Nothing Special   »   [go: up one dir, main page]

CN1187398A - Technique for integral casting of stainless steel propeller - Google Patents

Technique for integral casting of stainless steel propeller Download PDF

Info

Publication number
CN1187398A
CN1187398A CN97108262A CN97108262A CN1187398A CN 1187398 A CN1187398 A CN 1187398A CN 97108262 A CN97108262 A CN 97108262A CN 97108262 A CN97108262 A CN 97108262A CN 1187398 A CN1187398 A CN 1187398A
Authority
CN
China
Prior art keywords
sand
clay
casting
sodium silicate
stainless steel
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.)
Granted
Application number
CN97108262A
Other languages
Chinese (zh)
Other versions
CN1063687C (en
Inventor
杨光兴
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN97108262A priority Critical patent/CN1063687C/en
Publication of CN1187398A publication Critical patent/CN1187398A/en
Application granted granted Critical
Publication of CN1063687C publication Critical patent/CN1063687C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Mold Materials And Core Materials (AREA)

Abstract

An integral casting technique for stainless steel propeller technically features that integral casting mould is used, the backing sand is ordinary clay sand, the surfical sand is high bauxite sand, the paint is magnesium sand powder, a composite layer including backing sand, surficial sand and paint is formed during moulding, and open casting system with chosen casting time and temp is used.

Description

Technique for integral casting of stainless steel propeller
The present invention relates to a kind of HACR technique for integral casting of stainless steel propeller.
The general scraper plate that adopts of existing screw propeller casting is made mo(u)ld bottom half in conjunction with pitch plate, meets Ye Duoxiang with the wooden model heart or the sand mo(u)ld heart and makes mo(u)ld top half, because the wooden model heart is made very difficulty, and sand mo(u)ld heart intensity is low, and scale error is big, both cannot say for sure to demonstrate,prove casting quality, and when taking a lot of work again, work efficiency is low.Aspect Modeling Material, general Gao Meng, high-chromium alloy steel casting are made floor sand with quarz sand, make facing sand with magnesia or chromite sand, and these material prices are more expensive, and reuse is relatively poor.Aspect casting system, adopt bottom filling more, every leaf is established a runner gate, and ingate imports along blade plane, and establish chill and lacing wire, core cylinder iron, big rising head, this system's moulding complexity are established in the hub top, the molten steel stroke is long, and temperature is low, easily produces defectives such as misrun, and yield rate only is 60%.New material HACR corrosion-resistant steel (ZL85105573.7) has the few chromium of no nickel, anti-ammonia, alkali, marine corrosion, premium properties such as intensity height, but contain more basic anhydride in its molten steel, scab takes place easily and produce cold shut and surperficial elephant skin, in addition, this steel shrinks big, be easy to generate shrinkage cavity and crackle, thereby the casting difficulty is big.
The object of the present invention is to provide a kind of HACR technique for integral casting of stainless steel propeller.
The present invention be directed to the problem that exists in the casting difficult point of HACR novel stainless steel and the screw propeller foundry technique, worked out and a kind ofly can guarantee casting quality, reduce production costs, can adopt on the whole simultaneously, stove is convenient in the nowel moulding dries, improve the technology of work efficiency, its technological process comprises: make whole mold-sand molding-oven dry-moulding by casting-surface treatment-finished products such as polishing.
The making of whole mold
At first by design calculation secondary processes parameter,, process cover in the iron of propeller hub with the tangent plane plate and the pitch plate of plastic flagstone or the leaf plate of paperboard, each radius; Produce mo(u)ld bottom half with rubbing board, draw line of centers and helix line are completed leaf plate to line, fix each tangent plane plate on leaf plate; Between each tangent plane plate, filling out fast solid filler such as clay, the sodium silicate sand etc. of rapid-curing cutback of energy, repair fairing and become the mould heart, treat to make mo(u)ld top half by leaf after it does admittedly; Unpack to remove the mould heart, cover in the following good iron, mould assembling pour into a mould whole mold blank, this blank is trimmed by the one-time process parameter, and reaches requirement do static balance, whole mold, its material can be steel, aluminium or plastics.
Sand molding
The used floor sand of the present invention is a common clay sand, and facing sand is neutrality or basic matterials such as high-al clay sand, and coating is alkalescence such as magnesia powder material preferably.The facing sand proportioning is: high-al clay sand 100%, and clay 2-10%, sodium silicate 0-15%, moisture content 2-6%, best proportioning is a high-al clay sand 100%, clay 3-5%, sodium silicate 5-8%, moisture content 3-5%.Coating formula is: magnesia powder 100%, and clay 2-8%, sodium silicate or syrup 3-12%, water is an amount of, and best proportioning is a magnesia powder 100%, clay 3-4%, sodium silicate or syrup 5-8%, water is an amount of.During moulding, facing sand and coating are modulated by said ratio, floor sand is put into case and is built reality, at first on the following profile of whole mold, brush the thick facing sand of 10mm and whole mold is put into the common clay sand floor sand, compaction moulding, make it floor sand surface coverage layer of even facing sand, take out whole mold, evenly be coated with again on the facing sand surface and coat, so just make the composite stratotype with common clay sand (floor sand)-high-al clay sand (facing sand)-magnesia powder (coating) composition of propeller mo(u)ld bottom half, according to said method made the composite stratotype of propeller mo(u)ld top half then.
Moulding by casting
The present invention is a unchoked running system, is beneficial to quick cast with big pouring basin.From rising head water inlet, choked flow steadily divides to advance each blade then at the rising head neck, and blade top and leaf locate to set out gas port slightly, consecutive solidification, rising head is with spherical half blind riser, the size of riser neck and highly with the size of watering fluence, adjust, so that the feeding passage is unimpeded.Flow out for the ease of exhaust and slag liquid, offer excessive slag chute with the leaf top slightly at leaf.During cast, the used pouring temperature of the present invention is 1500 ℃-1550 ℃, and be the duration of pouring, and the 300-700Kg molten steel is 8-10 second, and the following molten steel of 300Kg (not comprising 300Kg) is 5 seconds.
Compare with existing propeller foundry engieering, the present invention has following advantage:
1, adopt the whole mold of cover in the iron, mould making process is easier, and is easy to process, and the material-saving that saves time, mold process easily detect and finishing, are convenient to mold itself and reach the balance requirement, thereby can improve casting dimension accuracy;
2, can adopt on the whole, the nowel casting, improved molding process, improve work efficiency more than 5 times;
3, common clay sand (floor sand)-high-al clay sand (facing sand)-magnesia powder (coating) composite stratotype is high temperature resistant, effectively prevents the fusion effect of molten steel to common clay sand, and anti-stick grittiness is good, the Modeling Material cost is low, the old sand reuse is good, and cast(ing) surface is more smooth, and quality is better;
4, the pouring temperature and the time of the present invention's employing are suitable for the HACR corrosion-resistant steel, can effectively prevent the defective of cold shut and elephant skin and the generation of shrinkage cavity and crackle, and yield rate can reach 70-80%.
Embodiment
1, adopts whole aluminum dipping form.
2, Modeling Material.Floor sand-common clay sand; Facing sand proportioning: high-al clay sand 100%, clay 4%, sodium silicate 6%, moisture content 4%; Coating formula: magnesia powder 100%, clay 4%, sodium silicate 7%, water is an amount of.
3, adopt unchoked running system, 1550 ℃ of pouring temperatures, the duration of pouring, the 250Kg molten steel was 5 seconds.

