DE60205025D1 - Vorrichtung und verfahren zur kontrolle der dynamischen steifigkeit von hydraulischen servoaktuatoren - Google Patents

Vorrichtung und verfahren zur kontrolle der dynamischen steifigkeit von hydraulischen servoaktuatoren

Info

Publication number
DE60205025D1
DE60205025D1 DE60205025T DE60205025T DE60205025D1 DE 60205025 D1 DE60205025 D1 DE 60205025D1 DE 60205025 T DE60205025 T DE 60205025T DE 60205025 T DE60205025 T DE 60205025T DE 60205025 D1 DE60205025 D1 DE 60205025D1
Authority
DE
Germany
Prior art keywords
actuator
dynamic stiffness
pressure differential
control surface
servoactuators
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
DE60205025T
Other languages
English (en)
Inventor
B Hickman
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.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
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 Honeywell International Inc filed Critical Honeywell International Inc
Application granted granted Critical
Publication of DE60205025D1 publication Critical patent/DE60205025D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/40—Transmitting means with power amplification using fluid pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60—Testing or inspecting aircraft components or systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B19/00—Testing; Calibrating; Fault detection or monitoring; Simulation or modelling of fluid-pressure systems or apparatus not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Feedback Control In General (AREA)
  • Servomotors (AREA)
  • Control Of Position Or Direction (AREA)
DE60205025T 2001-05-29 2002-05-23 Vorrichtung und verfahren zur kontrolle der dynamischen steifigkeit von hydraulischen servoaktuatoren Expired - Lifetime DE60205025D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/867,152 US6578425B2 (en) 2001-05-29 2001-05-29 Apparatus and method for verifying the dynamic stiffness capability of hydraulic servo actuators
PCT/US2002/016617 WO2002096751A1 (en) 2001-05-29 2002-05-23 Apparatus and method for verifying the dynamic stiffness capability of hydraulic servo actuators

Publications (1)

Publication Number Publication Date
DE60205025D1 true DE60205025D1 (de) 2005-08-18

Family

ID=25349223

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60205025T Expired - Lifetime DE60205025D1 (de) 2001-05-29 2002-05-23 Vorrichtung und verfahren zur kontrolle der dynamischen steifigkeit von hydraulischen servoaktuatoren

Country Status (5)

