ES2083120T3 - Simulador de vibraciones de mastil de helicoptero. - Google Patents
Simulador de vibraciones de mastil de helicoptero.Info
- Publication number
- ES2083120T3 ES2083120T3 ES92401742T ES92401742T ES2083120T3 ES 2083120 T3 ES2083120 T3 ES 2083120T3 ES 92401742 T ES92401742 T ES 92401742T ES 92401742 T ES92401742 T ES 92401742T ES 2083120 T3 ES2083120 T3 ES 2083120T3
- Authority
- ES
- Spain
- Prior art keywords
- shaft
- exciters
- helicopter
- vibration simulator
- rotor
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M7/00—Vibration-testing of structures; Shock-testing of structures
- G01M7/02—Vibration-testing by means of a shake table
- G01M7/06—Multidirectional test stands
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Apparatuses For Generation Of Mechanical Vibrations (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Vibration Prevention Devices (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
- Catching Or Destruction (AREA)
- Nonwoven Fabrics (AREA)
- Medicines Containing Plant Substances (AREA)
Abstract
CON EL FIN DE EFECTUAR EL CONTROL FUNCIONAL DE APARATOS TALES COMO VISORES (A) PREVISTOS PARA SER MONTADOS EN LA PARTE SUPERIOR DEL MASTIL QUE SOPORTA EL ROTOR DE UN HELICOPTERO, SE PROPONE UN SIMULADOR DE VIBRACIONES CONTROLADO POR TRES EXCITADORES LINEALES (14) DE EJES PARALELOS. LOS EXCITADORES (14) ACTUAN SOBRE UNA PLACA DE INTERFASE (32) QUE LLEVA UN MASTIL (50) EQUIPADO CON EL VISOR (A) A PROBAR, EN TRES PUNTOS QUE FORMAN UN TRIANGULO EQUILATERO CENTRADO SOBRE EL EJE DEL MASTIL. LOS MOVIMIENTOS DE LA PLACA (32) ESTAN LIMITADOS A UNA TRANSLACION SEGUN UN EJE VERTICAL Y A DOS ROTACIONES ALREDEDOR DE DOS EJES HORIZONTALES ORTOGONALES POR UN MECANISMO APROPIADO (30,26, 28,42, 44, 46). UN CALCULADOR NUMERICO, SENSIBLE A SEÑALES EMITIDAS POR ACELEROMETROS ASOCIADOS A CADA UNO DE LOS EXCITADORES, CONTROLA ESTOS ULTIMOS DE MANERA A RECONSTITUIR LAS VIBRACIONES ELEMENTALES DE UN MASTIL DE HELICOPTERO.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9107721A FR2678067B1 (fr) | 1991-06-24 | 1991-06-24 | Simulateur de vibrations de mat d'helicoptere. |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2083120T3 true ES2083120T3 (es) | 1996-04-01 |
Family
ID=9414187
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES92401742T Expired - Lifetime ES2083120T3 (es) | 1991-06-24 | 1992-06-22 | Simulador de vibraciones de mastil de helicoptero. |
Country Status (9)
Country | Link |
---|---|
US (1) | US5309766A (es) |
EP (1) | EP0520872B1 (es) |
JP (1) | JPH06341918A (es) |
AT (1) | ATE132259T1 (es) |
CA (1) | CA2071570A1 (es) |
DE (1) | DE69207083T2 (es) |
ES (1) | ES2083120T3 (es) |
FR (1) | FR2678067B1 (es) |
GR (1) | GR3019259T3 (es) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2731795B1 (fr) * | 1995-03-16 | 1997-06-06 | Eurocopter France | Banc d'essai pour rotors de giravions |
US5948987A (en) * | 1996-06-20 | 1999-09-07 | Liu; Hong S. | Rotational shock fixture |
US5644087A (en) * | 1996-06-20 | 1997-07-01 | Liu; Hong S. | Rotational shock vibration fixture |
WO1998056017A1 (fr) | 1997-06-03 | 1998-12-10 | Mitsubishi Denki Kabushiki Kaisha | Procede d'evaluation de la deterioration de papier isolant |
US6283757B1 (en) | 1998-10-09 | 2001-09-04 | Simulation Entertainment Group, Inc. | Full motion two seat interactive simulator |
