ATE467560T1 - Flugzeug mit vermindertem lärmpegel - Google Patents
Flugzeug mit vermindertem lärmpegelInfo
- Publication number
- ATE467560T1 ATE467560T1 AT07731141T AT07731141T ATE467560T1 AT E467560 T1 ATE467560 T1 AT E467560T1 AT 07731141 T AT07731141 T AT 07731141T AT 07731141 T AT07731141 T AT 07731141T AT E467560 T1 ATE467560 T1 AT E467560T1
- Authority
- AT
- Austria
- Prior art keywords
- airplane
- noise level
- reduced noise
- aircraft
- propeller
- Prior art date
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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
- B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type within, or attached to, fuselages
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Tires In General (AREA)
- Diaphragms For Electromechanical Transducers (AREA)
- Waveguide Aerials (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
- Toys (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Transmission Devices (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0602405A FR2898583B1 (fr) | 2006-03-20 | 2006-03-20 | Aeronef a impact environnemental reduit |
| PCT/FR2007/000447 WO2007107647A1 (fr) | 2006-03-20 | 2007-03-15 | Aeronef a impact environnemental reduit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE467560T1 true ATE467560T1 (de) | 2010-05-15 |
Family
ID=37311929
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT07731141T ATE467560T1 (de) | 2006-03-20 | 2007-03-15 | Flugzeug mit vermindertem lärmpegel |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US8196860B2 (de) |
| EP (1) | EP1996464B1 (de) |
| JP (1) | JP5070276B2 (de) |
| CN (1) | CN101405185B (de) |
| AT (1) | ATE467560T1 (de) |
| BR (1) | BRPI0707010A2 (de) |
| CA (1) | CA2641015A1 (de) |
| DE (1) | DE602007006440D1 (de) |
| FR (1) | FR2898583B1 (de) |
| RU (1) | RU2388657C1 (de) |
| WO (1) | WO2007107647A1 (de) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2892705B1 (fr) * | 2005-11-03 | 2009-04-24 | Airbus France Sas | Aeronef a impact environnemental reduit. |
| DE102008024463B4 (de) * | 2008-05-21 | 2011-02-24 | Bauhaus Luftfahrt E.V. | Flugzeugantriebssystem |
| FR2938504B1 (fr) * | 2008-11-14 | 2010-12-10 | Snecma | Entree d'air d'un moteur d'avion a helices propulsives non carenees |
| ES2373812B1 (es) * | 2008-12-17 | 2012-12-18 | Airbus Operations, S.L. | Superficie estabilizadora horizontal de aeronave. |
| US8740139B1 (en) * | 2012-04-23 | 2014-06-03 | The Boeing Company | Leading edge snag for exposed propeller engine installation |
| US10112696B2 (en) | 2012-11-12 | 2018-10-30 | United Technologies Corporation | Stabilizer sacrificial surfaces |
| WO2014074143A1 (en) * | 2012-11-12 | 2014-05-15 | United Technologies Corporation | Aircraft with forward sweeping t-tail |
| EP2920068B1 (de) * | 2012-11-15 | 2017-11-29 | United Technologies Corporation | Stabilisator mit struktureller box und opferoberflächen |
| USD735633S1 (en) * | 2013-06-14 | 2015-08-04 | Airbus Sas | Aircraft |
| FR3043984B1 (fr) * | 2015-11-25 | 2017-12-22 | Snecma | Avion propulse par une turbomachine muni d'un ecran acoustique |
| ES2683159T3 (es) * | 2015-12-31 | 2018-09-25 | Airbus Operations S.L | Aeronave con motores montados en la parte trasera |
| FR3077801B1 (fr) * | 2018-02-14 | 2022-04-22 | Dassault Aviat | Portion d'aeronef a trainee d'onde reduite |
| US11597501B2 (en) * | 2018-12-31 | 2023-03-07 | Blended Wing Aircraft, Inc. | Deployable noise shield panels |
| US11286795B2 (en) | 2019-10-15 | 2022-03-29 | General Electric Company | Mount for an airfoil |
| US11506067B2 (en) | 2019-10-15 | 2022-11-22 | General Electric Company | Gas turbine engine with clutch assembly |
| US12103702B2 (en) | 2019-10-15 | 2024-10-01 | General Electric Company | Removeable fuselage shield for an aircraft |
| US11834196B2 (en) | 2019-10-15 | 2023-12-05 | General Electric Company | System and method for control for unducted engine |
| US11401824B2 (en) | 2019-10-15 | 2022-08-02 | General Electric Company | Gas turbine engine outlet guide vane assembly |
