DE69201576T2 - System zur Verbesserung des Flatterverhaltens eines Flugzeuges. - Google Patents

System zur Verbesserung des Flatterverhaltens eines Flugzeuges.

Info

Publication number
DE69201576T2
DE69201576T2 DE69201576T DE69201576T DE69201576T2 DE 69201576 T2 DE69201576 T2 DE 69201576T2 DE 69201576 T DE69201576 T DE 69201576T DE 69201576 T DE69201576 T DE 69201576T DE 69201576 T2 DE69201576 T2 DE 69201576T2
Authority
DE
Germany
Prior art keywords
aircraft
improving
flutter behavior
flutter
behavior
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.)
Expired - Lifetime
Application number
DE69201576T
Other languages
English (en)
Other versions
DE69201576D1 (de
Inventor
Michel Lacabanne
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of DE69201576D1 publication Critical patent/DE69201576D1/de
Publication of DE69201576T2 publication Critical patent/DE69201576T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0066—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements for limitation of acceleration or stress
    • 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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models
DE69201576T 1991-01-29 1992-01-22 System zur Verbesserung des Flatterverhaltens eines Flugzeuges. Expired - Lifetime DE69201576T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9100975A FR2672028B1 (fr) 1991-01-29 1991-01-29 Systeme permettant d'ameliorer le comportement en flottement d'un aeronef.

Publications (2)

Publication Number Publication Date
DE69201576D1 DE69201576D1 (de) 1995-04-13
DE69201576T2 true DE69201576T2 (de) 1995-07-27

Family

ID=9409147

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69201576T Expired - Lifetime DE69201576T2 (de) 1991-01-29 1992-01-22 System zur Verbesserung des Flatterverhaltens eines Flugzeuges.

Country Status (4)

Country Link
US (1) US5224667A (de)
EP (1) EP0497660B1 (de)
DE (1) DE69201576T2 (de)
FR (1) FR2672028B1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004029196A1 (de) * 2004-06-16 2006-01-12 Airbus Deutschland Gmbh System und Verfahren zur Rumpfstrukturlastabminderung in Verkehrsmitteln

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5452865A (en) * 1993-06-28 1995-09-26 The Boeing Company Aircraft frequency adaptive modal suppression system
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
US5598991A (en) * 1995-05-12 1997-02-04 The Boeing Company Method and apparatus for detecting oscillatory phenomena indicative of airflow separation
GB9918289D0 (en) 1999-08-03 2000-05-24 British Aerospace Actuator system for aerospace controls and functions
KR100408831B1 (ko) * 2001-08-22 2003-12-06 한국항공우주산업 주식회사 표준 대기 플러터 속도의 직접 계산 방법
FR2835067B1 (fr) * 2002-01-21 2004-04-02 Trw Sys Aeronautiques Civil Dispositif de commande a boucle d'asservissement, notamment actionneur electro-hydraulique de commande de vol
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
KR100903773B1 (ko) 2003-01-23 2009-06-19 한국항공우주산업 주식회사 항공기 시험 분석 시스템
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
EP1528448B1 (de) * 2003-11-03 2010-01-06 The Boeing Company System zur Modenunterdrückung auf mehreren Achsen eines Flugzeugs
FR2864026B1 (fr) * 2003-12-23 2007-01-19 Eurocopter France Procede et dispositif pour reduire par une derive orientable les vibrations engendrees sur le fuselage d'un helicoptere
FR2864025B1 (fr) * 2003-12-23 2007-01-12 Eurocopter France Procede et dispositif pour reduire par un empennage orientable les vibrations engendrees sur le fuselage d'un helicoptere
DE102004029194A1 (de) * 2004-06-16 2006-01-26 Airbus Deutschland Gmbh Vorrichtung und Verfahren zur Bekämpfung mindestens einer Starrkörpereigenform und/oder einer elastischen Eigenbewegungsform eines Luftfahrzeugs
US20070083345A1 (en) * 2005-10-10 2007-04-12 The Boeing Company Method and apparatus for reducing gyro aliasing, noise, and quantization
FR2899561B1 (fr) * 2006-04-11 2008-05-16 Airbus France Sas Procede et dispostif de pilotage d'un aeronef autour d'un axe de pilotage
DE102009002435A1 (de) * 2009-04-16 2010-10-21 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug und Verfahren zum Detektieren von Fehlern in einem Hochauftriebssystem für ein Flugzeug
EP3643605B1 (de) 2018-10-25 2022-08-17 Bombardier Inc. System und verfahren zur verringerung der auswirkung einer erregung eines strukturellen flexiblen modus eines flugzeugs
CN113670138B (zh) * 2021-07-23 2023-08-18 河北汉光重工有限责任公司 一种可监测和优化颤振现象的折叠舵

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2832551A (en) * 1952-11-10 1958-04-29 Honeywell Regulator Co Automatic pilot for aircraft
US2985409A (en) * 1955-09-26 1961-05-23 North American Aviation Inc Gust alleviation system
US3279725A (en) * 1963-12-11 1966-10-18 North American Aviation Inc Flight controller for flexible vehicles
GB1086938A (en) * 1964-09-16 1967-10-11 Elliott Brothers London Ltd Aircraft structural fatigue alleviators
US3374966A (en) * 1966-07-19 1968-03-26 Nasa Usa Control system
US3412961A (en) * 1966-07-27 1968-11-26 Nasa Usa Means for suppressing or attenuating bending motion of elastic bodies
CH584937B5 (de) * 1973-07-10 1977-02-15 Suisse Horlogerie
US3902686A (en) * 1973-10-17 1975-09-02 Us Air Force Combined vertical and lateral identical location of accelerometer and force system
SE396473B (sv) * 1975-01-14 1977-09-19 Bofors Ab Anordning for dempning av tipp- och girsvengar
FR2531676A1 (fr) * 1982-08-11 1984-02-17 Onera (Off Nat Aerospatiale) Procede et installation de reduction du tremblement de la voilure d'un aeronef au moyen de gouvernes actives
US4697768A (en) * 1985-11-12 1987-10-06 Grumman Aerospace Corporation Flight control system employing complementary filter
US5072893A (en) * 1987-05-28 1991-12-17 The Boeing Company Aircraft modal suppression system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004029196A1 (de) * 2004-06-16 2006-01-12 Airbus Deutschland Gmbh System und Verfahren zur Rumpfstrukturlastabminderung in Verkehrsmitteln
DE102004029196B4 (de) * 2004-06-16 2007-11-22 Airbus Deutschland Gmbh System zur Rumpfstrukturlastabminderung in Verkehrsmitteln

Also Published As

Publication number Publication date
FR2672028B1 (fr) 1993-05-14
EP0497660B1 (de) 1995-03-08
EP0497660A1 (de) 1992-08-05
US5224667A (en) 1993-07-06
DE69201576D1 (de) 1995-04-13
FR2672028A1 (fr) 1992-07-31

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Legal Events

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8364 No opposition during term of opposition