Tape type sensor array for rudders pneumatic power parameter testing

A belt sensor array for aircraft pneumatic parameter testing based on multi-sensor includes a belt sensor composed of eight relatively dependent test nodes, x(x is less than or equal to 32) belt sensors are connected in series and form a sensor testing belt comprising m(m is less than or equal to 256) test nodes, n rows of sensor testing belt are parallel arranged and constitute a belt sensor array comprising m multiplied by n test nodes, a row test belt information management module is arranged between every row of sensor testing belt, test nodes in every row are connected with the row test belt information management module of the row through a special bus, row test belt information management module transfers information of the entire row to a data recorder through a high speed bus. Every test node of the invention is a comparatively independent unit, any position on an aircraft surface can be tested with parameters of vibration, pressure, temperature and strain, the invention can be applied to pneumatic p