| US12410758B2 (en) | 2022-01-10 | 2025-09-09 | General Electric Company | Three-stream gas turbine engine control |
| JP7779789B2 (ja) * | 2022-03-31 | 2025-12-03 | 本田技研工業株式会社 | 航空機 |
| JP7783785B2 (ja) | 2022-06-07 | 2025-12-10 | 本田技研工業株式会社 | 航空機 |
| US12275532B2 (en) | 2022-08-15 | 2025-04-15 | General Electric Company | Gas turbine engine noise reduction |
| US12480449B2 (en) | 2022-08-22 | 2025-11-25 | General Electric Company | Propulsion system including an electric machine for starting a gas turbine engine |
| US12352181B2 (en) | 2023-01-30 | 2025-07-08 | General Electric Company | Turbine airfoils |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3145954A (en) * | 1962-03-07 | 1964-08-25 | Robert W Jenny | Vehicle for non-air, semi-air, and full-air supported travel |
| US3652035A (en) * | 1969-06-12 | 1972-03-28 | Charles G Fredericks | Channel tail aircraft |
| US3684217A (en) * | 1970-09-30 | 1972-08-15 | Aereon Corp | Aircraft |
| GB1480340A (en) * | 1973-07-30 | 1977-07-20 | Hawker Siddeley Aviation Ltd | Aircraft |
| US4447022A (en) * | 1982-05-21 | 1984-05-08 | Lion Charles E | Reduced noise monolithic wing-stabilizer aircraft |
| DE3219159A1 (de) * | 1982-05-21 | 1983-11-24 | Dornier Gmbh | Anordnung von mit propellern arbeitenden antriebsanlagen an luftfahrzeugen |
| GB2188987B (en) * | 1986-04-09 | 1990-02-14 | Rolls Royce | A turbofan gas turbine engine and mountings therefor |
| US4767083A (en) * | 1986-11-24 | 1988-08-30 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | High performance forward swept wing aircraft |
| US4976396A (en) * | 1987-11-13 | 1990-12-11 | The Boeing Company | Aircraft configuration with aft mounted engines |
| US4896160A (en) * | 1988-02-19 | 1990-01-23 | Aereon Corporation | Airborne surveillance platform |
| US6113028A (en) * | 1996-02-22 | 2000-09-05 | Lohse; James R. | Amphibious aircraft |
| RU2139812C1 (ru) * | 1998-04-21 | 1999-10-20 | Российский авиационный консорциум | Самолет с тремя двигателями |
| RU2141433C1 (ru) * | 1999-01-06 | 1999-11-20 | Куваев Владимир Яковлевич | Сверхзвуковой самолет |
| US6196498B1 (en) * | 1999-12-21 | 2001-03-06 | Lockheed Martin Corporation | Semi-buoyant vehicle with aerodynamic lift capability |
| RU2252176C1 (ru) * | 2003-11-27 | 2005-05-20 | Открытое акционерное общество "Туполев" (ОАО "Туполев") | Устройство крепления авиационного двигателя летательного аппарата |
| FR2873096B1 (fr) * | 2004-07-15 | 2007-11-23 | Airbus France Sas | Avion multimoteur |
-
2006
- 2006-03-20 FR FR0602405A patent/FR2898583B1/fr not_active Expired - Fee Related
-
2007
- 2007-03-15 AT AT07731141T patent/ATE467560T1/de not_active IP Right Cessation
- 2007-03-15 DE DE602007006440T patent/DE602007006440D1/de active Active
- 2007-03-15 CA CA002641015A patent/CA2641015A1/fr not_active Abandoned
- 2007-03-15 CN CN2007800097518A patent/CN101405185B/zh not_active Expired - Fee Related
- 2007-03-15 RU RU2008141310/11A patent/RU2388657C1/ru not_active IP Right Cessation
- 2007-03-15 JP JP2009500886A patent/JP5070276B2/ja not_active Expired - Fee Related
- 2007-03-15 EP EP07731141A patent/EP1996464B1/de not_active Not-in-force
- 2007-03-15 US US12/162,756 patent/US8196860B2/en not_active Expired - Fee Related
- 2007-03-15 WO PCT/FR2007/000447 patent/WO2007107647A1/fr not_active Ceased
- 2007-03-15 BR BRPI0707010-1A patent/BRPI0707010A2/pt not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| JP2009530173A (ja) | 2009-08-27 |
| WO2007107647A1 (fr) | 2007-09-27 |
| FR2898583B1 (fr) | 2008-04-18 |
| CN101405185B (zh) | 2011-03-23 |
| CA2641015A1 (fr) | 2007-09-27 |
| CN101405185A (zh) | 2009-04-08 |
| EP1996464B1 (de) | 2010-05-12 |
| BRPI0707010A2 (pt) | 2011-04-12 |
| FR2898583A1 (fr) | 2007-09-21 |
| EP1996464A1 (de) | 2008-12-03 |
| US20090020643A1 (en) | 2009-01-22 |
| DE602007006440D1 (de) | 2010-06-24 |
| US8196860B2 (en) | 2012-06-12 |
| RU2388657C1 (ru) | 2010-05-10 |
| JP5070276B2 (ja) | 2012-11-07 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |