ATE449237T1 - Gegendrehmomentvorrichtung für hubschrauber - Google Patents
Gegendrehmomentvorrichtung für hubschrauberInfo
- Publication number
- ATE449237T1 ATE449237T1 AT05857698T AT05857698T ATE449237T1 AT E449237 T1 ATE449237 T1 AT E449237T1 AT 05857698 T AT05857698 T AT 05857698T AT 05857698 T AT05857698 T AT 05857698T AT E449237 T1 ATE449237 T1 AT E449237T1
- Authority
- AT
- Austria
- Prior art keywords
- rotor
- stator
- hub
- counter
- duct
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/10—Anti- vibration means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8254—Shrouded tail rotors, e.g. "Fenestron" fans
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/326—Application in turbines in gas turbines to drive shrouded, low solidity propeller
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jib Cranes (AREA)
Applications Claiming Priority (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US58836704P | 2004-07-16 | 2004-07-16 | |
| US58836604P | 2004-07-16 | 2004-07-16 | |
| US58837704P | 2004-07-16 | 2004-07-16 | |
| US58837604P | 2004-07-16 | 2004-07-16 | |
| US58837504P | 2004-07-16 | 2004-07-16 | |
| PCT/US2005/025283 WO2006110156A2 (en) | 2004-07-16 | 2005-07-15 | Counter-torque device for a helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE449237T1 true ATE449237T1 (de) | 2009-12-15 |
Family
ID=37087454
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT05857698T ATE449237T1 (de) | 2004-07-16 | 2005-07-15 | Gegendrehmomentvorrichtung für hubschrauber |
Country Status (8)
| Country | Link |
|---|---|
| US (2) | US8286908B2 (de) |
| EP (1) | EP1778951B1 (de) |
| JP (1) | JP2008506582A (de) |
| KR (1) | KR20070072850A (de) |
| AT (1) | ATE449237T1 (de) |
| CA (2) | CA2810889C (de) |
| DE (1) | DE602005017793D1 (de) |
| WO (1) | WO2006110156A2 (de) |
Families Citing this family (57)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2925208B1 (fr) * | 2007-12-14 | 2016-07-01 | Eurocopter France | Structure absorbante pour l'attenuation de bruits generes notamment par un rotor et carenage comportant une telle structure |
| WO2009152420A2 (en) * | 2008-06-13 | 2009-12-17 | The Penn State Research Foundation | Dipole flow driven resonators for fan noise mitigation |
| US9046108B2 (en) * | 2009-09-02 | 2015-06-02 | Apple Inc. | Centrifugal blower with asymmetric blade spacing |
| US9039393B2 (en) * | 2009-09-02 | 2015-05-26 | Apple Inc. | Centrifugal blower with asymmetric blade spacing |
| US9046109B2 (en) * | 2009-09-02 | 2015-06-02 | Apple Inc. | Centrifugal blower with asymmetric blade spacing |
| GB2482333A (en) * | 2010-07-30 | 2012-02-01 | Ge Aviat Systems Ltd | Aircraft propeller |
| GB2482545B (en) * | 2010-08-06 | 2017-05-03 | Ge Aviat Systems Ltd | Aircraft propellers with composite blades mounted to a single propeller hub |
| US8939395B2 (en) * | 2010-09-09 | 2015-01-27 | Groen Brothers Aviation, Inc. | Tail fan apparatus and method for low speed yaw control of a rotorcraft |
| FR2969120B1 (fr) | 2010-12-15 | 2013-08-30 | Eurocopter France | Pale amelioree pour dispositif anti-couple d'helicoptere |
| US20130094942A1 (en) * | 2011-10-12 | 2013-04-18 | Raymond Angus MacKay | Non-uniform variable vanes |
| US10107191B2 (en) | 2012-02-29 | 2018-10-23 | United Technologies Corporation | Geared gas turbine engine with reduced fan noise |
| US20130219922A1 (en) * | 2012-02-29 | 2013-08-29 | Jonathan Gilson | Geared gas turbine engine with reduced fan noise |
| EP2671798B1 (de) * | 2012-06-08 | 2015-08-05 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Helikopter mit einem Querkanal |
| EP2706009B1 (de) * | 2012-09-07 | 2016-04-27 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Leitwerk eines Hubschraubers |
| EP2799334B1 (de) * | 2013-04-29 | 2016-09-07 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Rotierende Blattanordnung mit aerodynamischem äußeren Toroidspoiler für eine ummantelte rotierende Antriebsanordnung |
| FR3005301B1 (fr) | 2013-05-03 | 2015-05-29 | Eurocopter France | Rotor carene d'aeronef, et giravion |
| RU2557683C2 (ru) * | 2013-10-18 | 2015-07-27 | Эйрбас Хеликоптерс Дойчланд Гмбх | Вертолет с поперечным каналом |
