The invention provides an optical method based high-speed aircraft hot surface full-field deformation measuring device. The optical method based high-speed aircraft hot surface full-field deformation measuring device comprises a double-layer
quartz lamp heating array, a thin-wall high-speed aircraft shell, a square transparent window, speckle particles, a
thermocouple sensor, a
signal amplifier, a
temperature control computer, a driving power supply, a
CMOS (Complementary
Metal Oxide Semiconductor) camera, a lens, a narrow-band-pass
optical filter and an
image processing computer. In order to solve the problem of
signal blockage caused by a high temperature
radiant heat source between the
CMOS camera and the surface of the high-speed aircraft shell, the vertical double-layer
quartz lamp heating array is designed and the square transparent window with small area is formed, so that the optical
camera lens can obtain images of the hot surface of the high-speed aircraft through the transparent window. The interference light
ray of the
quartz lamp heating array is shielded by selecting the narrow-band-pass
optical filter with specific wave length, so that speckle images with high quality and no degeneration on the hot surface of the high-speed aircraft is obtained; a
digital image correlation method is utilized for analyzing the speckle images under different temperatures to realize full measurement on the
displacement field and the strain field of the hot surface of the high-speed aircraft in a high temperature environment.