CN205270745U - Fire -retardant insulation riser of aviation machine casket magnesium alloy casting - Google Patents

Fire -retardant insulation riser of aviation machine casket magnesium alloy casting Download PDF

Info

Publication number
CN205270745U
CN205270745U CN201520686272.1U CN201520686272U CN205270745U CN 205270745 U CN205270745 U CN 205270745U CN 201520686272 U CN201520686272 U CN 201520686272U CN 205270745 U CN205270745 U CN 205270745U
Authority
CN
China
Prior art keywords
rising head
magnesium oxide
magnesium alloy
aviation machine
machine casket
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201520686272.1U
Other languages
Chinese (zh)
Inventor
杨庭彰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Harbin Futing Chuangfu Machinery Manufacturing Co Ltd
Original Assignee
Harbin Futing Chuangfu Machinery Manufacturing Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Harbin Futing Chuangfu Machinery Manufacturing Co Ltd filed Critical Harbin Futing Chuangfu Machinery Manufacturing Co Ltd
Priority to CN201520686272.1U priority Critical patent/CN205270745U/en
Application granted granted Critical
Publication of CN205270745U publication Critical patent/CN205270745U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model discloses a fire -retardant insulation riser of aviation machine casket magnesium alloy casting relates to metal processing technology field, and the improvement of concretely relates to fire -retardant insulation riser of aviation machine casket magnesium alloy casting structure is technological. Including aviation machine casket foundry goods, there is the rising head above the aviation machine casket foundry goods, be magnesium oxide inlayer rising head in the rising head, magnesium oxide inlayer rising head appearance is the toper of invering, and big, lower little stairstepping hole is gone up to magnesium oxide inlayer rising head hole, there is conical aluminium silicate heat preservation magnesium oxide inlayer rising head outside. The utility model provides a magnesium alloy aviation machine casket during fabrication, when as cast rising head diameter one regularly, highly great, the rising head is out of shape, influences product quality's problem.

Description

Aviation casing magnesium alloy cast fire-retardant heat insulation rising head
Technical field
This utility model relates to metal working technical area, is specifically related to the improvement opportunity of aviation casing magnesium alloy cast fire-retardant heat insulation dead head structure.
Background technology
Magnesium alloy has lightweight, and specific strength and specific stiffness are high, and damping shock absorption is good, capability of electromagnetic shielding and perfect heat-dissipating, the advantages such as casting forming function is excellent, and machining property is good, and therefore magnesium alloy is adapted in specific field application, for instance aviation field. Magnesium alloy is inhaled with its height and is made an uproar ability, good forming processing performance than performance, prominent vibration damping and the feature such as be easily recycled, and is described as the green structural material in 2l century. But the chemical property of magnesium is active, strong with the affinity of oxygen, the oxide-film of densification can not be formed after high-temperature oxydation. Therefore, magnesium alloy is prone to oxidizing fire in melting, liquid forming and heat treatment process, it is desirable to provide effective fire-resisting protection. At high temperature, especially fire-retardant under molten condition is for magnesium and alloy thereof: adopt method physically or chemically, forms effective protection aquiclude on its surface, completely cuts off air on the one hand, stops magnesium evaporation on the one hand, reaches to slow down oxidation, fire-retardant purpose. From the twenties in 20th century, magnesium alloy is just applied at aerospace field.
The aviation casing using magnesium alloy can alleviate weight, improves the mobility of aerospace vehicle, reduce oil consumption, brings considerable economic benefit.
During fabrication, the effect of insulated feeder is the feeding efficiency improving rising head by extending rising head setting time to the aviation casing of magnesium alloy. In Foundry Production, arranging one of rising head important measures being to ensure that casting quality, its Main Function is that foundry goods is carried out feeding. According to modulus calculation, casting alloy typically requires the rising head identical with foundry goods volume to be carried out feeding this means that in Foundry Production the metal of nearly 50 to carry out melting again, improves casting quality and rising head utilization rate. Insulated feeder can be adopted. Insulated feeder is by controlling rising head heat waste, extends riser metal liquid setting time, improves riser supplement shrink efficiency. This is possible not only to save riser metal liquid, and to improving casting quality important in inhibiting. The shape of existing insulated feeder is generally adopted cylindrical and two kinds of forms of kidney-shaped. Owing in casting process, technological parameter is difficult to constant, so the diametric(al) of insulated feeder is reduced to about 0.8 times, highly constant. Owing to insulated feeder and foundry goods volume need certain ratio, so rising head diameter one timing, highly relatively big, rising head deforms, and affects product quality.
Summary of the invention
This utility model provides aviation casing magnesium alloy cast fire-retardant heat insulation rising head, and this utility model solves the aviation casing of magnesium alloy during fabrication, and when rising head diameter one timing of casting, highly relatively big, rising head deforms, the problem affecting product quality.
For solving the problems referred to above, this utility model adopts the following technical scheme that aviation casing magnesium alloy cast fire-retardant heat insulation rising head, including aviation casing foundry goods, has rising head above aviation casing foundry goods; Being magnesium oxide internal layer rising head in rising head, magnesium oxide internal layer rising head profile is inverted taper, and magnesium oxide internal layer rising head endoporus is the stepped bore of upper big, lower small; The aluminium silicate heat-insulation layer of taper is had outside magnesium oxide internal layer rising head.
This utility model advantage: the aviation casing of magnesium alloy is at the cone shape that the insulated feeder cast is ladder, and top major diameter rising head can hold more raw material, and riser height can reduce, convenient manufacture. Rising head adopts aluminium silicate heat-insulation layer, high insulating effect, the constant product quality of production.
Accompanying drawing explanation
Fig. 1 is this utility model structural representation.
Symbol description in figure: aviation casing foundry goods 1, rising head 2, shrinkage cavity 3, aluminium silicate heat-insulation layer 4, magnesium oxide internal layer rising head 5.
Detailed description of the invention
By best embodiment, this utility model is described in detail below��
As it is shown in figure 1, aviation casing magnesium alloy cast fire-retardant heat insulation rising head, including aviation casing foundry goods 1, above aviation casing foundry goods 1, there is rising head 2; Being magnesium oxide internal layer rising head 5 in rising head 2, magnesium oxide internal layer rising head 5 profile is inverted taper, and magnesium oxide internal layer rising head 5 endoporus is the stepped bore of upper big, lower small; The aluminium silicate heat-insulation layer 4 of taper is had outside magnesium oxide internal layer rising head 5. Insulated feeder is the cone shape of ladder, and rising head is formulated according to designing requirement with parts connecting portion diameter, and top major diameter rising head can hold more raw material, and riser height can reduce, and convenient manufactures. The wall thickness of insulated feeder; The wall thickness of insulated feeder is the key factor affecting feeding effect. Too thin moulding difficulty, and heat insulation effect is poor; Too thick that heat insulation effect impact is little, but increase cost, general wall thickness takes the 18-20 of rising head diameter, the thinnest cannot be less than 20mm. Aluminium silicate is with hard paste grog for raw material, is the heat insulating material replacing asbestos, the heatproof of aluminium silicate wool: 800-1200 degree Celsius.
Insulated feeder of the present utility model has following characteristics: 1, have good heat-insulating property; 2, there is good high-temperature flame-proof performance; 3, there is good chemical stability under high temperature; 4, there is enough dry strength, wet strength; 5, use procedure does not produce environmental pollution, meet environmental requirement; 6, cheap, raw material sources is extensively, easily purchase.
Last it is noted that obvious, above-described embodiment is only for clearly demonstrating this utility model example, and is not the restriction to embodiment. For those of ordinary skill in the field, can also make other changes in different forms on the basis of the above description. Here without also cannot all of embodiment be given exhaustive. And the apparent change thus amplified out or variation are still among protection domain of the present utility model.