| EP2883791B1 (de) | 2013-12-10 | 2016-04-06 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Hubschrauber mit Heckschutz |
| EP2913270B1 (de) * | 2014-02-28 | 2016-02-24 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Drehflügler mit mindestens einem hauptrotor und mindestens einem rotor zum drehmomentausgleich |
| KR102258289B1 (ko) * | 2014-05-22 | 2021-05-31 | 삼성전자 주식회사 | 이차원 배열 안테나를 사용하는 이동통신 시스템에서의 채널 피드백의 생성 및 전송 방법 및 장치 |
| US10422350B2 (en) * | 2015-07-02 | 2019-09-24 | Apple Inc. | Fan having a blade assembly with different chord lengths |
| CN106915436A (zh) * | 2017-03-10 | 2017-07-04 | 西安交通大学 | 一种新型涵道式螺旋桨装置及其实现方法 |
| US10648486B2 (en) | 2017-05-08 | 2020-05-12 | Microsoft Technology Licensing, Llc | Fan with impeller based on an audio spread-spectrum |
| US11433997B2 (en) | 2017-10-30 | 2022-09-06 | Textron Innovations Inc. | Rotorcraft anti-torque systems and methods therefor |
| US10940945B2 (en) * | 2017-10-30 | 2021-03-09 | Bell Helicopter Textron Inc. | Rotorcraft anti-torque system |
| US10210856B1 (en) | 2018-03-23 | 2019-02-19 | Bell Helicopter Textron Inc. | Noise control system for a ducted rotor assembly |
| US11767097B2 (en) | 2018-04-17 | 2023-09-26 | University Of Kansas | Acoustic noise suppressing ducted fan propulsor mounting arrangement and treatments |
| FR3080606B1 (fr) | 2018-04-26 | 2020-07-10 | Airbus Helicopters | Rotor d'aeronef a pale distinctes et a nuisances sonores reduites |
| DE102018116166B4 (de) | 2018-07-04 | 2023-06-07 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Mantelpropeller und Luftfahrzeug |
| US20200017207A1 (en) * | 2018-07-12 | 2020-01-16 | Sikorsky Aircraft Corporation | Rotary wing aircraft with enhanced yaw capability |
| JP2020040511A (ja) * | 2018-09-10 | 2020-03-19 | 株式会社菊池製作所 | マルチコプターおよび消音装置 |
| US10889366B2 (en) | 2018-09-21 | 2021-01-12 | Textron Innovations Inc. | Ducted thrusters |
| FR3087832B1 (fr) | 2018-10-26 | 2020-10-16 | Airbus Helicopters | Systeme carene et aeronef |
| DE102019101359B4 (de) * | 2019-01-21 | 2022-03-17 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Luftfahrzeug |
| US11117655B2 (en) | 2019-06-10 | 2021-09-14 | Bell Textron Inc. | Counter-rotating tail rotor |
| DE102020201417A1 (de) | 2020-02-05 | 2021-08-05 | kopter germany GmbH | Rotorsystem für ein Fluggerät |
| US11273910B2 (en) | 2020-06-19 | 2022-03-15 | Textron Innovations Inc. | Sacrificial blade tips for ducted aircraft |
| US11370536B2 (en) | 2020-06-19 | 2022-06-28 | Textron Innovations Inc. | Tip gap control systems with active blade tips |
| US11203421B1 (en) | 2020-06-19 | 2021-12-21 | Textron Innovations Inc. | Passive tip gap management systems for ducted aircraft |
| US11407504B2 (en) | 2020-06-19 | 2022-08-09 | Textron Innovations Inc. | Tip gap control systems with inner duct control surfaces |
| US11479350B2 (en) | 2020-06-19 | 2022-10-25 | Textron Innovations Inc. | Tip gap monitoring systems for ducted aircraft |
| US11492107B2 (en) | 2020-07-22 | 2022-11-08 | Textron Innovations Inc. | Ducted proprotor systems having adaptive duct geometries |
| US11866162B2 (en) | 2020-12-01 | 2024-01-09 | Textron Innovations Inc. | Power management systems for electrically distributed yaw control systems |
| US11479349B2 (en) | 2020-12-01 | 2022-10-25 | Textron Innovations Inc. | Tail rotor balancing systems for use on rotorcraft |
| US11772785B2 (en) | 2020-12-01 | 2023-10-03 | Textron Innovations Inc. | Tail rotor configurations for rotorcraft yaw control systems |
| US11760472B2 (en) | 2020-12-01 | 2023-09-19 | Textron Innovations Inc. | Rudders for rotorcraft yaw control systems |
| US11685524B2 (en) | 2020-12-01 | 2023-06-27 | Textron Innovations Inc. | Rotorcraft quiet modes |
| US11720123B2 (en) | 2020-12-01 | 2023-08-08 | Textron Innovations Inc. | Airframe protection systems for use on rotorcraft |
| US11827344B2 (en) * | 2020-12-09 | 2023-11-28 | Textron Innovations Inc. | Low noise ducted fan |
| US11440651B1 (en) | 2021-03-01 | 2022-09-13 | Textron Innovations Inc. | Spherical bearing centrifugal force retention link |
| US11613371B1 (en) | 2021-11-19 | 2023-03-28 | John Daniel Romo | Electric vacuum jet engine |