Claims (2)

1, a kind of HACR technique for integral casting of stainless steel propeller, its technological process comprise makes whole mold-sand molding-oven dry-moulding by casting-surface treatment-finished products such as polishing, the invention is characterized in:
1. adopt whole mold;
2. moulding is a common clay sand with the raw MAT'L floor sand, and facing sand is based on high-al clay sand, and coating is based on magnesia powder, and the facing sand proportioning is a high-al clay sand 100%, clay 2-10%, sodium silicate 0-15%, moisture content 2-6%; Coating formula is a magnesia powder 100%, clay 2-8%, and sodium silicate (or syrup) 3-12%, water is an amount of; Form common clay sand (floor sand)-high-al clay sand (facing sand)-magnesia powder (coating) composite stratotype during moulding;
3. adopt unchoked running system, pouring temperature is 1500 ℃-1550 ℃, and be 300Kg-700Kg molten steel 8-10 second the duration of pouring, the following molten steel of 300Kg (not comprising 300Kg) 5 seconds.
2, HACR technique for integral casting of stainless steel propeller according to claim 1, the best proportioning that it is characterized in that facing sand is a high-al clay sand 100%, clay 3-5%, sodium silicate 5-8%, moisture content 3-5%; The best proportioning of coating is a magnesia powder 100%, clay 3-4%, and sodium silicate or syrup 5-8%, water is an amount of.
CN97108262A 1997-10-16 1997-10-16 Technique for integral casting of stainless steel propeller Expired - Fee Related CN1063687C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN97108262A CN1063687C (en) 1997-10-16 1997-10-16 Technique for integral casting of stainless steel propeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN97108262A CN1063687C (en) 1997-10-16 1997-10-16 Technique for integral casting of stainless steel propeller

