AIRCRAFT WING STRENGTH CONTROL DEVICE Russian patent published in 2012 - IPC G01N3/02 G01M7/00 

FIELD: transport.

SUBSTANCE: proposed device comprises three vibration transducers located at center of gravity and left and right outer wings, analog signal switch, ADC, three parallel registers, two adders, two operating memories, address modification counter and control unit. In compliance with this invention, added are address modification counter control device, microcomputer, unit of buffer registers and onboard flight parameters recorder. Note here that outputs of memories are connected to microcomputer 1^st and 2^nd inputs. Microcomputer 3^rd input made a data input of "start" signal while 2^nd input is connected to second input of address modification counter control device first input of which makes data input of signal "Manual reset". Said 3^rd input is connected with third inputs of memories fourth inputs of which are connected to first input of address modification counter control device with its 2^nd input connected to address modification counter.

EFFECT: higher validity of control.

11 dwg