Actuator module for actuating a load

Patent metadata

Field	Value
Publication number	US-9880194-B2
Application number	US-201515301454-A
Country	US
Kind code	B2
Filing date	Mar 31, 2015
Priority date	Apr 4, 2014
Publication date	Jan 30, 2018
Grant date	Jan 30, 2018

Abstract

The disclosure concerns an actuator module ( 10 ) for actuating a load ( 14 ). The actuator module ( 10 ) comprises a deformable frame ( 1 ) and an actuator ( 2 ) connected to the deformable frame ( 1 ). A time-varying force distribution (F) couples to an excited state (V 0 ) of an eigenmode (V) of the deformable frame ( 1 ). The force distribution (F), as well as a stiffness distribution (K) and/or mass distribution (M) of the deformable frame 1 are adapted such that static nodal points ( 11 s ) of the deformable frame 1 are coincided with mode nodal points ( 11 m ). The locations where the nodal points coincide can be used to connect the actuator module ( 10 ) to a base frame to reduce transfer of vibrations to the base frame and back which may otherwise undesirably influence the transfer function from actuator to load. The disclosure further concerns a method for designing and/or manufacturing the actuator module.

First claim

The invention claimed is:

1. An actuator system comprising an actuator module for actuating a load, the actuator module comprising
a deformable frame having a stiffness distribution and mass distribution determining a vibrational eigenmode of the deformable frame, wherein an interface formed by a surface of the deformable frame comprises a plurality of mode nodal points which are stationary during modal deformation of the deformable frame in an excited state of the eigenmode; and
an actuator connected to the deformable frame and arranged for exerting a time-varying force distribution onto the deformable frame via a connection between the deformable frame and the actuator, wherein the interface of the deformable frame comprises a plurality of static nodal points which are stationary during static deformation of the deformable frame when the time-varying force distribution exerted by the actuator is applied under quasi-static conditions;
wherein the time-varying force distribution is arranged to couple to the excited state of the eigenmode and the deformable frame comprises an actuation surface, in use, oscillating due to the combined modal and static deformations of the deformable frame for actuating the load contacting and/or connected to said actuation surface; and
wherein the force distribution, stiffness distribution, and/or mass distribution are adapted to have the static nodal points coincide with the mode nodal points within a tolerance distance of less than one percent of a size across the interface of the deformable frame.

2. The actuator system according to claim 1 , wherein the deformable frame comprises a plurality of frame connectors for connecting the actuator module to a base frame wherein the frame connectors are arranged at the interface of the deformable frame-centred on the static nodal points and/or mode nodal points.

3. The actuator system according to claim 2 , wherein each frame connector comprises a respective recess and/or protrusion centred on the static nodal points and/or mode nodal points for holding the deformable frame via the recess and/or protrusion.

4. The actuator system according to claim 2 , wherein the frame connectors are rotation symmetric around the static nodal points and/or mode nodal points.

5. The actuator system according to claim 1 , wherein the connection between the actuator and deformable frame is centred on a mode anti-node of the deformable frame which is a position on a surface of the deformable frame where the modal deformation of the deformable frame is maximal in the excited state of the eigenmode M.

6. The actuator system according to claim 1 , wherein the deformable frame comprises a mirror symmetric structure wherein an equal but opposite force distribution is applied on either side of the mirror symmetric structure by one or more actuators therein between, the force distributions resulting in an equal but opposite deformation of the mirror symmetric structure.

7. The actuator system according to claim 1 , comprising at least two actuators working in opposite directions for applying equal but opposite force distributions on different sides of the deformable frame.

8. The actuator system according to claim 1 , further comprising a base frame holding the actuator module, wherein the actuator module is connected to the base frame by engaging respective frame connectors on the interface of the deformable frame.

9. The actuator system according to claim 8 , wherein a connection between the actuator module and base frame is rotationally free around a respective static nodal point and/or mode nodal point.

10. The actuator system according to claim 8 , comprising a translation and/or rotation system between the base frame and a stationary base for controlled translation and/or rotation of the base frame with respect to the stationary base.

11. The actuator system according to claim 8 , wherein the base frame is connected a plurality of actuator modules.

12. The actuator system according to claim 8 , wherein the actuation surface is arranged for actuating a probe tip for scanning a specimen surface in an atomic force microscope.

13. A computer-implemented method for designing an actuator module, the method comprising
simulating a deformable frame having a stiffness distribution and mass distribution;
simulating exerting a force distribution onto the deformable frame under quasi-static conditions;
calculating positions of static nodal points which are stationary during static deformation of the deformable frame under quasi-static conditions;
calculating a vibrational eigenmode of the deformable frame that couples to the force distribution when a magnitude of the force distribution is time-oscillated;
calculating positions of mode nodal points at an interface formed by a surface of the deformable frame which are stationary during modal deformation of the deformable frame-in an excited state of the eigenmode;
calculating a distance between the static nodal points and the mode nodal points and varying one or more of the force distribution, stiffness distribution, and/or mass distribution until the static nodal points coincide with the mode nodal points within a tolerance distance of less than one percent of a size across the interface of the deformable frame.

14. A method for manufacturing an actuator module comprising
designing an actuator module, by simulating a deformable frame having a stiffness distribution and mass distribution; simulating exerting a force distribution onto the deformable frame under quasi-static conditions;
calculating positions of static nodal points which are stationary during static deformation of the deformable frame under quasi-static conditions;
calculating a vibrational eigenmode of the deformable frame that couples to the force distribution when a magnitude of the force distribution is time-oscillated;
calculating positions of mode nodal points at an interface formed by a surface of the deformable frame which are stationary during modal deformation of the deformable frame in an excited state of the eigenmode; and
calculating a distance between the static nodal points and the mode nodal points and varying one or more of the force distribution, stiffness distribution, and/or mass distribution until the static nodal points coincide with the mode nodal points within a tolerance distance of less than one percent of a size across the interface of the deformable frame;
providing a deformable frame with the stiffness distribution and mass distribution according to the design; and
providing an actuator connected to the deformable frame and arranged for exerting a time-varying force distribution onto the deformable frame via a connection between the deformable frame and the actuator, wherein the force distribution at least under quasi-static conditions is arranged according to the design.

Assignees

• Nederlandse Organisatie Voor Toegepast-Natuurwetenschappelijk Onderzoek Tno

Inventors

• Witvoet Gerrit
• Van Den Dool Teunis Cornelis
• Crowcombe William Edward
• De Lange Theodorus Jacobus
• Pereboom Hajo Pieter

Classifications

• G01Q10/04 Primary

  Fine scanning or positioning · CPC title

• G06F17/11

  for solving equations {, e.g. nonlinear equations, general mathematical optimization problems (optimization specially adapted for a specific administrative, business or logistic context G06Q10/04)} · CPC title

• G01Q30/04

  Display or data processing devices · CPC title

• G06F30/20

  Design optimisation, verification or simulation (optimisation, verification or simulation of circuit designs G06F30/30) · CPC title

• G06F17/5009

  Physics · mapped topic