JPS5984696A - 作動操縦翼面により航空機翼面の震動を減衰させる方法及び装置 - Google Patents
作動操縦翼面により航空機翼面の震動を減衰させる方法及び装置Info
- Publication number
- JPS5984696A JPS5984696A JP58146269A JP14626983A JPS5984696A JP S5984696 A JPS5984696 A JP S5984696A JP 58146269 A JP58146269 A JP 58146269A JP 14626983 A JP14626983 A JP 14626983A JP S5984696 A JPS5984696 A JP S5984696A
- Authority
- JP
- Japan
- Prior art keywords
- wing
- control
- signal
- aircraft
- amplitude
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000013016 damping Methods 0.000 title claims description 10
- 238000000034 method Methods 0.000 title claims description 9
- 230000010355 oscillation Effects 0.000 claims description 14
- 230000033001 locomotion Effects 0.000 claims description 12
- 238000012545 processing Methods 0.000 claims description 9
- 230000001133 acceleration Effects 0.000 claims description 2
- 238000005259 measurement Methods 0.000 claims description 2
- 230000003068 static effect Effects 0.000 claims description 2
- 230000001007 puffing effect Effects 0.000 description 17
- 238000000926 separation method Methods 0.000 description 11
- 238000012360 testing method Methods 0.000 description 6
- 238000005452 bending Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 230000003595 spectral effect Effects 0.000 description 3
- 238000013459 approach Methods 0.000 description 2
- 230000002238 attenuated effect Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 230000005284 excitation Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 239000003381 stabilizer Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 241000985610 Forpus Species 0.000 description 1
- 241000257303 Hymenoptera Species 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001808 coupling effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
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- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000003534 oscillatory effect Effects 0.000 description 1
- 238000001615 p wave Methods 0.000 description 1
- 230000000541 pulsatile effect Effects 0.000 description 1
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- 238000001228 spectrum Methods 0.000 description 1
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- 238000013519 translation Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
-
- 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
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Vibration Prevention Devices (AREA)
- Fluid-Pressure Circuits (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8213998A FR2531676A1 (fr) | 1982-08-11 | 1982-08-11 | Procede et installation de reduction du tremblement de la voilure d'un aeronef au moyen de gouvernes actives |
| FR8213998 | 1982-08-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5984696A true JPS5984696A (ja) | 1984-05-16 |
Family
ID=9276808
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58146269A Pending JPS5984696A (ja) | 1982-08-11 | 1983-08-10 | 作動操縦翼面により航空機翼面の震動を減衰させる方法及び装置 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4706902A (cg-RX-API-DMAC7.html) |
| EP (1) | EP0101384B1 (cg-RX-API-DMAC7.html) |
| JP (1) | JPS5984696A (cg-RX-API-DMAC7.html) |
| DE (1) | DE3382509D1 (cg-RX-API-DMAC7.html) |
| FR (1) | FR2531676A1 (cg-RX-API-DMAC7.html) |
| SU (1) | SU1512494A3 (cg-RX-API-DMAC7.html) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108885466A (zh) * | 2017-11-22 | 2018-11-23 | 深圳市大疆创新科技有限公司 | 一种控制参数配置方法及无人机 |
Families Citing this family (64)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3310510A1 (de) * | 1983-03-23 | 1984-09-27 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Flatterbremse bei flugzeugen |