| US12060148B2 (en) | 2022-08-16 | 2024-08-13 | Honeywell International Inc. | Ground resonance detection and warning system and method |
| CN115817797B (zh) * | 2022-11-17 | 2025-09-09 | 中国直升机设计研究所 | 一种可变距的无轴双旋翼涵道装置 |
| FR3148216A1 (fr) | 2023-04-25 | 2024-11-01 | Airbus Helicopters | procédé et aéronef muni d’au moins un réflecteur acoustique pour un système rotor caréné |
| WO2025193300A2 (en) * | 2023-12-18 | 2025-09-18 | Archer Aviation Inc. | Aerodynamic design of propeller blades in vtol aircraft |
| US12448111B1 (en) * | 2024-04-17 | 2025-10-21 | Textron Innovations Inc. | Method and system for inverse-tapered high-speed rotors |
| USD1122843S1 (en) * | 2024-08-01 | 2026-04-21 | Zipair | Set of tail rotors for a multicopter |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3285502A (en) * | 1965-01-25 | 1966-11-15 | Brookside Corp | Balanced fan construction |
| GB2114669B (en) * | 1982-02-12 | 1985-01-16 | Rolls Royce | Gas turbine engine bearing support structure |
| US5000660A (en) * | 1989-08-11 | 1991-03-19 | Airflow Research And Manufacturing Corporation | Variable skew fan |
| US4883240A (en) * | 1985-08-09 | 1989-11-28 | General Electric Company | Aircraft propeller noise reduction |
| JP2662838B2 (ja) * | 1992-03-24 | 1997-10-15 | 川崎重工業株式会社 | 回転翼航空機の尾部回転翼 |
| US5342167A (en) * | 1992-10-09 | 1994-08-30 | Airflow Research And Manufacturing Corporation | Low noise fan |
| FR2719549B1 (fr) | 1994-05-04 | 1996-07-26 | Eurocopter France | Dispositif anti-couple à rotor caréné et modulation de phase des pales, pour hélicoptère. |
| FR2719552B1 (fr) * | 1994-05-04 | 1996-07-26 | Eurocopter France | Aube de redresseur pour dispositif anti-couple à rotor et stator redresseur carénés d'hélicoptère. |
| FR2719553B1 (fr) * | 1994-05-04 | 1996-07-26 | Eurocopter France | Dispositif anti-couple à rotor arrière et stator redresseur carénés pour hélicoptère. |
| FR2719551B1 (fr) * | 1994-05-04 | 1996-07-12 | Eurocopter France | Dispositif anti-couple à rotor et stator redresseur carénés, et à aubes redresseuses inclinées. |
| FR2719550B1 (fr) | 1994-05-04 | 1996-07-26 | Eurocopter France | Dispositif anti-couple à rotor et stator redresseur carénés, et modulation de phase des pales du rotor, pour hélicoptère. |
| US6182787B1 (en) * | 1999-01-12 | 2001-02-06 | General Electric Company | Rigid sandwich panel acoustic treatment |
| US6439838B1 (en) * | 1999-12-18 | 2002-08-27 | General Electric Company | Periodic stator airfoils |
| FR2821788B1 (fr) * | 2001-03-09 | 2004-04-02 | Eads Airbus Sa | Procede de fabrication d'un panneau a couche resistive acoustique adaptee et panneau acoustique ainsi obtenu |
-
2005
- 2005-07-15 AT AT05857698T patent/ATE449237T1/de not_active IP Right Cessation
- 2005-07-15 CA CA2810889A patent/CA2810889C/en not_active Expired - Lifetime
- 2005-07-15 EP EP05857698A patent/EP1778951B1/de not_active Expired - Lifetime
- 2005-07-15 US US11/632,421 patent/US8286908B2/en not_active Expired - Fee Related
- 2005-07-15 JP JP2007521698A patent/JP2008506582A/ja not_active Abandoned
- 2005-07-15 DE DE602005017793T patent/DE602005017793D1/de not_active Expired - Lifetime
- 2005-07-15 KR KR1020077001148A patent/KR20070072850A/ko not_active Withdrawn
- 2005-07-15 CA CA2574108A patent/CA2574108C/en not_active Expired - Lifetime
- 2005-07-15 WO PCT/US2005/025283 patent/WO2006110156A2/en not_active Ceased
-
2012
- 2012-08-07 US US13/568,262 patent/US8640984B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| CA2810889C (en) | 2016-10-18 |
| WO2006110156A2 (en) | 2006-10-19 |
| KR20070072850A (ko) | 2007-07-06 |
| WO2006110156A3 (en) | 2008-02-21 |
| EP1778951B1 (de) | 2009-11-18 |
| CA2810889A1 (en) | 2006-10-19 |
| EP1778951A4 (de) | 2008-11-19 |
| US8640984B2 (en) | 2014-02-04 |
| US20090014581A1 (en) | 2009-01-15 |
| EP1778951A2 (de) | 2007-05-02 |
| US20130032664A1 (en) | 2013-02-07 |
| JP2008506582A (ja) | 2008-03-06 |
| US8286908B2 (en) | 2012-10-16 |
| CA2574108C (en) | 2016-05-24 |
| DE602005017793D1 (de) | 2009-12-31 |
| CA2574108A1 (en) | 2006-10-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |