CN206732060U - The fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings - Google Patents

The fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings Download PDF

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Publication number
CN206732060U
CN206732060U CN201720529689.6U CN201720529689U CN206732060U CN 206732060 U CN206732060 U CN 206732060U CN 201720529689 U CN201720529689 U CN 201720529689U CN 206732060 U CN206732060 U CN 206732060U
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Prior art keywords
insulated feeder
spherical
aviation casing
fire
aviation
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CN201720529689.6U
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Chinese (zh)
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杨庭彰
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Harbin Futing Chuangfu Machinery Manufacturing Co Ltd
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Harbin Futing Chuangfu Machinery Manufacturing Co Ltd
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Abstract

The utility model discloses the fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings, it is related to metal working technical area, and in particular to the improved technology of the fire-retardant anti-oxidation insulated feeder structure of aviation casing Mg alloy castings.Including aviation casing casting body, there is spherical feeding insulated feeder above aviation casing casting body;Spherical feeding insulated feeder top is spherical, bottom is inverted-cone shape structure, and spherical feeding insulated feeder internal layer is that titanium dioxide silica brick internal layer rising head, centre are that alumina silicate heat-insulation layer, outer layer are outer layer molds;Funnel shaped casting nozzle is connected above spherical feeding insulated feeder.The aviation casing Mg alloy castings insulated feeder that the utility model solves magnesium alloy is usually V-arrangement or stairstepping, rapid heat dissipation, the problem of influenceing the feeding performance of rising head.

