royce Air intake for a gas turbine engine
US4320912A (en) * 1979-09-10 1982-03-23 Rohr Industries, Inc. Cowl door latch adjustment fitting assembly
US4365775A (en) * 1980-12-08 1982-12-28 The Boeing Company Cowl structure alignment and shear device
US4658579A (en) * 1983-07-14 1987-04-21 United Technologies Corporation Load sharing for engine nacelle
US5014933A (en) * 1989-04-27 1991-05-14 The Boeing Company Translating lip aircraft cowling structure adapted for noise reduction
US5000399A (en) * 1990-02-23 1991-03-19 General Electric Company Variable contour annular air inlet for an aircraft engine nacelle
FR2731049B1 (fr) * 1995-02-28 1997-05-09 Aerospatiale Dispositif de fixation d'une bouche d'entree d'air sur un reacteur et reacteur comportant un tel dispositif
FR2835870B1 (fr) * 2002-02-14 2005-03-11 Airbus France Systeme de fermeture interpose entre deux elements
FR2868124B1 (fr) * 2004-03-29 2006-06-23 Airbus France Sas Structure d'entree d'air pour moteur d'aeronef
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
FR2926537B1 (fr) * 2008-01-18 2010-02-12 Aircelle Sa Systeme de verrouillage pour structure d'entree d'air d'une nacelle de turboreacteur
FR2927061B1 (fr) * 2008-02-01 2010-02-12 Aircelle Sa Systeme de verrouillage pour structure d'entree d'air d'une nacelle de turboreacteur
FR2931205B1 (fr) * 2008-05-16 2010-05-14 Aircelle Sa Ensemble propulsif pour aeronef, et structure d'entree d'air pour un tel ensemble
US8181905B2 (en) * 2008-12-17 2012-05-22 Rohr, Inc. Aircraft engine nacelle with translating inlet cowl

Also Published As

Publication number Publication date
EP2401202A1 (fr) 2012-01-04
CA2752533A1 (fr) 2010-09-02
FR2942457A1 (fr) 2010-08-27
WO2010097532A1 (fr) 2010-09-02
CN102333697A (zh) 2012-01-25
US8899255B2 (en) 2014-12-02
FR2942457B1 (fr) 2011-04-22
JP2012518738A (ja) 2012-08-16
RU2011139140A (ru) 2013-04-10
US20110308634A1 (en) 2011-12-22

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Legal Events

Date Code Title Description
B08F Application fees: dismissal - article 86 of industrial property law

Free format text: REFERENTE A 6A ANUIDADE.

B08K Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2383 DE 06-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.