Country Link
US (1) US6578425B2 (de)
EP (1) EP1392561B1 (de)
AT (1) ATE299461T1 (de)
DE (1) DE60205025D1 (de)
WO (1) WO2002096751A1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2953494B1 (fr) * 2009-12-08 2012-02-17 Goodrich Actuation Systems Sas Dispositif de test de la detection de la reprise effort par une voie secondaire d'un actionneur de commande de vol, et procede de test associe
US8374804B2 (en) * 2010-02-12 2013-02-12 Honeywell International Inc. Aircraft dynamic pressure estimation system and method
JP5498887B2 (ja) * 2010-07-27 2014-05-21 ナブテスコ株式会社 ダンピング試験方法、制御装置、油圧システム及びプログラム
CN101979883B (zh) * 2010-10-21 2013-01-16 武汉科技大学 大型伺服液压缸带载活塞偏摆测试系统及其测试方法
US8770037B2 (en) 2011-10-14 2014-07-08 Chrysler Group Llc System and method for structure stiffness determination
US20130118246A1 (en) * 2011-11-14 2013-05-16 Tareq Nasser Al-Buaijan Shut-off valve testing system
US20130133405A1 (en) * 2011-11-25 2013-05-30 Tareq Nasser Al-Buaijan Shut-off valve testing system
US20140033909A1 (en) * 2012-08-03 2014-02-06 Robert M. Murphy Methods and apparatus to control movement of a component
CN103104573B (zh) * 2013-03-11 2015-03-25 武汉科技大学 大型液压缸高频带载频率特性测试装置及其测试方法
CA2919342C (en) 2015-04-15 2023-08-15 Goodrich Actuation Systems Sas Check device for flight actuator primary load path failure detection device
CN105119579B (zh) * 2015-09-09 2018-06-22 浙江大学 伺服阀放大器
US10196131B2 (en) * 2016-02-16 2019-02-05 The Boeing Company Hydraulic system and method for an aircraft flight control system
CN107131178B (zh) * 2016-02-29 2019-01-11 宝山钢铁股份有限公司 一种可变刚度的伺服油缸性能测试方法及其测试系统
CN107542726B (zh) * 2016-06-29 2019-06-25 宝山钢铁股份有限公司 模拟实际工况的伺服油缸性能试验设备
JP6868166B2 (ja) * 2016-10-03 2021-05-12 Smc株式会社 シリンダの動作状態監視装置
GB2557273A (en) * 2016-12-02 2018-06-20 Airbus Operations Ltd Actuator testing
US10723441B2 (en) 2018-04-13 2020-07-28 The Boeing Company High-speed-deployed, drum-brake, inertia disk for rack and pinion rotational inerter
US10947997B2 (en) * 2018-04-13 2021-03-16 The Boeing Company Aircraft hydraulic system with a dual spool valve and methods of use
US10711809B2 (en) * 2018-04-13 2020-07-14 The Boeing Company Aircraft hydraulic system with a dual spool valve and methods of use
US11072418B2 (en) 2018-04-13 2021-07-27 The Boeing Company Hydraulic system for an aircraft
US10793261B2 (en) 2018-04-13 2020-10-06 The Boeing Company Electro-mechanically biased supercritical flight control surface loading to reduce high pressure actuation cycles
US10737764B2 (en) 2018-04-13 2020-08-11 The Boeing Company Base flight control member orientation mechanism and control
US10526071B2 (en) * 2018-04-13 2020-01-07 The Boeing Company Hydraulic systems and methods to control a member
CN110217407B (zh) * 2019-05-17 2022-11-01 陕西飞机工业（集团）有限公司 一种液压作动筒的试验装置
CN110411719B (zh) * 2019-07-05 2021-04-30 上海理工大学 磨床尾架动刚度测量装置及评价方法
CN110375938B (zh) * 2019-07-05 2021-04-30 上海理工大学 外圆磨床头架动刚度测量装置及方法
US11142301B2 (en) * 2019-08-27 2021-10-12 The Boeing Company Methods and apparatus for mitigating aerodynamic flutter of aircraft wing flaps
US20210341327A1 (en) * 2020-04-30 2021-11-04 Fisher Controls International Llc Methods and apparatus for quantifying pneumatic volume usage via valve controllers

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3945593A (en) * 1972-10-10 1976-03-23 Bodenseewerk Geratetechnik Gmbh Flight control apparatus
US4106730A (en) * 1976-10-01 1978-08-15 The Boeing Company Engine out control system for STOL aircraft
US4382281A (en) * 1980-08-08 1983-05-03 United Technologies Corporation Helicopter force feel actuator automatic static null compensation
US4496121A (en) 1982-09-21 1985-01-29 The Boeing Company Control surface lock for flutter constraint
US4510428A (en) 1983-03-25 1985-04-09 Unimation, Inc. Control system for manipulator apparatus with initializing stabilization and inertia scaling
US4598890A (en) 1983-08-01 1986-07-08 The Boeing Company Avionic control system
US4555974A (en) 1983-09-02 1985-12-03 Pneumo Corporation Servo actuator control/damping mechanism and method
JP2879946B2 (ja) 1990-06-04 1999-04-05 帝人製機株式会社 航空機翼のフラッタ抑制システム
JPH07112836B2 (ja) * 1991-06-14 1995-12-06 富士重工業株式会社 航空機の油圧操舵装置
FR2686310B1 (fr) 1992-01-20 1994-04-08 Aerospatiale Ste Nationale Indle Systeme pour la commande d'une surface aerodynamique d'un aeronef.
US5634389A (en) 1993-11-29 1997-06-03 Northrop Grumman Corporation Actuator stiffness enhancing system
US5881971A (en) * 1995-05-15 1999-03-16 The Boeing Company Monitoring systems for detecting failures in fly-by-wire aircraft flight control systems
US5616861A (en) * 1995-06-07 1997-04-01 Rosemount Aerospace Inc. Three pressure pseudo -Δ-P sensor for use with three pressure air data probe
US6439512B1 (en) * 2000-08-24 2002-08-27 Hr Textron, Inc. All-hydraulic powered horizontal stabilizer trim control surface position control system