Description

The fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings
Technical field
It the utility model is related to metal working technical area, and in particular to the fire-retardant anti-oxidation guarantor of aviation casing Mg alloy castings The improved technology of warm dead head structure.
Background technology
Magnesium alloy is adapted to apply in specific field, such as aviation field.Magnesium alloy high is subtracted with it than performance, protrusion Suction of shaking is made an uproar ability, good forming processing performance and the features such as be easily recycled, and is described as the green knot of 21 century Structure material.Magnesium alloy is prone to oxidizing fire in melting, liquid forming and heat treatment process, it is desirable to provide effective fire-retardant Protection.At high temperature, fire-retardant especially under molten condition is for magnesium and its alloy:Using method physically or chemically, on its surface Effective protection aquiclude is formed, on the one hand completely cuts off air, on the one hand prevents magnesium from evaporating, reach and slow down oxidation, fire-retardant purpose.
It can mitigate weight, the mobility for improving aerospace vehicle using the aviation casing of magnesium alloy, reduce oil consumption, band Carry out considerable economic benefit.
During fabrication, the effect of insulated feeder is to be emitted by extending rising head setting time to improve to the aviation casing of magnesium alloy The feeding efficiency of mouth.In Foundry Production, it is one of important measures for ensureing casting quality to set rising head, and its main function is pair Casting carries out feeding.Existing aviation casing Mg alloy castings insulated feeder is usually V-arrangement or stairstepping, because this structure emits Larger, the rapid heat dissipation of mouth opening, influence the feeding performance of rising head.
The content of the invention
The utility model provides the fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings, and the utility model solves magnesium The aviation casing Mg alloy castings insulated feeder of alloy is usually V-arrangement or stairstepping, rapid heat dissipation, influences the feeding performance of rising head Problem.
To solve the above problems, the utility model adopts the following technical scheme that:The fire-retardant oxygen of aviation casing Mg alloy castings Change insulated feeder, including aviation casing casting body, have spherical feeding insulated feeder above aviation casing casting body;It is spherical Feeding insulated feeder top is spherical, bottom is inverted-cone shape structure, and spherical feeding insulated feeder internal layer is in titanium dioxide silica brick Layer rising head, centre are that alumina silicate heat-insulation layer, outer layer are outer layer molds;Funnel shaped casting is connected above spherical feeding insulated feeder Mouthful.
The utility model advantage:Spherical feeding insulated feeder is designed with, rising head can accommodate more raw material, riser openings Smaller, radiating is few, improves heat insulating ability.Rising head uses alumina silicate heat-insulation layer, high insulating effect, the product quality stabilization of production.
Brief description of the drawings
Fig. 1 is the utility model structure diagram.
Symbol description in figure:Aviation casing casting body 1, casting nozzle 2, spherical feeding insulated feeder 3, alumina silicate heat-insulation layer 4, Titanium dioxide silica brick internal layer rising head 5, outer layer mold 6.
Embodiment
The utility model is described in detail with optimal embodiment below.
As shown in figure 1, the superpower feeding insulated feeder of aviation casing magnesium alloy casting, including aviation casing casting body 1, Aviation casing casting body 1 has spherical feeding insulated feeder 3 above;The spherical top of feeding insulated feeder 3 is spherical, bottom is down Put pyramidal structure, the spherical internal layer of feeding insulated feeder 3 be titanium dioxide silica brick internal layer rising head 5, centre be alumina silicate heat-insulation layer 4, it is outer Layer is outer layer mold 6;Spherical feeding insulated feeder 3 connects funnel shaped casting nozzle 2 above.
The top of spherical feeding insulated feeder is spheroidal, and here is inverted-cone shape structure, is easy to spherical feeding insulation to emit Intraoral raw material is injected into casting.Spherical feeding insulated feeder diameter is formulated according to design requirement.Spherical feeding insulated feeder It is interior to accommodate more raw material.Spherical feeding insulated feeder top connects funnel shaped casting nozzle, is easy to supplement injection liquid.By Small in spherical feeding insulated feeder upper port and funnel shaped casting nozzle junction port, radiating is small, heat-insulating property increase.Using silicon Sour aluminium heat-insulation layer be using hard paste clinker as raw material, be substitute asbestos heat insulating material, the heatproof of aluminium silicate wool:800- 1200 degrees Celsius.
Titanium dioxide silica brick internal layer rising head of the present utility model, be using earth silicon material fire form, method for cooking with Silica brick producing process is identical.Titanium dioxide silica brick internal layer rising head is that casting mold is interior for storing feeding a casting molten metal, and Exhaust, the cavity of collection slag effect can be designed, to avoid casting from the supplement knot that defect is attached to above casting or side occur Structure.
Finally it should be noted that:Obviously, above-described embodiment is only intended to clearly illustrate the utility model example, And the restriction not to embodiment.For those of ordinary skill in the field, may be used also on the basis of the above description To make other changes in different forms.There is no necessity and possibility to exhaust all the enbodiments.And thus Among the obvious changes or variations amplified out is still in the scope of protection of the utility model.

Claims (1)

1. the fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings, it is characterised in that including aviation casing casting body, There is spherical feeding insulated feeder above aviation casing casting body;Spherical feeding insulated feeder top is spherical, bottom is to be inverted Pyramidal structure, spherical feeding insulated feeder internal layer are that titanium dioxide silica brick internal layer rising head, centre are that alumina silicate heat-insulation layer, outer layer are outer Layer mold;Funnel shaped casting nozzle is connected above spherical feeding insulated feeder.
CN201720529689.6U 2017-05-13 2017-05-13 The fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings Active CN206732060U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720529689.6U CN206732060U (en) 2017-05-13 2017-05-13 The fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720529689.6U CN206732060U (en) 2017-05-13 2017-05-13 The fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings

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CN206732060U true CN206732060U (en) 2017-12-12

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7240578B1 (en) 2022-03-24 2023-03-16 有限会社ファンドリーテック・コンサルティング Riser with high hot water supply efficiency and casting method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7240578B1 (en) 2022-03-24 2023-03-16 有限会社ファンドリーテック・コンサルティング Riser with high hot water supply efficiency and casting method
JP2023143573A (en) * 2022-03-24 2023-10-06 有限会社ファンドリーテック・コンサルティング Riser and casting method having high molten metal feed efficiency

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