Claims (1)

1. aviation casing magnesium alloy cast fire-retardant heat insulation rising head, including aviation casing foundry goods, has rising head above aviation casing foundry goods; It is characterized in that, be magnesium oxide internal layer rising head in rising head, magnesium oxide internal layer rising head profile is inverted taper, and magnesium oxide internal layer rising head endoporus is the stepped bore of upper big, lower small; The aluminium silicate heat-insulation layer of taper is had outside magnesium oxide internal layer rising head.
CN201520686272.1U 2015-09-08 2015-09-08 Fire -retardant insulation riser of aviation machine casket magnesium alloy casting Expired - Fee Related CN205270745U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520686272.1U CN205270745U (en) 2015-09-08 2015-09-08 Fire -retardant insulation riser of aviation machine casket magnesium alloy casting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520686272.1U CN205270745U (en) 2015-09-08 2015-09-08 Fire -retardant insulation riser of aviation machine casket magnesium alloy casting

Publications (1)

Publication Number Publication Date
CN205270745U true CN205270745U (en) 2016-06-01

Family

ID=56055366

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520686272.1U Expired - Fee Related CN205270745U (en) 2015-09-08 2015-09-08 Fire -retardant insulation riser of aviation machine casket magnesium alloy casting

Country Status (1)

Country Link
CN (1) CN205270745U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112496279A (en) * 2020-11-13 2021-03-16 攀钢集团攀枝花钢铁研究院有限公司 Ingot feeding method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112496279A (en) * 2020-11-13 2021-03-16 攀钢集团攀枝花钢铁研究院有限公司 Ingot feeding method

Similar Documents

Publication Publication Date Title
CN103624237B (en) A kind of magnesium alloy Anti-gravity casting device and method thereof
CN205270745U (en) Fire -retardant insulation riser of aviation machine casket magnesium alloy casting
CN208772444U (en) A kind of torpedo tank lining structure therewith
CN205254036U (en) Aviation machine casket aluminium alloy casting insulation riser
CN204381298U (en) A kind of casting mold rising head
CN104308097B (en) Improve the ingot mould of ingot quality and utilization rate
CN206464539U (en) A kind of stopper rod of tundish with transition zone
CN104057034A (en) Manufacturing process of integrated gas stove burner
CN103706777B (en) A kind of liquid black metal stamp forging mould and preparation method
CN206732060U (en) The fire-retardant anti-oxidation insulated feeder of aviation casing Mg alloy castings
CN206732059U (en) Aviation casing Mg alloy castings Superstrong heat-preserving fire-retardant heat insulation rising head
CN109732073B (en) Gradient composite tundish nozzle for continuous casting and preparation method thereof
CN206732058U (en) The superpower feeding insulated feeder of aviation casing magnesium alloy casting
CN205020751U (en) Mould of casting subway locomotive bearing cap
CN206912183U (en) It is incubated casting molds rising head
CN104630535A (en) Method for preparing Al/Sip ceramic based composite material
CN209550580U (en) A kind of aluminum alloy low-pressure casting feeding device
CN205702322U (en) A kind of aluminium alloy casting heating device for rising head
CN203928718U (en) A kind of trapezoidal graphite crucible
CN203556668U (en) Extruding cylinder for extruder
CN203556800U (en) Knock-off core for heating feeder head of large-sized steel casting
CN203044832U (en) Aluminum alloy ingot casting hot top multi-mold casting device and insulation structure thereof
CN102886506A (en) Die for improving mechanical property of magnesium alloy casting
CN202824527U (en) Riser for casting mold
CN208667507U (en) A kind of ladle molten bath light thermal-insulation magnesia-alumina-carbon brick

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160601

Termination date: 20210908

CF01 Termination of patent right due to non-payment of annual fee