| 摘要 |
FIELD: measuring equipment.SUBSTANCE: claimed invention relates to automatic means of continuous monitoring of condition of launching facility during its operation. System which implements disclosed method, containing set of measuring transducers, signal pre-processing unit, including analogue-to-digital converter board, communication link, bus, signal matching device, converter, control station made in form of computer, and display connected to latter, audio alarm device, conditional image of controlled structure with colored marks-indicators, planned high-rise geodetic base of launching facility and temperature pressure fields at surface protective coating of launching facility change monitoring set. Planned high-altitude geodetic base of launching facility is network of deep reference points in form of three “clusters” and one reference point 14, arranged uniformly around launching facility at distance of 60-80 m from it, as well as system of deformation grades. Each “cluster” includes three depth levelling points. Set of pressure and temperature field on surface of launching facility protective coating change monitoring pressure and temperature sensors are adopted mounted on protective coating of launching facility on one visible straight line.EFFECT: high measurement accuracy and reliability of long-term monitoring of launching facility structure.2 cl, 4 dwg |
