First published online April 26, 2005
Journal of Experimental Biology 208, 1653-1664 (2005)
Published by The Company of Biologists 2005
doi: 10.1242/jeb.01483
Scaling of maximum net force output by motors used for locomotion
James H. Marden
208 Mueller Laboratory, Department of Biology, University Park, PA
16802, USA

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Fig. 1. Cross section of a Drosophila melanogaster (fruit fly) thorax (ca.
0.0003 g) and a diesel engine (118 681 kg). Along with superficial shape
similarities, vastly different motors have very similar performance in terms
of force output per motor mass. (Drosophila image courtesy of R.
Ordway.)
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Fig. 2. Maximum force output by translational motion motors (Group 1) as a function
of their mass. The least squares fit (solid line) is:
Fmax=891 M0.67. The dashed line is the
scaling fit for Group 2 motors in which Fmax scales as
M1.0 (Fig.
3). Maximum force output (N) and motor mass (kg).
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Fig. 3. Maximum force output by Group 2 motors as a function of their mass. The
least squares fit (solid line) is: Fmax=55
M0.999. The dashed line is the scaling fit for Group 1
motors for which Fmax scales as M0.67
(Fig. 2). Inset: the frequency
distribution of mass specific force output for all of the Group 2 motors on
the main plot. Maximum force output (N) and motor mass (kg).
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Fig. 5. Force outputs of small Group 3 motors (red curve) that operate in the
viscous regime. For comparison, data are included for Group 1 motors, along
with a dashed line representing Group 2 motors. The scaling curve for Group 3
motors connects their performance with that of the smallest Group 2 motor
(fruit fly). Maximum force output (N) and motor mass (kg).
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Fig. 6. Load-life curves for steel bearings (solid circles) and entire turbine
engines (open circles).
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Fig. 7. Predicted lifespan (N cycles) over a range of mass specific force
outputs for a generalized 1 kg motor that can withstand a maximal force load
of 890 N. This curve assumes that a=1 and b=3 in the
load-life equation (Eqn 2). Also shown is a curve relating specific load to
the observed number of wingbeat cycles for hummingbirds over one day of normal
flight (a highly conservative estimate of cycles to failure) and during
experimentally imposed maximal loading.
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Fig. 8. Specific force output (N kg-1 motor mass) for three electric
motors used with different combinations of propellers, gear ratios, voltage
and current. Dark bars show combinations that are indicated by the
manufacturer to cause rapid failure. Superimposed images show a schematic and
a photograph of one of these motors, consisting of the motor, gears and
propeller nose cone.
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Fig. 9. A general model for the load-life curve of motors, with transitions from
high-cycle to low-cycle fatigue occurring in the region between about 55-120 N
kg-1. In the background is the frequency distribution of specific
force output of all Group 2 motors from
Fig. 3.
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Fig. 10. Scaling of maximum force output (A) and ratio of total piston cross
sectional area to stroke length (B) in relation to motor mass over the entire
size range of piston engines. The vertical dashed line indicates the crossing
point of the scaling fits for Group 1 (dashed line) and Group 2 (solid line)
motors. Maximum force output (N), motor mass (kg), total piston area/stroke
length (m2 -1).
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Fig. 11. Cross sectional schematic of one of the largest piston engine (Burmeister
and Wain K98MC-C) and three of its human operators. The geometry of piston
engines larger than 4400 kg departs radically from what would be predicted
from the scaling of smaller piston engines; this departure begins at the
crossing point of the scaling relationships for Group 1 and Group 2 motors.
Reproduced with permission from B&W Engine Selection Guide, February
2000.
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© The Company of Biologists Ltd 2005