| GB8314656D0 (en) * | 1983-05-26 | 1983-06-29 | Secr Defence | Aircraft control |
| DE3803015A1 (de) * | 1988-02-02 | 1989-08-10 | Pfister Gmbh | Verfahren und system zum betrieb eines luftfahrzeugs |
| US5111766A (en) * | 1991-01-18 | 1992-05-12 | Ortemund Leon D | Sea wing |
| FR2672028B1 (fr) * | 1991-01-29 | 1993-05-14 | Aerospatiale | Systeme permettant d'ameliorer le comportement en flottement d'un aeronef. |
| US5150864A (en) * | 1991-09-20 | 1992-09-29 | Georgia Tech Research Corporation | Variable camber control of airfoil |
| US5319296A (en) * | 1991-11-04 | 1994-06-07 | Boeing Commercial Airplane Group | Oscillatory servo-valve monitor |
| US5374011A (en) * | 1991-11-13 | 1994-12-20 | Massachusetts Institute Of Technology | Multivariable adaptive surface control |
| US5458304A (en) * | 1992-08-26 | 1995-10-17 | Gilbert; Raymond D. | Disk spoiler system |
| JPH09504490A (ja) * | 1993-05-06 | 1997-05-06 | グラマン エアロスペース コーポレーション | 構造体の形状の制御装置および方法 |
| US5588800B1 (en) * | 1994-05-31 | 2000-12-19 | Mcdonell Douglas Helicopter Co | Blade vortex interaction noise reduction techniques for a rotorcraft |
| US5564656A (en) * | 1994-08-29 | 1996-10-15 | Gilbert; Raymond D. | Segmented spoilers |
| US5549260A (en) * | 1995-01-27 | 1996-08-27 | Dynamic Engineering, Inc. | Active control device for aircraft tail buffet alleviation |
| EP0732513B1 (de) * | 1995-03-14 | 2003-02-05 | Sulzer Markets and Technology AG | Verfahren zum aktiven Dämpfen globaler Strömungsoszillationen in abgelösten instabilen Strömungen und Vorrichtung zur Anwendung des Verfahrens |
| US5669582A (en) * | 1995-05-12 | 1997-09-23 | The Boeing Company | Method and apparatus for reducing unwanted sideways motion in the aft cabin and roll-yaw upsets of an airplane due to atmospheric turbulence and wind gusts |
| US5791875A (en) * | 1996-09-10 | 1998-08-11 | Mcdonnell Douglas Helicopter Co. | Tip vortex reduction system |
| US5813625A (en) * | 1996-10-09 | 1998-09-29 | Mcdonnell Douglas Helicopter Company | Active blowing system for rotorcraft vortex interaction noise reduction |
| US5938404A (en) * | 1997-06-05 | 1999-08-17 | Mcdonnell Douglas Helicopter Company | Oscillating air jets on aerodynamic surfaces |
| US6092990A (en) * | 1997-06-05 | 2000-07-25 | Mcdonnell Douglas Helicopter Company | Oscillating air jets for helicopter rotor aerodynamic control and BVI noise reduction |
| US6234751B1 (en) | 1997-06-05 | 2001-05-22 | Mcdonnell Douglas Helicopter Co. | Oscillating air jets for reducing HSI noise |
| US6543719B1 (en) | 1997-06-05 | 2003-04-08 | Mcdonnell Douglas Helicopter Co. | Oscillating air jets for implementing blade variable twist, enhancing engine and blade efficiency, and reducing drag, vibration, download and ir signature |
| DE19835191C1 (de) * | 1998-08-04 | 2000-04-20 | Daimler Chrysler Ag | Flugsteuerungseinrichtung zur Verbesserung der Längsstabilität eines geregelten Flugzeugs |
| DE19841632C2 (de) | 1998-09-11 | 2001-06-07 | Daimler Chrysler Ag | Verfahren zum Kompensieren von Strukturschwingungen eines Flugzeugs aufgrund von äußeren Störungen |
| FR2792285B1 (fr) | 1999-04-16 | 2001-06-08 | Onera (Off Nat Aerospatiale) | Surface aerodynamique d'aeronef a deflecteur de bord de fuite |
| DE19923087B4 (de) * | 1999-05-20 | 2004-02-26 | Eads Deutschland Gmbh | Vorrichtung zur Druck-, Schall- und Vibrationsmessung, sowie Verfahren zur Strömungsanalyse an Bauteiloberflächen |
| US6375127B1 (en) | 2000-07-07 | 2002-04-23 | Kari Appa | Active control surface modal system for aircraft buffet and gust load alleviation and flutter suppression |
