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A Process for Solving Fluorescent Cracks in Cast Titanium Alloys

A technology of casting titanium alloy and process method, which is applied in the field of metal materials, can solve the problems that the product is difficult to reach the qualified state, and there are too many cycles, so as to protect the quality and safety of the product, reduce the difficulty of operation, and solve the effect of fluorescence problems

Active Publication Date: 2021-10-15
AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Because the formed titanium alloy castings are cycled too much between the above processes, it is difficult for the products to reach the qualified state

Method used

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  • A Process for Solving Fluorescent Cracks in Cast Titanium Alloys
  • A Process for Solving Fluorescent Cracks in Cast Titanium Alloys
  • A Process for Solving Fluorescent Cracks in Cast Titanium Alloys

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0034] Such as image 3 , Figure 4 As shown, the fluorescent crack problem of a cast pure titanium casting is solved. The concrete steps of the inventive method are as follows:

[0035] First, before painting, double-sided adhesive tape is used to mark the oxyacetylene cutting part, and the width of the double-sided tape is 15mm; then, the casting part that may be touched by the flame or roasted is protected by high-temperature paint brushing the wall (protection of high-temperature paint Temperature ≥ 1700 ℃), coating thickness 1.5mm; tear off the top layer of double-sided adhesive tape, so that the flame cutting part is in a state of no coating; then cut the riser: keep the flame center cutting point 12mm away from the casting surface, Use the traditional oxyacetylene flame cutting method to cut off the casting from the gating system at the position marked by the sticker; finally, clean the coating of the casting after cutting: after cutting the spout, use water to blow s...

Embodiment 2

[0037] Such as Figure 5 , Image 6 The fluorescent crack problem of a ZTC4 cast titanium alloy ring casting shown is solved. The concrete steps that adopt technical scheme of the present invention are as follows:

[0038] First, before coating, mark the oxyacetylene cutting part with double-sided adhesive tape, the width of the double-sided adhesive tape is 15mm; then use high-temperature coating to completely immerse the casting to protect it (the protection temperature of high-temperature coating is ≥ 1700 ℃), and the coating Thickness 1.0mm; tear off the top layer of double-sided adhesive tape, so that the flame cutting part is in a state of no paint; then cut off the pouring riser: keep the cutting point of the flame center at a distance of 11mm from the casting surface, using the traditional oxyacetylene flame cutting method Cut off the casting from the pouring system facing the position marked by the sticker; finally, clean the coating of the casting after cutting: af...

Embodiment 3

[0040] Such as Figure 7 , Figure 8 As shown, the fluorescent crack problem of a ZTA15 cast titanium alloy frame casting is solved. The concrete steps that adopt technical solution of the present invention are as follows:

[0041] First, before coating, mark the oxyacetylene cutting part with a double-sided adhesive tape with a width of 10 mm; then use high-temperature paint to protect parts of the casting that may be touched by flames or baked for extra-large castings (protection temperature of high-temperature paint ≥1700℃) coating protection, the other part uses high-temperature coatings to completely immerse coating protection on the castings, the coating thickness is 1.2mm; tear off the top layer of double-sided adhesive tape, so that the flame cutting part is in a state of no coating; then carry out Removal of the pouring riser: Keep the cutting point of the flame center at a distance of 11mm from the surface of the casting, and use the traditional oxyacetylene flame ...

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Abstract

The invention belongs to the field of metal materials, and relates to a process method for solving fluorescent cracks in cast titanium alloys. The invention recognizes and marks the cutting parts of casting risers, and adopts double-sided adhesive tape to paste the flame-cut casting parts, so as to prevent the castings that may be touched by flames. The parts are protected by high-temperature paint, which blocks the burning or roasting of the surface of the titanium alloy casting by the flame when the casting riser system is cut by the oxyacetylene flame, eliminates the main factor of cracks on the casting surface, eliminates the occurrence of cracks, and reduces The number of post-finishing cycles to deal with cracks in production greatly improves production efficiency; it reduces product scrapping caused by repairing welding and annealing times exceeding the standard requirements due to crack defects, and greatly improves the yield; reduces casting repair defects The necessary number of thermal cycles reduces the hidden dangers of titanium alloy castings and improves product quality and safety.

Description

technical field [0001] The invention relates to a process method for solving fluorescent cracks in cast titanium alloys, in particular to a method for cutting risers of titanium alloy castings for avoiding fluorescent cracks. Belongs to the field of metal materials Background technique [0002] Titanium alloy has the characteristics of high specific strength, strong corrosion resistance, and non-magnetic properties. It is one of the ideal structural materials for aerospace. At present, the amount of titanium used in the aviation industry accounts for more than half of the world's titanium consumption, and it is a well-deserved aviation material. The complexity and integration of components can make a great contribution to improving the thrust-to-weight ratio of aerospace engines. Casting is an excellent way to achieve near net shape of complex, monolithic titanium alloy parts. The casting process structure is very complicated, and a complex gating and riser structure syst...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B22D31/00
CPCB22D31/00
Inventor 冯之华贺靠团冯新贾志伟南海张爱斌
Owner AVIC BEIJING INST OF AERONAUTICAL MATERIALS