Rigidizable insertion tool with position adjustment

Abstract

In some embodiments, apparatuses and methods are provided herein useful to inspect aircraft engine. In some embodiments, a rigidizable insertion tool includes a plurality of links arranged in a sequence. The plurality of links includes at least one deformable link that is structurally deformable. The rigidizable insertion tool may include a tension assembly configured to apply a first tensioning force on the plurality of links to actuate the plurality of links from a relaxed state to a rigidized state having a first shape. The tension assembly may apply a second tensioning force greater than the first tensioning force on the plurality of links while in the rigidized state to cause structural deformation of the at least one deformable link and change a shape of the plurality of links from the first shape. The second tensioning force may change the shape from the first shape to a second shape.