BR9712021A - Aparelho e método para redução de ruìdo de turbo propulsor. - Google Patents
Aparelho e método para redução de ruìdo de turbo propulsor.Info
- Publication number
- BR9712021A BR9712021A BR9712021-9A BR9712021A BR9712021A BR 9712021 A BR9712021 A BR 9712021A BR 9712021 A BR9712021 A BR 9712021A BR 9712021 A BR9712021 A BR 9712021A
- Authority
- BR
- Brazil
- Prior art keywords
- inlet
- duct
- propeller blades
- propellant
- reducing
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 3
- 239000003380 propellant Substances 0.000 abstract 3
- 238000011010 flushing procedure Methods 0.000 abstract 1
- 238000005406 washing Methods 0.000 abstract 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
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/18—Aerodynamic features
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Abstract
"APARELHO E MéTODO PARA REDUçãO DE RUìDO DE TURBO PROPULSOR". Um aparelho e método para reduzir ruído dentro da fuselagem de uma aeronave acionada por propulsor (20). Em uma modalidade as lâminas do propulsor (38) são espaçadas e na frente de uma entrada desviada (48). A entrada (48) fornece ar para um motor de turbina a gás (58) energizando o propulsor (32), e também para um duto de lavagem (60). As lâminas do propulsor (38) e a entrada (48) são espaçadas de foram que durante as condições de cruzeiro da aeronave, a borda traseira (54) das lâminas de propulsor sejam espaçadas da entrada em mais de um quarto do comprimento de corda (55) das lâminas do propulsor (38) e menos de cerca do comprimento de corda das lâminas do propulsor. Em outra modalidade, o duto de lavagem (60) é construído para fluir uma quantidade aumentada de ar. Nessa segunda modalidade, o duto de motor (56) flui mais de cerca de 40% da quantidade total de ar que entra no duto de entrada (48) e menos de cerca de 60% desse fluxo de ar total.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US2564696P | 1996-09-10 | 1996-09-10 | |
US08/920,618 US5961067A (en) | 1996-09-10 | 1997-08-27 | Method for reducing turboprop noise |
PCT/US1997/015616 WO1998010984A1 (en) | 1996-09-10 | 1997-09-05 | Apparatus and method for reducing turboprop noise |
Publications (1)
Publication Number | Publication Date |
---|---|
BR9712021A true BR9712021A (pt) | 2000-01-18 |
Family
ID=26699999
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR9712021-9A BR9712021A (pt) | 1996-09-10 | 1997-09-05 | Aparelho e método para redução de ruìdo de turbo propulsor. |
Country Status (7)
Country | Link |
---|---|
US (1) | US5961067A (pt) |
EP (1) | EP0925222A1 (pt) |
JP (1) | JP2001509750A (pt) |
AU (1) | AU4182097A (pt) |
BR (1) | BR9712021A (pt) |
CA (1) | CA2264649A1 (pt) |
WO (1) | WO1998010984A1 (pt) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110794367A (zh) * | 2019-10-12 | 2020-02-14 | 中国直升机设计研究所 | 一种桨涡干扰声源定位方法 |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2798359B1 (fr) * | 1999-09-14 | 2001-11-09 | Eurocopter France | Perfectionnements aux aeronefs convertibles a rotors basculants |
US6671590B1 (en) | 2001-04-30 | 2003-12-30 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method and system for active noise control of tiltrotor aircraft |
DE10215551A1 (de) * | 2002-04-09 | 2003-10-23 | Rolls Royce Deutschland | Turboprop-Flugzeugtriebwerk |
