The invention discloses a forming method and structure of a complex-shape
metal-based sweating and cooling control surface, relates to the technical field of
thermal protection of hypersonic aircrafts, and is used for realizing connection of a
front edge structure of a control surface and a main body structure of the control surface. A defocusing
electron beam is adopted to preheat the
welding part; after the preheating process is ready, an electromagnetic lens is adjusted to focus an
electron beam to a
welding area of the workpiece, it is ensured that energy of the
electron beam can be concentrated on a
welding point, and welding of a control plane
front edge structure and a control plane main body structure is started; welding pores are eliminated using electron beam modification welding. A complex-shape
metal-based sweating cooling control
surface structure is manufactured by adopting a complex-shape
metal-based sweating cooling control surface forming method, the complex-shape metal-based sweating cooling control
surface structure is composed of a control surface
front edge structure and a control surface main body structure, and the control surface front
edge structure is provided with micro channels. According to the method, the welding connection is realized by adopting a process of combining electron beam defocusing preheating before welding, vacuum
electron beam welding and electron beam modification welding, so that the permeability and the pressure-bearing performance of the control surface are ensured.