| US6478541B1 (en) | 2001-08-16 | 2002-11-12 | The Boeing Company | Tapered/segmented flaps for rotor blade-vortex interaction (BVI) noise and vibration reduction |
| US6698684B1 (en) | 2002-01-30 | 2004-03-02 | Gulfstream Aerospace Corporation | Supersonic aircraft with spike for controlling and reducing sonic boom |
| CA2474552C (en) | 2002-01-30 | 2011-07-26 | Gulfstream Aerospace Corporation | Fuselage shaping and inclusion of spike on a supersonic aircraft for controlling and reducing sonic boom |
| FR2838101B1 (fr) * | 2002-04-08 | 2004-12-17 | Airbus France | Aeronef a commandes de vol electriques, pourvu d'un fuselage susceptible de se deformer et de vibrer |
| US6915989B2 (en) * | 2002-05-01 | 2005-07-12 | The Boeing Company | Aircraft multi-axis modal suppression system |
| FR2841211B1 (fr) * | 2002-06-21 | 2004-12-17 | Airbus France | Procede et dispositif pour reduire les mouvements vibratoires du fuselage d'un aeronef |
| US6659397B1 (en) * | 2002-10-18 | 2003-12-09 | Richard Charron | Control system for ornithopter |
| US6766981B2 (en) * | 2002-10-25 | 2004-07-27 | Northrop Grumman Corporation | Control system for alleviating a gust load on an aircraft wing |
| US6685143B1 (en) * | 2003-01-03 | 2004-02-03 | Orbital Research Inc. | Aircraft and missile forebody flow control device and method of controlling flow |
| FR2852577B1 (fr) | 2003-03-19 | 2006-01-06 | Centre Nat Rech Scient | Dispositif de controle d'ecoulement d'air autour d'un profile aerodynamique pour aeronef, du type aile d'avion |
| FR2853094B1 (fr) * | 2003-03-26 | 2005-05-27 | Airbus France | Procede pour contrer les vibrations induites dans un aeronef par le fonctionnement en moulinet d'une soufflante et systeme de commandes de vol electriques mettant en oeuvre ce procede |
| EP2146263B1 (en) | 2003-11-03 | 2019-05-08 | The Boeing Company | Aircraft multi-axis modal suppression system |
| US7510149B2 (en) * | 2004-08-02 | 2009-03-31 | Lockheed Martin Corporation | System and method to control flowfield vortices with micro-jet arrays |
| US7367530B2 (en) | 2005-06-21 | 2008-05-06 | The Boeing Company | Aerospace vehicle yaw generating systems and associated methods |
| FR2888210B1 (fr) * | 2005-07-08 | 2007-08-17 | Airbus France Sas | Procede et dispositif pour alleger les charges sur la voilure d'un aeronef en roulis |
| US20070114327A1 (en) * | 2005-11-18 | 2007-05-24 | The Boeing Company | Wing load alleviation apparatus and method |
| CA2634012C (en) | 2005-12-15 | 2018-05-01 | Gulfstream Aerospace Corporation | Isentropic compression inlet for supersonic aircraft |
| US8209071B2 (en) * | 2007-04-16 | 2012-06-26 | Raytheon Company | Methods and apparatus for aircraft turbulence detection |
| US8393158B2 (en) | 2007-10-24 | 2013-03-12 | Gulfstream Aerospace Corporation | Low shock strength inlet |
| US8090485B2 (en) * | 2007-11-27 | 2012-01-03 | Embraer S.A. | Low-frequency flight control system oscillatory faults prevention via horizontal and vertical tail load monitors |
| FR2929241B1 (fr) | 2008-03-31 | 2010-06-04 | Airbus France | Procede et dispositif de reduction du tremblement d'un avion. |
| US9302766B2 (en) * | 2008-06-20 | 2016-04-05 | Aviation Partners, Inc. | Split blended winglet |
| EP3663193B1 (en) | 2008-06-20 | 2025-08-06 | Aviation Partners, Inc. | Curved wing tip |
| FR2946430B1 (fr) * | 2009-06-03 | 2011-08-26 | Airbus France | Procede et dispositif pour determiner des charges critiques dues a un tremblement sur une structure d'un avion. |
