The invention belongs to a blade clearance measuring technology, and particularly relates to a method for measuring the
tip clearance of
turbine concave cavity blades. Disclosed by the invention is a method for measuring the
tip clearance of the
turbine concave cavity blades, which comprises the steps of firstly acquiring original blade tip signals and carrying out filtering and
smoothing processing, then setting high and low threshold levels according to the shape of the concave cavity blades, enabling the high level to be between the peak of original blade
tip clearance signals and the concave cavity valley, enabling the low level to be between inter-blade valley signals and concave cavity valley signals, differentiating different blades according to the low level, identifying two peaks according to the high level, extracting
peak level, and then determining tip clearance values at a blade back side and a blade basin side according to a fitting relation between clearance and
voltage. According to the invention, blade tip signals at the blade back and the blade basin of
turbine concave cavity blades can be identified and extracted based on a full-period sampling technology based tip clearance measuring
algorithm, variations in tip clearance at the back and the basin are monitored visually in real time, and whether collision occurs or not between the blade tip and a casing can be judged precisely.