US6257067B1 (en) * | 1999-04-28 | 2001-07-10 | Hughes Electronics Corporation | Vertical direction spacecraft vibration test system with pseudo-free boundary conditions |
US6412360B1 (en) * | 1999-09-28 | 2002-07-02 | Barry F. Hebert | Spacecraft test system |
CN102445319B (zh) * | 2011-09-26 | 2014-02-12 | 江苏大学 | 实现空间三平移高频激振的并联工作台 |
CN102865985B (zh) * | 2012-09-03 | 2015-12-09 | 江苏大学 | 一种基于柔性关节的空间三平移并联激振振动装置 |
CN105424335B (zh) * | 2015-11-04 | 2018-06-05 | 中国直升机设计研究所 | 一种旋翼操纵装置 |
CN105699036B (zh) * | 2016-03-04 | 2018-07-20 | 中国工程物理研究院总体工程研究所 | 一种双振动台并推振动试验用扩展台 |
CN105841905B (zh) * | 2016-05-23 | 2018-07-06 | 中国工程物理研究院总体工程研究所 | 一种可自动调心的直线运动补偿装置 |
CN106596023B (zh) * | 2016-11-29 | 2019-01-22 | 中国直升机设计研究所 | 一种直升机真实振动环境模拟试验系统 |
CN106596014B (zh) * | 2016-11-29 | 2019-02-26 | 中国直升机设计研究所 | 一种直升机舱内飞行振动环境模拟试验方法 |
CN110566473B (zh) * | 2019-09-06 | 2021-01-05 | 中广核工程有限公司 | 非能动核电厂主泵振动监测系统 |
CN110920933B (zh) * | 2019-12-04 | 2022-07-01 | 中国直升机设计研究所 | 一种直升机操纵杆调频设计方法 |
CN112484948A (zh) * | 2020-11-05 | 2021-03-12 | 国家能源集团乌海能源有限责任公司 | 压电俘获试验系统 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2984072A (en) * | 1959-01-12 | 1961-05-16 | Hydraulic Engineering Inc | Hydraulic jack assembly with synchronizing and flow equalizing valve mechanism |
US3340726A (en) * | 1965-01-29 | 1967-09-12 | Raymond N Armstrong | Dynamic force measurement instrument |
US4031744A (en) * | 1975-04-25 | 1977-06-28 | Kaman Aerospace Corporation | Method and apparatus for analyzing a damped structural specimen |
US4019374A (en) * | 1975-07-24 | 1977-04-26 | Trw Inc. | Electromagnetic impulser for dynamically loading a structure |
US4387881A (en) * | 1981-07-02 | 1983-06-14 | Mcduffie Thomas F | Barge jacking apparatus |
US4545462A (en) * | 1983-06-22 | 1985-10-08 | Sul Yun T | Lift for vehicle maintenance |
US4807851A (en) * | 1988-01-11 | 1989-02-28 | United Tank Lifting Technologies, Inc. | Process for lifting tanks |
JPH065192B2 (ja) * | 1988-11-25 | 1994-01-19 | アイエムブイ株式会社 | 振動制御装置 |
-
1991
- 1991-06-24 FR FR9107721A patent/FR2678067B1/fr not_active Expired - Lifetime
-
1992
- 1992-06-17 US US07/899,990 patent/US5309766A/en not_active Expired - Fee Related
- 1992-06-18 CA CA002071570A patent/CA2071570A1/en not_active Abandoned
- 1992-06-22 ES ES92401742T patent/ES2083120T3/es not_active Expired - Lifetime
- 1992-06-22 AT AT92401742T patent/ATE132259T1/de not_active IP Right Cessation
- 1992-06-22 DE DE69207083T patent/DE69207083T2/de not_active Expired - Fee Related
- 1992-06-22 EP EP92401742A patent/EP0520872B1/fr not_active Expired - Lifetime
- 1992-06-24 JP JP4166121A patent/JPH06341918A/ja not_active Withdrawn
-
1996
- 1996-03-12 GR GR960400660T patent/GR3019259T3/el unknown
Also Published As
Publication number | Publication date |
---|---|
FR2678067A1 (fr) | 1992-12-24 |
FR2678067B1 (fr) | 1993-10-15 |
EP0520872B1 (fr) | 1995-12-27 |
DE69207083T2 (de) | 1996-07-25 |
CA2071570A1 (en) | 1992-12-25 |
EP0520872A1 (fr) | 1992-12-30 |
US5309766A (en) | 1994-05-10 |
DE69207083D1 (de) | 1996-02-08 |
JPH06341918A (ja) | 1994-12-13 |
GR3019259T3 (en) | 1996-06-30 |
ATE132259T1 (de) | 1996-01-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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