The invention discloses a combined sealing method and device for a continuous low-temperature
combustion rotary engine. The combined sealing method and device are characterized in that the device comprises a continuous low-temperature
combustion rotary engine shell (1), a main shaft timing gear (2), an auxiliary shaft timing gear (3), a right auxiliary shaft oil seal (5), an end face sealing hex socket (6), an auxiliary wheel (8), an auxiliary shaft (9), an end
face seal (10), a main shaft (12), a bearing seal (16), an end face outer leakage sealing ring (17), an end face inner leakage sealing ring (18), a main shaft auxiliary gear matching part (19), a main shaft gear (20), an end face inner seal (21), a left auxiliary shaft oil seal (22), an upper air inlet (23), a main shaft gear protrusion groove (24), a main shaft gear protrusion (25), an upper exhaust port (26), a lower air inlet (27), a lower exhaust port (28), an end face sealing installation hole (29), an end face sealing positioning pin (30), an end face inner leakage sealing groove (31), an end face outer leakage sealing groove (32) and an auxiliary wheel groove (33). By means of the scheme, the sealing problem in the air intake,
combustion and expansion processes of the novel continuous combustion low-temperature
rotary engine is solved, due to axial sealing and radial sealing and meanwhile by the adoption of a non-contact combined sealing technology, movable sealing of the whole
system can be achieved, and the sealing requirement is met.