Tunable Proof Mass Actuator  2 Pages
Catalog excerpts
Tunable Proof Mass Actuator Objective Passive proof mass dampers are useful for the reduction of vibrations in ﬂexible structures. A proofmass damper is basically a dissipating spring connected on one end to a free reaction mass. The reaction mass generates dynamic inertial forces due to its linear acceleration at and above resonance. On its other end, the proof mass damper is ﬁxed to the ﬂexible structure to be dampened. When the resonant frequency of the proof mass damper is tuned with the vibration mode of the ﬂexible structure, such a structural mode is broken and the associated vibration level is signiﬁcantly reduced (Fig 1). Fig. 1: Effect of a proof mass damper on the frequency response of ﬂexible structure. However effectiveness of passive proof mass dampers depends strongly on how precisely they are tuned. In many applications, the tuning frequency is not quite constant and varies with the operating conditions of the system. For example in an helicopter, the rotor frequency varies with the ﬂight conditions, which changes slightly the structural modes. Another limitation of usual proof mass dampers is in their incapability to address both very low frequency operations (<100Hz) and very large force generation (>1kN), as needed in aircraft or civil engineering applications. To address these issues, a Tunable Dynamic Force Generator (TDFG) has been developed within the MESEMA EU project. In contrast to usual proof mass dampers, the TDFG is based on a pendulum structure. In this case, governing parameters are the moving mass and a returning force. This pendulum structure allows achieving a low resonant frequency associated with large inertial forces. It also allows using an electrically adjustable returning force to obtain the desired tunability. Fig. 2: TPMA in vibration test at DIISun, Naples. Based on the concept from LPAZIP, the TDFG prototype was designed, manufactured and tested by Cedrat Technologies within the MESEMA FP6 EU project. Application tests are being performed by U.Naples (DIISUN). The TDFG (Fig.2) is based on a pendulum principle: A usual pendulum makes use of gravity to generate the returning force and to deﬁne the natural resonant frequency. In the TDFG the returning force combines a mechanically adjustable preload thanks to a spring mechanism and an electrically adjustable preload component thanks to an internal preloading actuator. As a consequence, the pendulum resonant frequency can be adjusted mechanically (by easy manual screwing operation) and electrically. Different types of preloading actuators have been tested: an ampliﬁed magnetostrictive actuator called AMA 230L and an ampliﬁed piezoelectric actuator APA 230L. The AMA & APA® use a metallic shell to amplify motions from the smart material and to prestress it (see http://www.cedrat. com/hardware/piezo_actuators/piezo_actuators.htm). Both actuators are good candidates for this application since they have the beneﬁt to be small, compact and produce high forces with low power consumption. Fig. 3: AMA preloading Performances of the Tunable Proof Mass Actuator CEDRAT www.cedrat.com The TDFG prototype provides several proofs of concept: • The resonant frequency can vary from 4 to 20Hz. • The amplitude of motion of the moving mass (6.7kg) can achieve up to 10mm. • The dynamic inertial force produced by the T
Open the catalog to page 1Tunable Proof Mass Actuator The mechanical tunability is observed over a very large frequency range versus preload (Fig.4). The electrical tunability is observed by a frequency shift of the resonance versus applied voltage (Fig.5). The required electric power for the tunability can be lower than 1W. The mechanical tunability given by the relationship between the preload and the resonant frequency has been measured with manual mechanical setting of the preload. The electrical tunability has been established experimentally with both the AMA 230L and the APA 230L. However, the AMA 230L is a...
Open the catalog to page 2All CEDRAT TECHNOLOGIES catalogs and technical brochures

Piezo and magnetic products
77 Pages

RK42F3ULC75B
2 Pages

CA45
4 Pages

LA75A
4 Pages

LA75B
4 Pages

LA75C
3 Pages

SA75A
3 Pages

SA75B
3 Pages

SA75D
3 Pages

SP75A
3 Pages

UC65
3 Pages

UC55
3 Pages

UC45
2 Pages

CSA96
3 Pages

RK42F3ULC24
2 Pages

ECSU10
2 Pages

ECS45
2 Pages

ECS75
3 Pages

ECP1000
2 Pages

ECP500
2 Pages

SMAC Product Overview
20 Pages

XY25XS
2 Pages

APA30uXS
2 Pages

PPA10M
2 Pages

FP7 SONO PROJECT
2 Pages

ASPIC PROJECT
1 Pages

viper cleansky project
2 Pages

MISAC PROJECT
2 Pages

PPSMPAB PROJECT
3 Pages

AEROPZT PROJECT
2 Pages

DYNXPERTS PROJECT
1 Pages

ELIFT3 PROJECT
1 Pages

FluMIn3 projecT
1 Pages

PM900M Proof Mass Damper
2 Pages

ETS500
2 Pages

CONTACTLESS TORQUE SENSORS
2 Pages

MCSUITE Project
3 Pages

addendum
1 Pages

Aerospace and Defense
2 Pages