BRPI0418168A - canal de ar dinámico para o suprimento de ar ambiente em uma aeronave, e, processo para a operação de um canal de ar dinámico - Google Patents
canal de ar dinámico para o suprimento de ar ambiente em uma aeronave, e, processo para a operação de um canal de ar dinámicoInfo
- Publication number
- BRPI0418168A BRPI0418168A BRPI0418168-9A BRPI0418168A BRPI0418168A BR PI0418168 A BRPI0418168 A BR PI0418168A BR PI0418168 A BRPI0418168 A BR PI0418168A BR PI0418168 A BRPI0418168 A BR PI0418168A
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- dynamic
- air duct
- dynamic air
- air
- Prior art date
Links
- 239000003570 air Substances 0.000 title abstract 8
- 239000012080 ambient air Substances 0.000 title abstract 3
- 230000007613 environmental effect Effects 0.000 abstract 1
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
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
-
- 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
- F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
-
- 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
- Y02T50/50—On board measures aiming to increase energy efficiency
-
- 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)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- General Health & Medical Sciences (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Air-Flow Control Members (AREA)
- Duct Arrangements (AREA)
- Mobile Radio Communication Systems (AREA)
Abstract
CANAL DE AR DINáMICO PARA O SUPRIMENTO DE AR AMBIENTE EM UMA AERONAVE, E , PROCESSO PARA A OPERAçãO DE UM CANAL DE AR DINáMICO Um canal de ar dinâmico (10) para o suprimento de ar ambiente em uma aeronave inclui uma primeira entrada de ar (12) e um canal de fluxo principal (16) que se estende a jusante da primeira entrada de ar (12). Para garantir que os sistemas a bordo da aeronave sejam supridos, de uma maneira simples e confiável, com requerido ar ambiente em qualquer estado operacional da aeronave, esto é tanto durante o vóo quanto no solo, o canal de ar dinâmico (10) tem uma segunda entrada de ar (24) que é indeoendente da primeira entrada de ar (12).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2003161722 DE10361722B4 (de) | 2003-12-30 | 2003-12-30 | Stauluftkanal zur Umgebungsluftzufuhr in einem Flugzeug |
| PCT/EP2004/014864 WO2005063579A1 (en) | 2003-12-30 | 2004-12-30 | Ram air channel for the supply of ambient air in an aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0418168A true BRPI0418168A (pt) | 2007-06-19 |
Family
ID=34716262
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0418168-9A BRPI0418168A (pt) | 2003-12-30 | 2004-12-30 | canal de ar dinámico para o suprimento de ar ambiente em uma aeronave, e, processo para a operação de um canal de ar dinámico |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US7832684B2 (pt) |
| EP (1) | EP1699698B1 (pt) |
| JP (1) | JP4614972B2 (pt) |
| CN (1) | CN100586796C (pt) |
| BR (1) | BRPI0418168A (pt) |
| CA (1) | CA2552166C (pt) |
| DE (2) | DE10361722B4 (pt) |
| RU (1) | RU2376209C2 (pt) |
| WO (1) | WO2005063579A1 (pt) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102008026117A1 (de) * | 2008-05-30 | 2009-12-10 | Airbus Deutschland Gmbh | Frischlufteinlass für ein Flugzeug |
| DE102008002205A1 (de) * | 2008-06-04 | 2009-12-17 | Airbus Deutschland Gmbh | Lufteinlassventil für ein Flugzeug und Herstellungsverfahren für ein Lufteinlassventil |
| DE102008030399B4 (de) * | 2008-06-26 | 2019-03-21 | Airbus Operations Gmbh | Luftkanal zur Umgebungsluftzufuhr in einem Flugzeug |
| US20110265490A1 (en) * | 2010-04-30 | 2011-11-03 | Kevin Samuel Klasing | Flow mixing vent system |
| US9140272B2 (en) * | 2011-10-24 | 2015-09-22 | Hamilton Sundstrand Corporation | Ram air fan outer housing |
| US10059430B2 (en) | 2014-06-25 | 2018-08-28 | Gulfstream Aerospace Corporation | Aircraft air scoop systems with passive pneumatic actuators |
| DE102015216499A1 (de) | 2015-08-28 | 2017-03-02 | Airbus Operations Gmbh | Verfahren und System zur Ventilation eines Flugzeugbereichs |
| US9611034B1 (en) * | 2015-11-03 | 2017-04-04 | United Technologies Corporation | Wide fuselage aircraft with increased boundary layer ingestion |
| US11035295B2 (en) | 2018-04-18 | 2021-06-15 | Lockheed Martin Corporation | Engine nacelle heat exchanger |
