Repair method for inter-layer delamination of fiber-wound shell of solid-propellant rocket engine
A solid rocket and motor technology, which is applied to other household appliances, household appliances, household components, etc., can solve the problems of the influence of the reliability of the insulation layer and the weakening of the strength of the composite layer, and achieve the effect of low requirements, reducing damage and avoiding damage.
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[0058]A certain type of solid rocket motor shell is a fiber-wound composite shell, and its thermal insulation layer is EPDM rubber. The surface of the 2.5mm thick thermal insulation layer has a bulge defect with an area of 800mm×300mm, and the defect depth is 3.0mm. In the composite layer, if the existing repair plan is used, a large area of the insulation layer needs to be excavated, limited by the thickness of the insulation layer and the area of the word repair, the repair cycle is long, and the delivery node cannot be met, and it is forced to dig It will damage the interface between the composite layer and the thermal insulation layer and the surface fiber, which will affect the strength of the shell itself. The repair method of the present invention is as follows
[0059]1) Determine the defect area and defect depth through ultrasonic C-scan or DR inspection;
[0060]2) Use a blade to dig two pits with a diameter of 3mm at both ends of the defect area until the interface of the...
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