MICRO ROTARY BALL
BEARING WITH INTEGRATED
BALL CAGE:
FABRICATION AND CHARACTERIZATION
Robert Hergert, Ingrid S.Y. Ku, Tom Reddyhoff, and Andrew S. Holmes
Imperial College London, UK
Journal:- IEEE 23 rd INTERNATIONAL CONFERENCE ON MEMS (Micro Electro Mechanical Systems), 2010
v ABSTRACT
This paper presents a
rotary MEMS ball bearing with an integrated silicon ball cage. The device is a deep
groove radial ball bearing consisting of steel balls encapsulated between two
micromachined silicon wafers. The silicon ball cage is released from the bulk
silicon substrate during fabrication. The objective was to show that a simple
caged bearing design provides reliable motion at both high and low speeds.
v INTRODUCTION
Reliable rotary MEMS devices
require a long lasting and mechanically stable bearing.
They can provide greater
longevity and higher speed operation than pin-joint bearings while being more
stable and easier to control than magnetic levitation bearings. Ball bearings can
also operate reliably at lower speeds and have a less complex design than air
bearings such as those described in. Ghodssi et al. have recently demonstrated
the effectiveness of micro ball bearings in MEMS devices. As discussed in, one
of the problems encountered in current designs is the tendency for the balls to
co-locate or jam in the bearing raceway. We have addressed this problem by
integrating a ball cage in our design.
v DESIGN
Figure 1 - CAD rendering of an
assembled bearing with ball cage (left) and exploded diagram showing all of the
individual parts (right).
In the exploded diagram on the
right the top part is the bearing rotor. The middle part represents the ball
cage with the steel balls in the cage openings. Both of these parts fit into
the stator, at the bottom, which is designed to fit into a torque testing
device. All of the pieces, with the exception of the steel balls, are
fabricated from a silicon substrate. The bearing is fabricated in two halves, which
are held together with solder bonds.
Figure 2 - Depiction of the
bearing design parameters: g -cage release gap (40μm), C – cage width (100μm),
t –raceway tolerance (10μm), Dr – rotor diameter (1.18mm), Db – bearing raceway
diameter (2.2mm).
v FABRICATION
Figure 4 - SEM images of the micromachined
bearing parts: ball cage (top left), rotor (top right), stator (bottom left)
and fully assembled device (bottom right).
Figure 5 - SEM image of DRIE damage on the
stator. Similar damage is present on the rotor.
v TEST SETUP
Prototype ball bearings have been characterized
in a custom microtribology test rig developed at Imperial College. A full
description of the measurement setup can be found in [7]. The rig allows the
measurement of the frictional torque of the ball bearing under varying normal
loads and over a range of rotational speeds. The outer part of the bearing is
mounted in a silicon micromachined test platform incorporating an elastic
suspension (see Figure 6), while the inner part is coupled to the shaft of a precision
motor, which provides both normal force and rotation.
Figure 6 - Micromachined test
platform. Outer springs are used to determine normal load; inner platform beams
are used to measure applied torque.
The limitation of this testing
arrangement is that we can only measure the axial normal load and not the radial
load on the bearing. However, this does provide the opportunity to stress test
the device using the least ideal load configuration for a radial deep groove
bearing.
v RESULTS
Initial testing shows that the
bearings perform well at both high and low speeds. Testing was carried out on
two devices at speeds ranging from 10 to 20,000 rpm with a 60mN axial load. The
motor used during testing limited the maximum speed. The torque profile for the
devices conforms to the expected torque curve. At lower speeds the torque will
decrease as the balls move from sliding and stick/slip to rolling friction.
Figure 8 shows the average of three low speed torque measurements for both
tested bearings.
Torque measurements from three
high speed tests on the second device.
After 5 hours of continuous
testing, we debonded the second device to evaluate the wear at the contact
points between the steel balls and the silicon cage and raceway. Figures 9 to
11 show that there was relatively little wear of the silicon structures during
testing. The first device failed after 3 hours of testing due to poor adhesion between
the solder and the silicon arms of the cage.
SEM image showing the wear on one
half of the ball cage. Wear areas enclosed in the circles are the lateral
contact points of the steel balls.
v CONCLUSION
We have shown that an
encapsulated ball bearing with an integrated ball cage can perform reliably between
10 and 20,000 rpm. The current design shows relatively minimal silicon wear
after several hours of continuous operation. A closer evaluation of the
fabrication damage and the testing wear will need to be carried out determine
the causes of the raceway damage. These initial results seem to indicate that a
micro ball bearing with an integrated
cage could provide a stable
platform for rotary MEMS devices at both high and low speeds.
However, longevity and higher
speed testing would provide a clearer picture of the durability and applicability
of the design.
REFERENCES
[1] D. M. Tanner, J. A. Walraven, S. S. Mani, S. E.
Swanson, “Pin-joint design effect on the
reliability of a polysilicon microengine,” Proc.
of IRPS, pp. 122-129, 2002.
[2] S. Lee, K. Daejong, M.D. Bryant, F.F. Ling, “A
micro corona motor,” Sensors and Actuators: A.
Physical, vol. 118, No. 2, pp. 226-232, 28 Feb.,
2005.
[3] S. Tanaka, Y. Miura, P. Kang, et al., “MEMSbased
air turbine with radial-inflow type journal
bearing,” IEEJ Trans on Electrical and
Electronic Engineering, vol. 3, No. 3, pp. 297-
304, 2008.
REFERENCES
[1] D. M. Tanner, J. A. Walraven, S. S. Mani, S. E.
Swanson, “Pin-joint design effect on the
reliability of a polysilicon microengine,” Proc.
of IRPS, pp. 122-129, 2002.
[2] S. Lee, K. Daejong, M.D. Bryant, F.F. Ling, “A
micro corona motor,” Sensors and Actuators: A.
Physical, vol. 118, No. 2, pp. 226-232, 28 Feb.,
2005.
[3] S. Tanaka, Y. Miura, P. Kang, et al., “MEMSbased
air turbine with radial-inflow type journal
bearing,” IEEJ Trans on Electrical and
Electronic Engineering, vol. 3, No. 3, pp. 297-
304, 2008.
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