Thermal, elastic, and feedback analyses are applied to the case of a beam with a distributed thermal actuator. The actuator is capable of producing a thermal gradient across the section of the beam. One candidate for such an actuator uses the Pettier effect, which appears in certain semiconductors. These devices act as heat pumps when a voltage is applied, causing a temperature gradient. It is shown that the thermal gradients can induce deflection in the beam. If the thermal gradients are applied in the proper sense to a vibrating beam, it is possible to increase the vibration damping exhibited by the structure. Experimental results are given for a cantilever beam, whose first vibrational mode damping ratio was increased from 0.81 to 1.4% with simple lead compensation. Nomenclature A = cross-sectional area of beam b = beam width CQV - voltage to heat flow conversion constant C(s) = compensator dynamics c = specific heat d = separation of cap neutral axis from beam centroid E = Young's modulus H = Heaviside step function Gs - sensor gain coefficient g = acceleration of gravity at Earth's surface h = depth of beam cap / = bending moment of inertia / = electric current K = thermal conductivity Kc = compensator gain <£ { j = Laplace transform of { ) £ = length of beam 4 = thermal length of beam section near actuator MT = bending moment induced by applied thermal gradient
[1]
J. C. Jaeger,et al.
Conduction of Heat in Solids
,
1952
.
[2]
Andrew P. Sage,et al.
Linear systems control
,
1978
.
[3]
H. Ashley,et al.
On Passive Damping Mechanisms in Large Space Structures
,
1982
.
[4]
U. Lee.
Thermoelastic and electromagnetic damping analysis
,
1985
.
[5]
F. B. Hildebrand.
Advanced Calculus for Applications
,
1962
.
[7]
Raphael T. Haftka,et al.
An analytical investigation of shape control of large space structures by applied temperatures
,
1985
.
[8]
William Prager,et al.
Theory of Thermal Stresses
,
1960
.