The invention relates to an
integrated manufacturing method for a pintle type head interlayer shell of an airspace engine. A three-dimensional model of the
metal shell is set up, and the STL formattedfile of the three-dimensional model is guided into a Magics additive manufacturing auxiliary
software platform; according to the structure characteristics of the
metal shell, the forming direction and the placement position are confirmed, and a
process support is designed and added; TC4
titanium alloy laser selective melting forming
processing technological parameters are input slice
software, and the model added with the support is subjected to
slicing treatment; forming is carried out under protection of
inert gas; after forming is finished, floating
powder is cleared away, and the shell issubjected to heat treatment; a substrate and the shell are linearly
cut and separated, the auxiliary support is removed, and finishing and
grinding are carried out; and the shell is subjected to surface treatment. By means of the method, the pintle type head interlayer shell of the airspace engine are designed and manufactured according to the additive manufacturing process technology, a shell component is integrally manufactured through the
metal additive manufacturing method, and the
manufacturing quality reliability of the pintle type head interlayer shell of the airspace engine is improved.