The invention relates to the field of liquid-
propellant rocket engine
turbine pumps, and provides a high-temperature gas outlet end connecting structure of a low-temperature
turbine pump. The high-temperature gas outlet end connecting structure comprises a high-temperature gas outlet
pipe and a low-temperature shell, wherein the low-temperature shell is mounted on a rotating shaft through a
turbine end bearing, a
turbine rotor is fixed on the rotating shaft, the high-temperature gas outlet
pipe comprises an outlet
flange, a transition section, a small end, a gas collecting
pipe and a large end, a flow guiding support plate is arranged in the circumferential direction of the inner surface of the gas collecting pipe, the outlet
flange, the transition section, the small end, the flow guidingsupport plate, the gas collecting pipe and the big end are integrally formed, and are made of high-temperature
alloy materials, the large end and the small end are arranged on the two opposite sides of the gas collecting pipe, and the high-temperature gas outlet pipe and the low-temperature shell are connected through
nuts and bolts. An internal profile of the high-temperature gas outlet pipe is subjected to three-dimensional optimization, the high-temperature gas outlet pipe is guaranteed to be smooth in circulation and extremely small in loss, and the
working capacity and efficiency of the turbine pump are improved.