| EP3587273B1 (en) * | 2018-06-22 | 2023-10-11 | Airbus Operations, S.L.U. | Air intake system |
| CN112678186B (zh) * | 2021-01-19 | 2023-01-31 | 中国商用飞机有限责任公司 | 飞机环控空气进气口流量调节装置 |
Family Cites Families (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2604278A (en) * | 1943-07-02 | 1952-07-22 | Power Jets Res & Dev Ltd | Gas turbine aircraft propulsion installation with auxiliary air intake |
| US2699906A (en) * | 1949-10-25 | 1955-01-18 | Northrop Aircraft Inc | Air inlet for airplane gaseous combustion turbine engines |
| US3222863A (en) * | 1963-10-07 | 1965-12-14 | Boeing Co | Aerodynamic inlet |
| DE1250744B (pt) * | 1964-01-14 | 1967-09-21 | ||
| US3446223A (en) * | 1966-02-04 | 1969-05-27 | Lockheed Aircraft Corp | Air intake for gas turbine engines |
| US3347496A (en) * | 1966-05-03 | 1967-10-17 | Ryan Aeronautical Co | Engine air inlet system for supersonic v/stol aircraft |
| DE1944472A1 (de) | 1969-09-02 | 1971-03-18 | Messerschmitt Boelkow Blohm | Doppelwandige Verschlussklappe fuer eine Hilfseinlaufoeffnung eines Strahltriebwerkes |
| US3664612A (en) * | 1969-12-22 | 1972-05-23 | Boeing Co | Aircraft engine variable highlight inlet |
| US3618876A (en) * | 1969-12-22 | 1971-11-09 | Boeing Co | Aircraft engine leading edge auxiliary air inlet |
| DE2511468C3 (de) * | 1975-03-15 | 1980-11-13 | Vereinigte Flugtechnische Werke- Fokker Gmbh, 2800 Bremen | Triebwerkseinlauf mit einer Hilfseinlaufklappe |
| US4132240A (en) * | 1977-03-28 | 1979-01-02 | General Electric Company | Variable double lip quiet inlet |
| IL62132A0 (en) | 1980-02-26 | 1981-03-31 | Gen Electric | Inlet cowl for a two-dimensional inlet |
| US4474344A (en) * | 1981-03-25 | 1984-10-02 | The Boeing Company | Compression-sealed nacelle inlet door assembly |
| DE3444822A1 (de) * | 1984-12-08 | 1986-06-12 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Regelbarer diffusor fuer einen lufteinlauf an einem flugzeug |
| GB2208702A (en) * | 1987-08-18 | 1989-04-12 | Rolls Royce Plc | A heat exchanger system |
| FR2763098B1 (fr) * | 1997-05-07 | 1999-06-11 | Snecma | Systeme d'admission d'air dans une veine de turbomachine |
| RU2140378C1 (ru) | 1997-12-10 | 1999-10-27 | Акционерное общество открытого типа "ОКБ Сухого" | Воздухозаборник для транспортного средства |
| US6079667A (en) * | 1998-06-09 | 2000-06-27 | Mcdonnell Douglas Corporation | Auxiliary inlet for a jet engine |
| DE10119433C1 (de) * | 2001-04-20 | 2002-08-22 | Liebherr Aerospace Gmbh | Stauluftkanal für eine Flugzeugklimaanlage |
-
2003
- 2003-12-30 DE DE2003161722 patent/DE10361722B4/de not_active Expired - Fee Related
-
2004
- 2004-12-30 US US10/582,572 patent/US7832684B2/en not_active Expired - Fee Related
- 2004-12-30 RU RU2006122218A patent/RU2376209C2/ru not_active IP Right Cessation
- 2004-12-30 CA CA 2552166 patent/CA2552166C/en not_active Expired - Fee Related
- 2004-12-30 BR BRPI0418168-9A patent/BRPI0418168A/pt not_active Application Discontinuation
- 2004-12-30 WO PCT/EP2004/014864 patent/WO2005063579A1/en active Application Filing
- 2004-12-30 JP JP2006546126A patent/JP4614972B2/ja not_active Expired - Fee Related
- 2004-12-30 EP EP04804449A patent/EP1699698B1/en not_active Not-in-force
- 2004-12-30 DE DE200460019682 patent/DE602004019682D1/de active Active
- 2004-12-30 CN CN200480039561A patent/CN100586796C/zh not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JP4614972B2 (ja) | 2011-01-19 |
| US7832684B2 (en) | 2010-11-16 |
| US20070125906A1 (en) | 2007-06-07 |
| RU2006122218A (ru) | 2008-02-10 |
| CA2552166C (en) | 2009-08-25 |
| DE10361722B4 (de) | 2009-06-10 |
| CN1902094A (zh) | 2007-01-24 |
| EP1699698A1 (en) | 2006-09-13 |
| CN100586796C (zh) | 2010-02-03 |
| RU2376209C2 (ru) | 2009-12-20 |
| EP1699698B1 (en) | 2009-02-25 |
| DE10361722A1 (de) | 2005-08-04 |
| DE602004019682D1 (de) | 2009-04-09 |
| JP2007517710A (ja) | 2007-07-05 |
| CA2552166A1 (en) | 2005-07-14 |
| WO2005063579A1 (en) | 2005-07-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B25D | Requested change of name of applicant approved |
Owner name: AIRBUS OPERATIONS GMBH (DE) Free format text: NOME ALTERADO DE: AIRBUS DEUTSCHLAND GMBH |
|
| B07A | Technical examination (opinion): publication of technical examination (opinion) | ||
| B09B | Decision: refusal | ||
| B09B | Decision: refusal |