The invention relates to a plane component deformation
decomposition and vibration mode identification method based on an
orthogonal decomposition theory. The method comprises the following steps: step 1, the plane deformation of a four-node square unit is formed by laminating eight basic deformation such as the
rigid body displacement in an x direction, the
rigid body displacement in a y direction, the extruding deformation in the x direction, the extruding deformation in the y direction, the bending deformation in the x direction, the bending deformation in the y direction, the shear deformation and the
rigid body rotation displacement; targeting for the four-node square unit, an
orthogonal decomposition method is adopted to respectively establish the basic
deformation vector of each of the rigid body displacement in the x direction, the rigid body displacement in the y direction, the extruding deformation in the x direction, the extruding deformation in the y direction, the bending deformation in the x direction, the bending deformation in the y direction, the shear deformation and the
rigid body rotation displacement. The method is also applicable when the structure of a plane component is divided into large units, the calculation
workload is alleviated; moreover, the bending deformation and the shear vibration mode can be identified, and the stress situation and vibration type inside a component can be more accurately and completely reflected.