Exact analytical solutions are given for stationary two-dimensional temperature, stress, and displacement distributions in hybrid laminates containing isotropic and/or orthotropic layers. The similarity that exists between the thermoelastic and piezoelastic formulations is exploited in establishing solutions for cylindrical bending of piezother-moelastic laminates exposed to combined thermo-electro-mechanical loads. Results are compared with those based upon classical and high-order bending theories.