US7647197B2 (en) | 2002-08-09 | 2010-01-12 | Surveylab Group Limited | Mobile instrument, viewing device, and methods of processing and storing information |
US7976279B2 (en) * | 2007-06-11 | 2011-07-12 | Hamilton Sundstrand Corporation | Blade pitch actuation mechanism |
US8240120B2 (en) * | 2007-10-25 | 2012-08-14 | United Technologies Corporation | Vibration management for gas turbine engines |
US8425191B2 (en) * | 2008-05-30 | 2013-04-23 | United Technologies Corporation | Propfan assembly |
US20100014977A1 (en) * | 2008-07-15 | 2010-01-21 | Shattuck Colman D | Variable pitch aft propeller vane system |
CA2669000A1 (en) * | 2009-06-18 | 2010-12-18 | Garold Toews | A kit for modifying a strut of an aircraft with an aerodynamic cover |
WO2014058510A2 (en) * | 2012-08-01 | 2014-04-17 | Bye Uas, Inc. | Unmanned aerial systems |
ES2744631T3 (es) * | 2012-08-01 | 2020-02-25 | Bye Uas Inc | Sistemas aéreos no tripulados |
GB201303860D0 (en) | 2013-03-05 | 2013-04-17 | Rolls Royce Plc | Engine installation |
US10259574B2 (en) * | 2015-12-18 | 2019-04-16 | Amazon Technologies, Inc. | Propeller surface area treatments for sound dampening |
US10259562B2 (en) | 2015-12-18 | 2019-04-16 | Amazon Technologies, Inc. | Propeller blade trailing edge fringes for improved sound control |
US10933988B2 (en) | 2015-12-18 | 2021-03-02 | Amazon Technologies, Inc. | Propeller blade treatments for sound control |
US10011346B2 (en) | 2015-12-18 | 2018-07-03 | Amazon Technologies, Inc. | Propeller blade indentations for improved aerodynamic performance and sound control |
US10099773B2 (en) | 2015-12-18 | 2018-10-16 | Amazon Technologies, Inc. | Propeller blade leading edge serrations for improved sound control |
US10460717B2 (en) | 2015-12-18 | 2019-10-29 | Amazon Technologies, Inc. | Carbon nanotube transducers on propeller blades for sound control |
US10260417B2 (en) | 2015-12-22 | 2019-04-16 | General Electric Company | Air intake turboprop assemblies |
US9725155B2 (en) * | 2015-12-30 | 2017-08-08 | General Electric Company | Method and system for open rotor engine fuselage protection |
US10723440B2 (en) | 2016-03-23 | 2020-07-28 | Amazon Technologies, Inc. | Aerial vehicle with different propeller blade configurations |
US10399666B2 (en) | 2016-03-23 | 2019-09-03 | Amazon Technologies, Inc. | Aerial vehicle propulsion mechanism with coaxially aligned and independently rotatable propellers |
US11305874B2 (en) | 2016-03-23 | 2022-04-19 | Amazon Technologies, Inc. | Aerial vehicle adaptable propeller blades |
US10583914B2 (en) | 2016-03-23 | 2020-03-10 | Amazon Technologies, Inc. | Telescoping propeller blades for aerial vehicles |
US10526070B2 (en) | 2016-03-23 | 2020-01-07 | Amazon Technologies, Inc. | Aerial vehicle propulsion mechanism with coaxially aligned propellers |
FR3057616B1 (fr) * | 2016-10-19 | 2019-10-18 | Safran Aircraft Engines | Turbopropulseur |
US10746047B2 (en) | 2017-10-27 | 2020-08-18 | General Electric Company | Structure for mitigating vibratory modes of counter-rotating engine rotors |
US11040767B2 (en) * | 2017-11-30 | 2021-06-22 | General Electric Company | Systems and methods for improved propeller design |
US11163302B2 (en) | 2018-09-06 | 2021-11-02 | Amazon Technologies, Inc. | Aerial vehicle propellers having variable force-torque ratios |
US11072435B2 (en) * | 2018-10-25 | 2021-07-27 | Honeywell International Inc. | Inlet flow structure for turboprop engine |
