BRPI0908256A2 - Estrutura de entrada de ar capaz de ser montada a montante de estrutura central de nacela de motor de avião e nacela de motor de avião - Google Patents

Estrutura de entrada de ar capaz de ser montada a montante de estrutura central de nacela de motor de avião e nacela de motor de avião

Info

Publication number
BRPI0908256A2
BRPI0908256A2 BRPI0908256-5A BRPI0908256A BRPI0908256A2 BR PI0908256 A2 BRPI0908256 A2 BR PI0908256A2 BR PI0908256 A BRPI0908256 A BR PI0908256A BR PI0908256 A2 BRPI0908256 A2 BR PI0908256A2
Authority
BR
Brazil
Prior art keywords
aircraft engine
engine nacelle
hot air
supply tube
upstream
Prior art date
Application number
BRPI0908256-5A
Other languages
English (en)
Inventor
Guy Vauchel
Stéphane 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 BRPI0908256A2 publication Critical patent/BRPI0908256A2/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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • F02C7/047—Heating to prevent icing
    • 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangements 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—Arrangements 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Sealing Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Gasket Seals (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Helmets And Other Head Coverings (AREA)
BRPI0908256-5A 2008-02-27 2009-01-28 Estrutura de entrada de ar capaz de ser montada a montante de estrutura central de nacela de motor de avião e nacela de motor de avião BRPI0908256A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0801071A FR2927882B1 (fr) 2008-02-27 2008-02-27 Structure d'entree d'air pour une nacelle d'un aeronef
PCT/FR2009/000095 WO2009112695A1 (fr) 2008-02-27 2009-01-28 Structure d'entrée d'air pour une nacelle d'un aéronef

Publications (1)

Publication Number Publication Date
BRPI0908256A2 true BRPI0908256A2 (pt) 2015-07-21

Family

ID=39854417

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0908256-5A BRPI0908256A2 (pt) 2008-02-27 2009-01-28 Estrutura de entrada de ar capaz de ser montada a montante de estrutura central de nacela de motor de avião e nacela de motor de avião

Country Status (10)

Country Link
US (1) US8777164B2 (pt)
EP (1) EP2250357B1 (pt)
CN (1) CN101952573B (pt)
AT (1) ATE535694T1 (pt)
BR (1) BRPI0908256A2 (pt)
CA (1) CA2713471A1 (pt)
ES (1) ES2378030T3 (pt)
FR (1) FR2927882B1 (pt)
RU (1) RU2480598C2 (pt)
WO (1) WO2009112695A1 (pt)

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CN102439141A (zh) * 2009-02-06 2012-05-02 吉联亚生物科技有限公司 治疗新生血管形成的方法和组合物
FR2954279B1 (fr) * 2009-12-18 2014-08-22 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef integrant des moyens d'injection en air chaud pour le traitement du givre optimises
FR2961789B1 (fr) * 2010-06-24 2012-07-20 Eurocopter France Procede pour eviter le colmatage d'une grille, grille et entree d'air mettant en oeuvre un tel procede
JP5582927B2 (ja) * 2010-08-30 2014-09-03 三菱重工業株式会社 航空機の防除氷システム及びこれを備える航空機
FR2975435B1 (fr) * 2011-05-16 2016-09-02 Snecma Dispositif de degivrage d'un bec de separation de turbomachine
US20140263837A1 (en) * 2013-03-12 2014-09-18 Spirit Aerosystems, Inc. Nacelle inlet thermal anti-ice spray duct
US9528442B2 (en) * 2013-08-21 2016-12-27 The Boeing Company Aircraft engine anti-icing (EAI) barrier assembly, system and method
CN103758588B (zh) * 2014-02-19 2015-09-09 襄阳三鹏航空科技有限公司 一种飞机用涡轮增压器的外壳机构及其制造工艺
US10138811B2 (en) * 2014-03-13 2018-11-27 The Boeing Company Enhanced temperature control anti-ice nozzle
CA2975844C (en) * 2015-02-05 2023-09-19 Bombardier Inc. Apparatus for obstructing air flow through an aperture for a duct in an aircraft wing
US10100734B2 (en) * 2015-02-24 2018-10-16 Honeywell International Inc. Multi-channel particle separator
US10723464B2 (en) 2015-08-26 2020-07-28 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
US10393020B2 (en) * 2015-08-26 2019-08-27 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
US10189572B2 (en) * 2016-05-02 2019-01-29 The Boeing Company Systems and methods for preventing ice formation on portions of an aircraft
US20170314412A1 (en) * 2016-05-02 2017-11-02 General Electric Company Dimpled Naccelle Inner Surface for Heat Transfer Improvement
CN105863845B (zh) * 2016-06-07 2017-12-15 中国南方航空工业(集团)有限公司 结冰指示系统
US20180229850A1 (en) * 2017-02-15 2018-08-16 Pratt & Whitney Canada Corp. Anti-icing system for gas turbine engine
CN107654295B (zh) * 2017-12-13 2019-07-19 中国航空工业集团公司沈阳飞机设计研究所 一种单侧安装的进气道密封组件
US11220344B2 (en) * 2018-12-17 2022-01-11 Rohr, Inc. Anti-ice double walled duct system
US10989116B2 (en) 2019-03-05 2021-04-27 Rohr, Inc. Inlet anti-ice double walled duct with supply line seal
CN112572807A (zh) * 2020-12-21 2021-03-30 中国商用飞机有限责任公司 飞机上具有喷射气流的笛形管防冰装置

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FR2771452B1 (fr) * 1997-11-21 2000-04-14 Aerospatiale Dispositif de degivrage pour capot d'entree d'air de moteur a reaction
FR2772341B1 (fr) * 1997-12-12 2000-03-24 Aerospatiale Diffuseur d'air chaud pour capot d'entree d'air de moteur a reaction a circuit de degivrage
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FR2886674B1 (fr) * 2005-06-07 2007-08-03 Airbus France Sas Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur
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FR2921901B1 (fr) 2007-10-08 2011-03-18 Aircelle Sa Structure d'entree d'air apte a etre montee en amont d'une structure mediane de nacelle pour moteur d'aeronef, et nacelle equipee d'une telle structure d'entree d'air
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Also Published As

Publication number Publication date
CN101952573B (zh) 2013-07-17
RU2010139200A (ru) 2012-04-10
CA2713471A1 (fr) 2009-09-17
ATE535694T1 (de) 2011-12-15
CN101952573A (zh) 2011-01-19
US8777164B2 (en) 2014-07-15
US20110011981A1 (en) 2011-01-20
EP2250357B1 (fr) 2011-11-30
FR2927882B1 (fr) 2010-02-12
EP2250357A1 (fr) 2010-11-17
WO2009112695A1 (fr) 2009-09-17
FR2927882A1 (fr) 2009-08-28
ES2378030T3 (es) 2012-04-04
RU2480598C2 (ru) 2013-04-27

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 8A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2395 DE 29-11-2016 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.