Physics – Optics
Scientific paper
Jul 2005
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005esasp.591..311s&link_type=abstract
In: Proceedings of the 11th European Space Mechanisms and Tribology Symposium, ESMATS 2005, 21-23 September 2005, Lucerne, Switz
Physics
Optics
Mechanisms Components
Scientific paper
Piezoelectric motors offer several outstanding characteristics that may be very interesting for new scientific instruments in space applications. Piezo motors use a combination of electro-mechanical and frictional forces for generating a progressive motion; they are well suited for positioning applications because they exhibit a large force at rest without any power supply, and they often do not require any reduction gear. They are increasingly used in optical applications. Using piezo motors in space applications may become more and more relevant because of the continuous trend towards adaptive optics in future scientific payloads. In general, piezoelectric actuators are more and more used in space. Piezoelectric motors exhibit a number of advantages compared to conventional electromagnetic (stepping) motors, e.g. superior force/mass ratio, improved direct drive capability, no power supply to maintain a position, feasibility of a fully non-magnetic motor design. In this context, two complementary concepts have been designed and evaluated in the frame of ESA funded research and development activities: a resonant concept, called Rotary Piezo Actuator (RPA), a quasi-static concept, called Rotary Piezo Motor for High Precision Pointing (RPMHPP). The developed Rotary Piezo Actuator (RPA) is based on a Ultrasonic Piezo Drive (UPD) unit that drives a friction ring on the rotor part supported by a ball bearing assembly. This new motorization principle offers excellent motion dynamics and positioning accuracy combined with a high un-powered torque at standstill, and it does not rely on any magnetic features. A rotary piezo motor compliant with the requirements of a reference space application has been designed and tested. The technology remains challenging to be mastered, since the interdisciplinary aspects of the concept include, among others, drive electronics and controller design, piezo-electricity, contact mechanics and tribology. The conceptual design has lead to a cup configuration, in which the stator is placed in the inner diameter of a duplex ball bearing assembly. Despite the mass penalty of the rotor suspension, this configuration has been preferred for an easier wear debris confinement and higher support stiffness. Development testing examined two routes for the friction material (that should exhibit a low wear rate and a high friction coefficient, which should be similar in air and in vacuum): a polymer solution, already known and tested by CEDRAT TECHNOLOGIES, and a ceramic solution. Some potential applications have been identified both in the space sector (for instance magnetometer motorisation for the SWARM mission) and in other sectors, such as motorisation of equipment for Magnetic Resonant Imaging, taking benefit from the non-magnetic design option of the RPA. The second concept (RPMHPP) aims at providing very high pointing accuracy for future instruments such as the one foreseen for telescope pointing in the LISA constellation. In this concept, the piezo actuators operate in quasi-static mode and lead to a robust design, able to withstand a large non-operational temperature range (-140 to +140°C). Although the concept could allow for a full rotation, the prototype was implemented with an elastic guiding of the shaft: the angular stroke is +/-1° and the measured angular positioning accuray is in the range of 100 nrad.
Coste Ph.
Le Letty Ronan
Seiler Rene
Six M. F.
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