ES8200767A1 - Un metodo de medir la rigidez,el coeficiente de amortigua- cion y la inercia de un sistema - Google Patents

Un metodo de medir la rigidez,el coeficiente de amortigua- cion y la inercia de un sistema

Info

Publication number
ES8200767A1
ES8200767A1 ES498726A ES498726A ES8200767A1 ES 8200767 A1 ES8200767 A1 ES 8200767A1 ES 498726 A ES498726 A ES 498726A ES 498726 A ES498726 A ES 498726A ES 8200767 A1 ES8200767 A1 ES 8200767A1
Authority
ES
Spain
Prior art keywords
mass
acceleration
signal
measuring
rigidity
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
Application number
ES498726A
Other languages
English (en)
Other versions
ES498726A0 (es
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.)
Fokker BV
Original Assignee
Fokker BV
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 Fokker BV filed Critical Fokker BV
Publication of ES498726A0 publication Critical patent/ES498726A0/es
Publication of ES8200767A1 publication Critical patent/ES8200767A1/es
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0041Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining deflection or stress
    • G01M5/005Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining deflection or stress by means of external apparatus, e.g. test benches or portable test systems
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G01L5/22Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the force applied to control members, e.g. control members of vehicles, triggers
    • G01L5/223Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the force applied to control members, e.g. control members of vehicles, triggers to joystick controls

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Abstract

METODO PARA MEDIR LA RIGIDEZ, EL COEFICIENTE DE AMORTIGUACION Y LA INERCIA DE UN SISTEMA CONSTITUIDO POR UNA MASA (1) UNIDA A UN RESORTE (2) Y A UN AMORTIGUADOR (3), EN PARTICULAR DEL MIEMBRO ACCIONADO CON LA MANO O CON EL PIE DEL MECANISMO DE CONTROL DE UN AVION O DE UN SIMULADOR DE VUELO. COMPRENDE LAS SIGUIENTES FASES: PRIMERA, CREAR TRES SEÑALES ELECTRICAS, A SABER: UNA SEÑAL DE FUERZA QUE TENGA UN VALOR DIRECTAMENTE PROPORCIONAL A LA FUERZA EJERCIDA SOBRE LA MASA, UNA SEÑAL DE ACELERACION QUE TENCA UN VALOR DIRECTAMENTE PROPORCIONAL A LA ACELERACION DE LA MASA Y UNA SEÑAL DE VELOCIDAD QUE TENGA UN VALOR DIRECTAMENTE PROPORCIANL A LA VELOCIDAD DE LA MASA; SEGUNGA, MOVER DICHA MASA DE TAL MANERA QUE ALCANCE UNA ACELERACION Y UNA VELOCIDAD CON VALORES DISTINTOS DE CERO, Y POR ULTIMO, AJUSTAR LA AMPLITUD DE LA SEÑAL DE ACELERACION Y DE LA SEÑAL DE VELOCIDAD DE TAL MODO QUE RESTANDO ESTAS DOS SEÑALES DE LA SEÑAL DE FUERZA, SE OBTENGA SUSTANCIALMENTE LA MISMA RELACION CON RESPECTO A LA DESVIACION QUE LA QUE SE OBIENE MIDIENDO LA RIGIDEZ.
ES498726A 1980-01-23 1981-01-22 Un metodo de medir la rigidez,el coeficiente de amortigua- cion y la inercia de un sistema Expired ES8200767A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL8000442A NL8000442A (nl) 1980-01-23 1980-01-23 Werkwijze en inrichting voor het meten van de parameters van een gedempt massa/veersysteem, in het bijzonder het bedieningsorgaan van een besturingssysteem.

Publications (2)

Publication Number Publication Date
ES498726A0 ES498726A0 (es) 1981-11-01
ES8200767A1 true ES8200767A1 (es) 1981-11-01

Family

ID=19834731

Family Applications (2)

Application Number Title Priority Date Filing Date
ES498726A Expired ES8200767A1 (es) 1980-01-23 1981-01-22 Un metodo de medir la rigidez,el coeficiente de amortigua- cion y la inercia de un sistema
ES501904A Expired ES8206027A1 (es) 1980-01-23 1981-05-06 Un dispositivo para medir la rigidez,el coeficiente de amor-tiguacion y la inercia de un sistema

Family Applications After (1)

Application Number Title Priority Date Filing Date
ES501904A Expired ES8206027A1 (es) 1980-01-23 1981-05-06 Un dispositivo para medir la rigidez,el coeficiente de amor-tiguacion y la inercia de un sistema

Country Status (6)

Country Link
US (1) US4358959A (es)
EP (1) EP0033178B1 (es)
CA (1) CA1157155A (es)
DE (1) DE3171284D1 (es)
ES (2) ES8200767A1 (es)
NL (1) NL8000442A (es)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8431323D0 (en) * 1984-12-12 1985-01-23 Warin C C Investigating muscles/joints
US4947697A (en) * 1989-06-28 1990-08-14 Cae Electronics Ltd. System for measuring force versus position of a flight controller in an aircraft or flight simulator
US6062715A (en) * 1997-03-21 2000-05-16 Mcdonnell Douglas Corporation Computer implemented aircraft simulation method and apparatus
FR2871570B1 (fr) * 2004-06-10 2006-09-29 Paris Eaux Gestion Dispositif de mesure de la rigidite d'une paroi et procede correspondant
CN112284656B (zh) * 2020-09-30 2023-04-11 中国科学院精密测量科学与技术创新研究院 一种零长弹簧刚度和漂移量一体化批量检测系统及方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1251056B (es) * 1967-09-28
US3030803A (en) * 1959-01-26 1962-04-24 Lord Mfg Co Measurement of dynamic properties of elastomers and like flexible materials
US3416363A (en) * 1966-10-17 1968-12-17 Gen Motors Corp Method and apparatus for determining the dynamic qualities of elastic materials
US3836757A (en) * 1972-03-03 1974-09-17 Gln Inc Method and apparatus for the computation of dynamic properties

Also Published As

Publication number Publication date
EP0033178B1 (en) 1985-07-10
CA1157155A (en) 1983-11-15
NL8000442A (nl) 1981-08-17
US4358959A (en) 1982-11-16
DE3171284D1 (en) 1985-08-14
ES498726A0 (es) 1981-11-01
EP0033178A1 (en) 1981-08-05
ES501904A0 (es) 1982-07-01
ES8206027A1 (es) 1982-07-01

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19970519