System of the Monitoring the Aircraft Construction in the Tests Process

Abstract

The necessity of the organization and implementation of continuous monitoring of deformations in the dements of the aircraft construction for the early detection of critical values is shown. The short review of existing methods and devices for measuring micro-movements is given. Variants of designs of micro-movements sensors are considered and a block diagram of a measuring instrument, which was built on the basis of a capacitive transducer with an "open" field, is given. The functioning of the system of non-contact measurement of deformation elements of the aircraft structure is considered.