The invention discloses a 
titanium alloy thin-wall part hot-stretch 
creep deformation composite molding method. The 
titanium alloy thin-wall part hot-stretch 
creep deformation composite molding method comprises eight steps that 1, equipment and raw materials are prepared; 2, 
electrode splints are electrified and a blank material needing to be molded is heated; 3, real-time measure of a temperature of the blank material needing to be molded is carried out and output 
voltage of a power supply is adjusted in real time to realize a blank material heating rate of 5 to 25 DEG C per second; 4, when a temperature of the blank material needing to be molded is in a range of 600 to 750 DEG C, jaws of a stretch molding device clamp the blank material needing to be molded and the blank material needing to be molded is subjected to pre-stretch at a preset 
strain rate; 5, when a pre-strain ratio is in a range of 0.1 to 4%, the molded blank material is subjected to 
coating at a temperature of 600 to 750 DEG C and a preset 
strain rate until the molded blank material is completely fitted to a mold; 6, the molded blank material treated by the step 5 is subjected to stretch supplement at a temperature of 600 to 750 DEG C and a preset 
strain rate until an end strain ratio is in a range of 0.1 to 8%; 7, the molded blank material treated by the step 6 is subjected to heat preservation for a period of time so that 
stress relaxation in the molded blank material occurs and 
creep deformation molding is realized; and 8, the 
powder supply is 
cut off and the molded blank material treated by the step 7 is cooled and is taken down.