BRPI0818497A2 - Estrutura de entrada de ar para ser montada a montante de uma estrutura intermediária de nacela para motor de avião, e nacela equipada com tal estrutura de entrada de ar. - Google Patents
Estrutura de entrada de ar para ser montada a montante de uma estrutura intermediária de nacela para motor de avião, e nacela equipada com tal estrutura de entrada de ar.Info
- Publication number
- BRPI0818497A2 BRPI0818497A2 BRPI0818497A BRPI0818497A2 BR PI0818497 A2 BRPI0818497 A2 BR PI0818497A2 BR PI0818497 A BRPI0818497 A BR PI0818497A BR PI0818497 A2 BRPI0818497 A2 BR PI0818497A2
- Authority
- BR
- Brazil
- Prior art keywords
- frame
- air inlet
- nacelle
- inlet frame
- aircraft engine
- Prior art date
Links
- 238000011144 upstream manufacturing Methods 0.000 title 1
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
-
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/04—Hot gas application
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Centrifugal Separators (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0707049A FR2921901B1 (fr) | 2007-10-08 | 2007-10-08 | 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 |
PCT/FR2008/001208 WO2009060137A2 (fr) | 2007-10-08 | 2008-08-28 | 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 |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0818497A2 true BRPI0818497A2 (pt) | 2015-04-22 |
Family
ID=39400863
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0818497 BRPI0818497A2 (pt) | 2007-10-08 | 2008-08-28 | Estrutura de entrada de ar para ser montada a montante de uma estrutura intermediária de nacela para motor de avião, e nacela equipada com tal estrutura de entrada de ar. |
Country Status (8)
Country | Link |
---|---|
US (1) | US8800258B2 (pt) |
EP (1) | EP2197743A2 (pt) |
CN (1) | CN101855135A (pt) |
BR (1) | BRPI0818497A2 (pt) |
CA (1) | CA2700087A1 (pt) |
FR (1) | FR2921901B1 (pt) |
RU (1) | RU2486106C2 (pt) |
WO (1) | WO2009060137A2 (pt) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2927882B1 (fr) | 2008-02-27 | 2010-02-12 | Aircelle Sa | Structure d'entree d'air pour une nacelle d'un aeronef |
FR2954280B1 (fr) * | 2009-12-18 | 2012-03-23 | Airbus Operations Sas | Entree d'air d'une nacelle d'aeronef comprenant un traitement du givre optimise |
FR2961175B1 (fr) * | 2010-06-14 | 2013-01-04 | Aircelle Sa | Nacelle de turboreacteur |
US9309781B2 (en) * | 2011-01-31 | 2016-04-12 | General Electric Company | Heated booster splitter plenum |
FR2975435B1 (fr) * | 2011-05-16 | 2016-09-02 | Snecma | Dispositif de degivrage d'un bec de separation de turbomachine |
DE102012000890A1 (de) * | 2012-01-18 | 2013-07-18 | Rolls-Royce Deutschland Ltd & Co Kg | Befestigungselement und Enteisungsvorrichtung eines Fluggasturbinentriebwerks |
DE102012023718A1 (de) | 2012-12-05 | 2014-06-05 | Eads Deutschland Gmbh | Einlauf für ein Triebwerk eines Luftfahrzeugs |
US10266273B2 (en) | 2013-07-26 | 2019-04-23 | Mra Systems, Llc | Aircraft engine pylon |
ITUB20151085A1 (it) * | 2015-05-28 | 2016-11-28 | Alenia Aermacchi Spa | Gondola per motore aeronautico con sistema antighiaccio utilizzante un fluido bifase. |
BE1023289B1 (fr) * | 2015-07-17 | 2017-01-24 | Safran Aero Boosters S.A. | Bec de separation de compresseur basse pression de turbomachine axiale avec conduit annulaire de degivrage |
RU177304U1 (ru) * | 2017-08-29 | 2018-02-15 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Труба подвода горячего воздуха к противообледенительной системе |
FR3072421B1 (fr) * | 2017-10-18 | 2019-09-27 | Airbus Operations | Levre d'entree d'air d'un moteur d'aeronef comportant un systeme de degivrage |
FR3087477A1 (fr) * | 2018-10-22 | 2020-04-24 | Safran Aircraft Engines | Dispositif de degivrage d'un bec de turbomachine |
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 |
FR3094698B1 (fr) * | 2019-04-02 | 2022-09-09 | Safran Aircraft Engines | Manche d’entree d’air pour une nacelle d’un ensemble propulsif d’aeronef |
US11085328B2 (en) * | 2019-09-09 | 2021-08-10 | Rohr, Inc. | Assembly for sealing an annular gap between an inner structure and an outer structure |
RU203051U1 (ru) * | 2020-10-23 | 2021-03-19 | Михаил Николаевич Киселёв | Устройство создания тяги от встречного потока текучей среды |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR608599A (fr) | 1925-03-31 | 1926-07-29 | Perfectionnements aux machines automatiques à fabriquer les bouteilles et autres objets creux en verre | |
SU435983A1 (ru) * | 1972-12-15 | 1974-07-15 | Н. Д. Березовский , Г. А. Бершов | Роликовый редуктор |
IL78786A0 (en) * | 1985-06-03 | 1986-08-31 | Short Brothers Plc | Duct for hot air |
FR2757823B1 (fr) * | 1996-12-26 | 1999-03-12 | Aerospatiale | Nacelle de turboreacteur a ecoulement laminaire |
FR2771452B1 (fr) * | 1997-11-21 | 2000-04-14 | Aerospatiale | Dispositif de degivrage pour capot d'entree d'air de moteur a reaction |
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 |
-
2007
- 2007-10-08 FR FR0707049A patent/FR2921901B1/fr not_active Expired - Fee Related
-
2008
- 2008-08-28 WO PCT/FR2008/001208 patent/WO2009060137A2/fr active Application Filing
- 2008-08-28 BR BRPI0818497 patent/BRPI0818497A2/pt not_active IP Right Cessation
- 2008-08-28 EP EP08846454A patent/EP2197743A2/fr not_active Withdrawn
- 2008-08-28 RU RU2010117280/11A patent/RU2486106C2/ru not_active IP Right Cessation
- 2008-08-28 CN CN200880108535A patent/CN101855135A/zh active Pending
- 2008-08-28 CA CA2700087A patent/CA2700087A1/fr not_active Abandoned
- 2008-08-28 US US12/681,994 patent/US8800258B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
RU2486106C2 (ru) | 2013-06-27 |
FR2921901B1 (fr) | 2011-03-18 |
WO2009060137A2 (fr) | 2009-05-14 |
WO2009060137A3 (fr) | 2010-07-29 |
US8800258B2 (en) | 2014-08-12 |
RU2010117280A (ru) | 2011-11-20 |
EP2197743A2 (fr) | 2010-06-23 |
CN101855135A (zh) | 2010-10-06 |
US20100242428A1 (en) | 2010-09-30 |
FR2921901A1 (fr) | 2009-04-10 |
CA2700087A1 (fr) | 2009-05-14 |
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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 8A 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 2385 DE 20-09-2016 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. |