The　intelligent　structure　will　be　the　key　to　the　industrial　manufacturing　field　in　the　future,　piezoelectric　materials　are　the　most　commonly　used　active　materials　in　many　mechatronic　and　vibration　control　systems.　In　this　paper,　we　illustrated　the　nonlinear　vibration　behaviors　of　the　piezoelectric-laminated　composite　cantilever　rectangular　plate　subjected　to　transverse　and　parametric　excitation.　Two　piezoelectric　layers　are　attached　to　the　upper　and　lower　surfaces　of　graphite/epoxy　composite　laminated　plate.　The　nonlinear　dynamic　equations　are　derived　via　the　classical　laminated　plate　theory,　von　Karman　large　deformation　theory,　the　constitutive　equation　of　the　piezoelectric　materials,　and　the　Hamilton　principle.　Considering　the　Galerkin　method,　the　nonlinear　ordinary　differential　equations　for　the　two-order　vibration　mode　of　the　piezoelectric　laminated　composite　cantilever　rectangular　plate　are　achieved.　The　multiple　scale　method　is　applied　to　obtain　the　average　equations　to　study　the　nonlinear　vibration　characteristic　of　the　stable　motion.　The　primary　resonance　and　the　1:1　internal　resonance　of　the　piezoelectric　laminated　composite　cantilever　rectangular　plate　are　investigated.　The　amplitude-frequency　response　curves,　force-amplitude　response　curves,　time　histories,　phase　curves,　and　bifurcation　diagrams　are　given　to　investigate　the　nonlinear　dynamic　characteristic　of　the　piezoelectric　laminated　composite　cantilever　rectangular　plate.　The　detailed　parametric　analyses　show　that　bubble　response　curves　are　separated　from　the　amplitude-frequency　response　curves　with　the　continuous　increase　of　the　external　excitation　due　to　the　internal　resonance.　In　addition,　the　results　reveal　the　energy　transform　between　the　various　order　vibration　modes　of　the　system.　This　work　is　expected　to　provide　theoretical　guidance　for　the　nonlinear　vibration　of　the　smart　piezoelectric　laminated　composite　structure.