Also Published As

Publication number Publication date
US6578425B2 (en) 2003-06-17
EP1392561A1 (de) 2004-03-03
EP1392561B1 (de) 2005-07-13
ATE299461T1 (de) 2005-07-15
US20020178825A1 (en) 2002-12-05
WO2002096751A1 (en) 2002-12-05

Similar Documents

Publication Publication Date Title
DE60205025D1 (de) Vorrichtung und verfahren zur kontrolle der dynamischen steifigkeit von hydraulischen servoaktuatoren
WO2002025214A3 (en) Graphical system and method for defining pilot tasks, patterns and constraints
DE60201782D1 (de) Verfahren und Einrichtung zur Steuerung mindestens einer Trimmungsklappe eines Flugzeugs während des Starts
SE8406304D0 (sv) Method and circuit configuration for supressing unwelcome control actions in slip-controlled brake systems
EP2189330A3 (de) Aktive Aufhängung
EP1288055A3 (de) Adaptive Geschwindigkeitsregelvorrichtung- und system
EP1013527A3 (de) Ein System und ein Verfahren zur Kraftfahrzeugdynamiksteuerung
EP0950591A3 (de) Verfahren für die Überwachung von Bremsen
EP0379329A3 (de) Mit Fluidum-Druck betätigte Verstärker für Fahrzeugbrems-Systeme
DE602007006956D1 (de) Verfahren und vorrichtung zur steuerung einer semiaktiven aufhängung
EP1764284A3 (de) Verfahren und Vorrichtung zur verbesserten aktiven Dämpfung von Lenksystemen
WO2003023322A3 (en) Airplane emergency navigational system
EP1288107A3 (de) Methode zum automatischen Anpassen von Referenz-Modellen in Fahrzeug-Stabilitätsverbesserungs-Systemen
WO2004047502A3 (en) Computerized automated dynamic control system for single-track vehicles
EP1386805A3 (de) Verfahren zur dynamischen Bestimmung von auf dem Boden aufstehenden und abhebenden Rädern und deren Anwendung in Wankstabilitätsregelungen
SE0101855D0 (sv) Verfahren und vorrichtung zur sicherstellung der bremswirkung von in einem fahrzeug angeordneten bremsaktuatoren
ATE349729T1 (de) Verfahren und vorrichtung zur steuerung eines flugzeuges
EP1197820A3 (de) Steuerungsverfahren zur Beschleunigung und zur Verzögerung
WO2003016114A3 (de) Verfahren zur entgasung einer hydraulischen fahrzeugbremsanlage
EP0952060A3 (de) Verfahren und Vorrichtung zum Einstellen bzw. Ändern des Lüftspiels zwischen Bremsbelägen und Reibflächen von Fahrzeugbremsen
NO20060566L (no) Bremseanordning for et skinnekjoretoy
EP1315053A3 (de) Verfahren und Vorrichtung zur Steuerung eines Prozesses
MX2021001243A (es) Dispositivo de dialogo por voz, sistema de dialogo por voz, y metodo de control para sistema de dialogo por voz.
US11755056B2 (en) Force compensation method and device
WO2003072376A3 (en) Vehicle dynamics control system

Legal Events

Date Code Title Description
8332 No legal effect for de