WO2021092677A1 (en) | 2019-11-14 | 2021-05-20 | Delson Aeronautics Ltd. | Ultra-wide-chord propeller |
US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2564696A (en) | 1946-12-03 | 1951-08-21 | Hydrocarbon Research Inc | Hydrocarbon synthesis |
US2738148A (en) * | 1952-09-29 | 1956-03-13 | Curtiss Wright Corp | Method of developing lift from the propeller blades of an airplane |
US4240250A (en) * | 1977-12-27 | 1980-12-23 | The Boeing Company | Noise reducing air inlet for gas turbine engines |
US4250703A (en) * | 1979-03-15 | 1981-02-17 | Avco Corporation | Swinging door particle separator and deicing system |
US4397431A (en) * | 1981-11-02 | 1983-08-09 | Avco Corporation | Fail-safe, anti-icing system for aircraft engines |
US4456458A (en) * | 1982-09-20 | 1984-06-26 | The De Havilland Aircraft Of Canada, Limited | Air intake system for engine |
US4534526A (en) * | 1982-12-27 | 1985-08-13 | United Technologies Corporation | Cabin noise suppression in propeller driven aircraft |
US4715559A (en) * | 1986-05-15 | 1987-12-29 | Fuller Christopher R | Apparatus and method for global noise reduction |
GB2203801B (en) * | 1987-04-14 | 1991-11-27 | Rolls Royce Plc | A gas turbine engine |
US5014933A (en) * | 1989-04-27 | 1991-05-14 | The Boeing Company | Translating lip aircraft cowling structure adapted for noise reduction |
US4972672A (en) * | 1989-09-28 | 1990-11-27 | Pratt & Whitney Canada, Inc. | Controlled bypass inlet duct |
US5551649A (en) * | 1989-10-20 | 1996-09-03 | Fokker Aircraft B.V. | Propeller blade position controller |
US5058617A (en) * | 1990-07-23 | 1991-10-22 | General Electric Company | Nacelle inlet for an aircraft gas turbine engine |
US5415522A (en) * | 1993-11-01 | 1995-05-16 | General Electric Company | Active noise control using noise source having adaptive resonant frequency tuning through stress variation |
US5588619A (en) * | 1994-11-21 | 1996-12-31 | Lopresti; Leroy | Propeller syncro-pulsing |
US5478199A (en) * | 1994-11-28 | 1995-12-26 | General Electric Company | Active low noise fan assembly |
US5526292A (en) | 1994-11-30 | 1996-06-11 | Lord Corporation | Broadband noise and vibration reduction |
-
1997
- 1997-08-27 US US08/920,618 patent/US5961067A/en not_active Expired - Fee Related
- 1997-09-05 CA CA002264649A patent/CA2264649A1/en not_active Abandoned
- 1997-09-05 WO PCT/US1997/015616 patent/WO1998010984A1/en not_active Application Discontinuation
- 1997-09-05 JP JP51370798A patent/JP2001509750A/ja active Pending
- 1997-09-05 AU AU41820/97A patent/AU4182097A/en not_active Abandoned
- 1997-09-05 BR BR9712021-9A patent/BR9712021A/pt not_active Application Discontinuation
- 1997-09-05 EP EP97939807A patent/EP0925222A1/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110794367A (zh) * | 2019-10-12 | 2020-02-14 | 中国直升机设计研究所 | 一种桨涡干扰声源定位方法 |
CN110794367B (zh) * | 2019-10-12 | 2022-06-21 | 中国直升机设计研究所 | 一种桨涡干扰声源定位方法 |
Also Published As
Publication number | Publication date |
---|---|
JP2001509750A (ja) | 2001-07-24 |
WO1998010984A1 (en) | 1998-03-19 |
US5961067A (en) | 1999-10-05 |
AU4182097A (en) | 1998-04-02 |
EP0925222A1 (en) | 1999-06-30 |
CA2264649A1 (en) | 1998-03-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FF | Decision: intention to grant | ||
FA11 | Dismissal: dismissal - article 38, par. 2 of industrial property law |