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BRPI1008068A2 - nacela de motor turbojato - Google Patents

nacela de motor turbojato

Info

Publication number
BRPI1008068A2
BRPI1008068A2 BRPI1008068A BRPI1008068A BRPI1008068A2 BR PI1008068 A2 BRPI1008068 A2 BR PI1008068A2 BR PI1008068 A BRPI1008068 A BR PI1008068A BR PI1008068 A BRPI1008068 A BR PI1008068A BR PI1008068 A2 BRPI1008068 A2 BR PI1008068A2
Authority
BR
Brazil
Prior art keywords
turbojet engine
engine nacelle
nacelle
turbojet
engine
Prior art date
Application number
BRPI1008068A
Other languages
English (en)
Inventor
Guy Bernard Vauchel
Stephane Beilliard
Original Assignee
Aircelle 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 Aircelle Sa filed Critical Aircelle Sa
Publication of BRPI1008068A2 publication Critical patent/BRPI1008068A2/pt

Links

Classifications

    • 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
    • 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
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F05D2250/41—Movement of components with one degree of freedom
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • 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]
    • 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]
    • Y10T137/0645—With condition responsive control means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
BRPI1008068A 2009-02-04 2010-02-01 nacela de motor turbojato BRPI1008068A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0950685A FR2941674B1 (fr) 2009-02-04 2009-02-04 Nacelle de turboreacteur.
PCT/FR2010/050154 WO2010089498A2 (fr) 2009-02-04 2010-02-01 Nacelle de turboréacteur

Publications (1)

Publication Number Publication Date
BRPI1008068A2 true BRPI1008068A2 (pt) 2016-03-15

Family

ID=40906859

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1008068A BRPI1008068A2 (pt) 2009-02-04 2010-02-01 nacela de motor turbojato

Country Status (9)

Country Link
US (1) US8820344B2 (pt)
EP (1) EP2393713B1 (pt)
CN (1) CN102307784B (pt)
BR (1) BRPI1008068A2 (pt)
CA (1) CA2751121A1 (pt)
ES (1) ES2535411T3 (pt)
FR (1) FR2941674B1 (pt)
RU (1) RU2524321C2 (pt)
WO (1) WO2010089498A2 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9211955B1 (en) * 2012-12-10 2015-12-15 The Boeing Company Methods and apparatus for supporting engines and nacelles relative to aircraft wings
FR3010051B1 (fr) 2013-08-29 2015-09-11 Aircelle Sa Capot avant pour une nacelle de turboreacteur comportant un systeme de manœuvre
ES2763875T3 (es) * 2015-12-15 2020-06-01 Airbus Operations Sl Sistema de suspensión para una unidad de potencia auxiliar
US10837362B2 (en) 2016-10-12 2020-11-17 General Electric Company Inlet cowl for a turbine engine
BE1025077B1 (fr) * 2017-03-22 2018-10-23 Safran Aero Boosters S.A. Capot de turbomachine avec ecran
FR3095416B1 (fr) * 2019-04-26 2021-04-23 Safran Nacelles Entrée d’air de nacelle de turboréacteur
US11390393B2 (en) * 2019-06-04 2022-07-19 Rohr, Inc. Nacelle with a translatable inlet for an aircraft propulsion system
US11866251B2 (en) * 2021-05-06 2024-01-09 Ovivo Inc. Seal for cover on wastewater treatment tank
EP4501793A1 (fr) * 2023-07-31 2025-02-05 Airbus Operations (S.A.S.) Entrée d air d aéronef comprenant une paroi extérieure et des cadres avant et arrière reliés par au moins un élément de jonction distinct de la paroi extérieure
EP4644256A1 (fr) 2024-04-29 2025-11-05 Airbus (S.A.S.) Lèvre d'entrée d'air pour une nacelle d'un turboréacteur double flux d'aéronef

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE425257A (pt) *
FR800845A (fr) 1935-04-18 1936-07-20 Procédé d'insolation des minerais en présence de matières radio-actives
GB1382809A (en) * 1971-12-04 1975-02-05 Rolls Royce Air intakes for gas turbine engines
DE2642523A1 (de) * 1976-09-22 1978-03-23 Burkhart Dipl Ing Grob Verfahren und vorrichtung zur herstellung eines flugzeugbauteils in profilverstaerkter schalenbauweise
US5000399A (en) * 1990-02-23 1991-03-19 General Electric Company Variable contour annular air inlet for an aircraft engine nacelle
GB9301457D0 (en) * 1993-01-26 1993-03-17 Short Brothers Plc An aircraft propulsuve power unit
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
RU2210523C1 (ru) * 2001-12-14 2003-08-20 Открытое акционерное общество "Авиационный комплекс им. С.В. Ильюшина" Гондола силовой установки летательного аппарата
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
FR2927609B1 (fr) 2008-02-18 2010-06-25 Aircelle Sa Entree d'air pour nacelle d'aeronef, et nacelle equipee d'une telle entree d'air

Also Published As

Publication number Publication date
ES2535411T3 (es) 2015-05-11
CN102307784A (zh) 2012-01-04
CN102307784B (zh) 2014-10-08
EP2393713B1 (fr) 2015-02-25
CA2751121A1 (fr) 2010-08-12
RU2011136050A (ru) 2013-03-10
RU2524321C2 (ru) 2014-07-27
US20110284095A1 (en) 2011-11-24
US8820344B2 (en) 2014-09-02
FR2941674B1 (fr) 2011-02-11
EP2393713A2 (fr) 2011-12-14
WO2010089498A3 (fr) 2010-11-25
FR2941674A1 (fr) 2010-08-06
WO2010089498A2 (fr) 2010-08-12

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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 7A ANUIDADE.

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