The present invention relates to a high-temperature
metal sealing ring for a small gas
turbine, comprising: a sealing ring, a sealing
mating surface and a
stress relief groove; the sealing
mating surface comprises a
mating surface 1 and a mating surface 2, and the
stress relief groove is arranged on the inner side of the sealing ring. The beneficial effects of the present invention are: a
stress relief groove is provided to absorb the high-temperature expansion, and when the temperature changes from low temperature to high temperature, the expansion direction will point to the direction of reducing the stress relief groove, which effectively solves the
stress concentration caused by high-temperature expansion and improves the service life of the
metal sealing ring under high temperature conditions; the width of the stress relief groove is set to the ring expansion of the sealing ring at the
working temperature of the sealing ring, and the stress relief groove is just closed during normal operation, which effectively improves the sealing effect under high temperature environment; there are sealing mating surfaces on both sides with a
surface roughness not greater than Ra0.8, and the free spacing is 1.005 to 1.01 times the width of the sealing groove, so as to ensure plane sealing during use, and use the
pressure difference to achieve sealing, thereby improving the sealing effect.