| DE102010028311A1 (de) | 2010-04-28 | 2011-11-03 | Airbus Operations Gmbh | System und Verfahren zur Minimierung von Buffeting |
| CN107054628B (zh) * | 2011-06-09 | 2019-04-16 | 航空伙伴股份有限公司 | 分裂融合式小翼 |
| EP3176074B1 (en) | 2015-12-03 | 2019-11-27 | Airbus Operations GmbH | System and method for detecting mechanical failure in the high lift system of an aircraft |
| CN110099847B (zh) * | 2016-06-30 | 2023-06-30 | 庞巴迪公司 | 分裂式副翼控制 |
| EP3269635A1 (en) * | 2016-07-12 | 2018-01-17 | The Aircraft Performance Company UG | Airplane wing |
| GB2569175A (en) * | 2017-12-08 | 2019-06-12 | Airbus Operations Ltd | Aircraft with active support |
| ES2905192T3 (es) * | 2018-01-15 | 2022-04-07 | The Aircraft Performance Company Gmbh | Ala de avión |
| CN114228980B (zh) * | 2021-12-06 | 2023-06-06 | 南京工业大学 | 一种基于颤振小翼的非定常流动控制方法 |
| GB2615311A (en) * | 2022-01-31 | 2023-08-09 | Airbus Operations Ltd | Aircraft wing with movable wing tip device |
| GB2616252A (en) * | 2022-01-31 | 2023-09-06 | Airbus Operations Ltd | Aircraft with movable wing tip device |
| FR3134796A1 (fr) * | 2022-04-20 | 2023-10-27 | Institut National Polytechnique De Toulouse | Optimisation de la portance d’une aile limitant l’augmentation de la trainée |
| GB2628523B (en) * | 2022-11-16 | 2025-07-09 | Airbus Operations Ltd | Aircraft wing |
| CN119442492B (zh) * | 2025-01-13 | 2025-04-18 | 西北工业大学 | 一种针对宽频激波抖振的联合控制机翼设计方法 |
| CN120909322B (zh) * | 2025-10-10 | 2025-12-05 | 天津天境飞航科技有限公司 | 一种复合翼无人机过渡模态控制方法和系统 |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2745613A (en) * | 1951-12-10 | 1956-05-15 | Douglas Aircraft Co Inc | Gust load alleviating device |
| US3020006A (en) * | 1954-12-06 | 1962-02-06 | James R Warren | Vibration damping mechanism |
| US3184188A (en) * | 1961-06-19 | 1965-05-18 | Bendix Corp | Stress sensor and control system for limiting stresses applied to aircraft |
| US3240447A (en) * | 1962-01-10 | 1966-03-15 | North American Aviation Inc | Vehicle control system |
| US3279725A (en) * | 1963-12-11 | 1966-10-18 | North American Aviation Inc | Flight controller for flexible vehicles |
| US3236478A (en) * | 1964-04-23 | 1966-02-22 | North American Aviation Inc | Flight control system |
| GB1086938A (en) * | 1964-09-16 | 1967-10-11 | Elliott Brothers London Ltd | Aircraft structural fatigue alleviators |
| US3734432A (en) * | 1971-03-25 | 1973-05-22 | G Low | Suppression of flutter |
| US3902686A (en) * | 1973-10-17 | 1975-09-02 | Us Air Force | Combined vertical and lateral identical location of accelerometer and force system |
| EP0046875B1 (de) * | 1980-09-02 | 1989-09-20 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Anordnung, insbesondere für Luftfahrzeuge zur Übertragung von Steuersignalen |
-
1982
- 1982-08-11 FR FR8213998A patent/FR2531676A1/fr active Granted
-
1983
- 1983-08-10 EP EP83401646A patent/EP0101384B1/fr not_active Expired - Lifetime
- 1983-08-10 DE DE8383401646T patent/DE3382509D1/de not_active Expired - Lifetime
- 1983-08-10 SU SU833633575A patent/SU1512494A3/ru active
- 1983-08-10 JP JP58146269A patent/JPS5984696A/ja active Pending
-
1985
- 1985-05-06 US US06/731,161 patent/US4706902A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108885466A (zh) * | 2017-11-22 | 2018-11-23 | 深圳市大疆创新科技有限公司 | 一种控制参数配置方法及无人机 |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2531676B1 (cg-RX-API-DMAC7.html) | 1985-02-01 |
| EP0101384A1 (fr) | 1984-02-22 |
| FR2531676A1 (fr) | 1984-02-17 |
| US4706902A (en) | 1987-11-17 |
| SU1512494A3 (ru) | 1989-09-30 |
| EP0101384B1 (fr) | 1992-02-12 |
| DE3382509D1 (de) | 1992-03-26 |
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