Publications (2)

Publication Number Publication Date
CN1187398A true CN1187398A (en) 1998-07-15
CN1063687C CN1063687C (en) 2001-03-28

Family

ID=5170274

Family Applications (1)

Application Number Title Priority Date Filing Date
CN97108262A Expired - Fee Related CN1063687C (en) 1997-10-16 1997-10-16 Technique for integral casting of stainless steel propeller

Country Status (1)

Country Link
CN (1) CN1063687C (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101386056B (en) * 2008-10-07 2010-12-08 大连船用推进器有限公司 Tire retreading casting molding method
CN102658342A (en) * 2012-05-03 2012-09-12 黄善送 Rolling machining method for propellers of stainless steel ships
CN104014742A (en) * 2014-05-09 2014-09-03 大连理工大学 Casting process and casting mould of large propeller hub body
CN104030708A (en) * 2014-06-17 2014-09-10 张希君 Precision casting sand and preparation method thereof

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1026471C (en) * 1990-08-07 1994-11-09 宫哲圣 Propeller line skeleton moulding method
EP0721387B1 (en) * 1994-07-27 1999-12-08 Bitzer Kühlmaschinenbau GmbH Method and casting device for producing parts with a helically symmetrical outer contour
CN1140112A (en) * 1996-05-10 1997-01-15 河北省沧州机械厂 Centrifugal casting and moulding technique for screw of screw oil extruder

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101386056B (en) * 2008-10-07 2010-12-08 大连船用推进器有限公司 Tire retreading casting molding method
CN102658342A (en) * 2012-05-03 2012-09-12 黄善送 Rolling machining method for propellers of stainless steel ships
CN104014742A (en) * 2014-05-09 2014-09-03 大连理工大学 Casting process and casting mould of large propeller hub body
CN104030708A (en) * 2014-06-17 2014-09-10 张希君 Precision casting sand and preparation method thereof
CN104030708B (en) * 2014-06-17 2015-12-02 张希君 A kind of precision casting sand and preparation method thereof

Also Published As

Publication number Publication date
CN1063687C (en) 2001-03-28

Similar Documents

Publication Publication Date Title
CN102717032B (en) A precision casting method for automobile turbocharger housing parts
CN104308081B (en) A kind of method for aluminium alloy castings V method moulding anti-gravity pouring
CN105382206B (en) A kind of gear case body casting mold and its forming method
CN102000781A (en) Metal mold sand coating device for casting upper mold of brake drum
CN104190875A (en) Composite casting mold forming method for complex thin-wall casing
CN110153371A (en) Prevent the casting method of spherulitic iron crankshaft shrinkage defect
CN103624220A (en) Production technology of explosion-proof and corrosion-proof motor casing
CN107855467A (en) The model casting system and investment casting method of U-shaped magnesium alloy member
CN118543789B (en) Iron mold covered sand casting structure and manufacturing process of main shaft casting of large wind turbine generator set
CN109773124A (en) Integral casting process of a Francis turbine runner
CN107745081A (en) The differential pressure running gate system and differential pressure pouring procedure of U-shaped magnesium alloy member
CN102825211A (en) Non-occupying coating and application thereof
CN1063687C (en) Technique for integral casting of stainless steel propeller
CN201913186U (en) Metal mold sand coating device for casting lower shape of brake drum
CN102430704B (en) Preparation method for lost foam casting paint
CN104874731A (en) Method for casting large-scale bucket tooth casting by using lost foam
CN118543788B (en) Iron type casting mold structure of main shaft casting of large wind generating set and manufacturing process thereof
CN107398531A (en) The casting technique of high-precision stainless steel body
CN108655342A (en) A kind of preparation facilities and preparation method of environmental protection founding materials
CN106493298A (en) A kind of process for improving lost foam casting Part Surface Roughness
CN113953445B (en) Device and method for producing bidirectional pump impeller by 3DP sand printing technology
CN110052583A (en) Precise casting process of hollow guide blade
CN116329484A (en) Precision casting method for large castings
CN213856955U (en) Wind power hub pouring system
CN1597179A (en) Mould and method for preparation high-pressure switch cast aluminium can

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee