CN104827616A - Spherical fragment bonding molding die - Google Patents
Spherical fragment bonding molding die Download PDFInfo
- Publication number
- CN104827616A CN104827616A CN201510219065.XA CN201510219065A CN104827616A CN 104827616 A CN104827616 A CN 104827616A CN 201510219065 A CN201510219065 A CN 201510219065A CN 104827616 A CN104827616 A CN 104827616A
- Authority
- CN
- China
- Prior art keywords
- die
- screwed hole
- fragmentation
- uniform
- cylinder
- 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
Links
- 238000000465 moulding Methods 0.000 title abstract description 8
- 239000012634 fragment Substances 0.000 title abstract description 5
- 238000013467 fragmentation Methods 0.000 claims description 57
- 238000006062 fragmentation reaction Methods 0.000 claims description 57
- 238000000034 method Methods 0.000 abstract description 12
- 239000003292 glue Substances 0.000 abstract description 11
- 238000007493 shaping process Methods 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000002360 explosive Substances 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 238000003032 molecular docking Methods 0.000 description 2
- 230000003746 surface roughness Effects 0.000 description 2
- 239000004372 Polyvinyl alcohol Substances 0.000 description 1
- 229910001080 W alloy Inorganic materials 0.000 description 1
- 230000003471 anti-radiation Effects 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920002451 polyvinyl alcohol Polymers 0.000 description 1
- 239000005336 safety glass Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
Landscapes
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Abstract
The invention discloses a spherical fragment bonding molding die. The die comprises a glue pouring opening cover plate, a wrapping barrel, a female die and a male die, the wrapping barrel is a cylinder, the upper end surface and the lower end surface of the cylinder are respectively provided with circumferentially uniformly distributed screw holes, the upper end surface of the wrapping barrel is connected with the female die through an inner hexagonal screw, and the lower end surface of the wrapping barrel is connected with the male die through an inner hexagonal screw; the male die is a shell structure, the upper surface of the shell structure is a paraboloid, the lower surface of the shell structure is a conical surface, the edge of the male die is provided with a ring of an outer flange, and the outer flange is provided with uniformly distributed screw holes and uniformly distributed circular through holes; the female die is a shell structure provided with a central circular through hole, and the lower surface of the female die is a paraboloid; and the inner flange of the female die is connected with the glue pouring opening cover plate through an inner hexagonal screw, the glues pouring opening cover plate is a circular plate with a central circular boss, the circumference of the glue pouring opening cover plate is provided with uniformly distributed circular through holes and uniformly distributed screw holes, and the height of the circular boss is same to the thickness of the inner flange of the female die. The die optimizes the fragment bonding molding process, and effectively improves the fragment bonding molding quality.
Description
Technical field
The invention belongs to warhead parts-moulding technical field, relate to a kind of bonding forming mould, particularly a kind of fragmentation bonding forming device.
Background technology
The element of fragmentation artillery warhead is explosive and fragmentation, after explosive charge, fragmentation is driven to obtain very high speed, high speed fragments directly clashes into target, rely on fragmentation Kinetic Energy Kill target, the advantage such as have that density is large, speed is high due to fragmentation and armor-penetrating ability is strong, therefore, by increasingly extensive be used as antipersonnel ammunition kill and wound element, the fragmentation artillery warhead field such as to kill and wound in air defense, antiradiation, face has a wide range of applications.Fragmentation can target kill and fragmentation shape and arrangement mode closely related, therefore, the application technology of fragmentation is the key technology of design fragmentation artillery warhead.
At present, spherical fragmentation is applied in warhead mainly through the mode of bonding forming, the people such as Wang Yingchun are at the document experimental study of high density tungsten alloy brokenness " under the explosively loading condition " (Arms Material scientific and engineering, in January, 2003,26th volume the 1st phase 40 pages) in report a kind of fragmentation adhesive moulding technique, after tungsten fragmentation, metal dust are mixed in preset shaping mould with adhesive, sinter molding in stove.Following problem is there is in the method in bonding fragmentation process:
(1) after fragmentation has been arranged in mould, when the upper port place encapsulating of mould, because the stickiness of glue is comparatively large, is easy to block in port, the air between fragmentation and dies cavity cannot be got rid of, make fragmentation cannot bonding forming.
(2), after fragmentation sinter molding, fragmentation and firm the bonding together of mould, for mould and fragmentation mask work bring inconvenience, molded fragmentation module is easily torn by forced demoulding.
Summary of the invention
In order to overcome shortcomings and deficiencies of the prior art, the invention provides a kind of fragmentation adhesive mould possessing exhaust and demoulding functions, the quality of fragmentation bonding forming can be ensured, and in knockout course, guarantee the integrality of shaping fragmentation.
Spherical fragmentation bonding forming mould provided by the invention, comprise soket head cap screw, encapsulating velar plate, enclose cylinder and punch, it is characterized in that, also comprise die, the described cylinder that encloses is cylinder, the upper and lower end face of cylindrical shell is all processed with the uniform screwed hole of circumference, and the upper surface of enclosing cylinder is connected with die by soket head cap screw, and the lower surface of enclosing cylinder is connected with punch by soket head cap screw; Punch is shell structure, and upper surface is parabola, and lower surface is taper seat, and the edge of punch, with a circle outward flange, outward flange is processed with uniform screwed hole and uniform manhole; Die is the shell structure with central circular through hole, upper surface is taper seat, lower surface is parabola, the edge of die is with a circle outward flange, outward flange is processed with uniform screwed hole and uniform manhole, manhole place, with a circle inner flange, inner flange is processed with uniform screwed hole; The inner flange of die is connected with encapsulating velar plate by soket head cap screw, and encapsulating velar plate is the plectane with central circular boss, is processed with uniform manhole and uniform screwed hole along its circumference, and the height of round boss is identical with the inner flange thickness of die.
The screwed hole of described die is positioned at the outer edge place of inner flange.The screwed hole of described die, the screwed hole of punch and the screwed hole enclosing a upper and lower end face are identical nominal diameter and pitch.Described die is equal with punch wall thickness, with enclose barrel thick ratio be 1.5 ~ 2:1.
Spherical fragmentation bonding forming mould of the present invention, the technique effect brought is presented as:
(1) be designed with exhaust outlet in the upper end of mould, during encapsulating, the air between fragmentation and dies cavity can be got rid of from exhaust outlet, thus guarantees that the space between fragmentation and fragmentation, between fragmentation and mould is fully filled with glue, ensure that the quality of fragmentation bonding forming.
(2) on mould, demoulding mouth is designed with, when using the demoulding mouth demoulding, mould is by the uniform pulling force of circumference, and mould and fragmentation split displacement can accomplish controllable precise, effectively reduce risk fragmentation integrality being caused to damage, thus guarantee the integrality of shaping fragmentation in knockout course.
Accompanying drawing explanation
Fig. 1 is spherical fragmentation bonding forming mould structure schematic diagram of the present invention.
Fig. 2 is the structural representation of encapsulating velar plate in the present invention.
Fig. 3 is the structural representation of die in the present invention.
Fig. 4 is the structural representation of convex mould of the present invention.
Label in figure represents respectively: 1, soket head cap screw, 2, encapsulating velar plate, 3, die, 4, soket head cap screw, 5, cylinder is enclosed, 6, soket head cap screw, 7, punch, 2-1, manhole, 2-2, round boss, 2-3, screwed hole, 3-1, outward flange, 3-2, manhole, 3-3, screwed hole, 3-4, manhole, 3-5, inner flange, 3-6, screwed hole, 7-1, manhole, 7-2, screwed hole, 7-3, outward flange.
Detailed description of the invention
Below in conjunction with drawings and Examples, the present invention is described in further detail, it should be noted that the present invention is not limited to following specific embodiment, and all equal conversion carried out on technical solution of the present invention basis are all in protection scope of the present invention.
As Figure 1-Figure 4, the present embodiment provides a kind of spherical fragmentation bonding forming mould, comprise encapsulating velar plate 2, soket head cap screw [1,4,6], enclose cylinder 5 and punch 7, it is characterized in that, also comprise die 3, described in enclose cylinder 5 for steel cylinder body, in cylindrical shell, cylinder roughness is no more than 0.8 micron, cylindrical shell inner periphery blackening process, the upper and lower end face of cylindrical shell is respectively processed with the uniform screwed hole of 6 circumferences, the screwed hole of cylindrical shell upper surface is connected with die 3 by soket head cap screw 4, and the screwed hole of cylindrical shell lower end is connected with punch 7 by soket head cap screw 6, punch 7 is steel shell structure, upper surface is parabola, lower surface is taper seat, upper surface roughness is no more than 0.8 micron, upper surface blackening process, the parabola size of upper surface is determined according to the docking shape of warhead, and the edge of punch 7 is welded with a circle outward flange 7-3, outward flange 7-3 is processed with 6 uniform screwed hole 7-2 and 6 uniform manhole 7-1, screwed hole 7-2 and manhole 7-1 be distributed in the circumferentially same of outward flange 7-3 and also position interlaced, die 3 is the safety glass shell structure with central circular through hole 3-4, upper surface is taper seat, lower surface is parabola, parabola size is determined according to the docking shape of warhead, lower surface roughness is no more than 0.8 micron, lower surface blackening process, the edge of die 3 is welded with a circle outward flange 3-1, outward flange 3-1 is processed with 6 uniform screwed hole 3-6 and 6 uniform manhole 3-2, screwed hole 3-6 and manhole 3-2 be distributed in the circumferentially same of outward flange 3-1 and also position interlaced, manhole 3-4 place is welded with a circle inner flange 3-5, inner flange 3-5 is processed with 4 uniform screwed hole 3-3, the inner flange 3-5 of die 3 is connected with encapsulating velar plate 2 by soket head cap screw 1, encapsulating velar plate 2 is the steel plectane with central circular boss 2-2, along its circumference be processed with 4 uniform manhole 2-1 and 4 uniform screwed hole 2-3, screwed hole 2-3 and manhole 2-1 be distributed in the circumferentially same of encapsulating velar plate 2 and also position interlaced, the height of central circular boss 2-2 is equal with the inner flange 3-5 thickness of die 3.
In the present embodiment, the screwed hole 3-3 of die 3 is positioned at the outer edge place of inner flange 3-5.
The nominal diameter of the screwed hole 3-6 of described die 3, the screwed hole 7-2 of punch 7 and the screwed hole that encloses cylinder 5 upper and lower end face is M10, and pitch is 1.5mm's.
The nominal diameter of the screwed hole 2-3 of described encapsulating velar plate 2 is M6, and pitch is 1mm's.
Described screwed hole 3-3, screwed hole 3-6, screwed hole 7-2 and screwed hole 2-3 are tapped through hole.
Described die 3 is equal with punch 7 wall thickness, with enclose cylinder 5 wall thickness ratio be 2:1.
Using method of the present invention and operation principle as follows: be stained with the thin plastic paper of a circle at the inner periphery glue enclosing cylinder 5, one deck releasing agent (polyvinyl alcohol releasing agent) is scribbled uniformly at punch 7 upper surface, by soket head cap screw 6 by punch 7 with enclose cylinder 5 and be linked and packed, one deck releasing agent is scribbled uniformly at die 3 lower surface, by soket head cap screw 4 by die 3 with enclose cylinder 5 and be linked and packed, fragmentation is put into mould cavity from the manhole 3-4 of die 3, fragmentation is after the arrangement of cavities of mould completes, encapsulating (3105# mould is with adding thermosetting cement) from the manhole 3-4 of die 3, in the process that glue down oozes in mould cavity, air in mould cavity is discharged from the screwed hole 3-3 of die 3, even if manhole 3-4 is blocked during encapsulating, air in mould cavity by the inwall of die 3 and screwed hole 3-3 also with extraneous UNICOM, and die 3 is transparent, in encapsulating process, the mobility status of glue glue in a mold can be seen, the bonding forming quality of fragmentation can be guaranteed, also the efficiency of encapsulating can be improved.After encapsulating completes, by soket head cap screw 1, encapsulating velar plate 2 and die 3 are linked and packed.Mould is put into baking oven, and temperature is adjusted to 70 DEG C, is dried to 24 hours.After fragmentation bonding forming, dismantle 4 soket head cap screws 1, soket head cap screw 1 is screwed in the screwed hole 2-3 of encapsulating velar plate 2, after 4 soket head cap screws 1 hold out against with die 3, 4 soket head cap screws are twisted with synchronous also the continuation slowly of identical angular speed, simultaneously, cover plate 2 can be subject to the pulling force separated with die 3 upwards, the pulling force be subject to due to cover plate 2 is that circumference is uniform, mould and fragmentation separating distance are screwed into angle by soket head cap screw 1 and can accomplish controllable precise, therefore, can effectively reduce risk fragmentation integrality being caused to damage, thus guarantee the integrality of shaping fragmentation in knockout course.Use identical method respectively by punch 7 and die 3 with enclose cylinder 5 and be separated, the upper and lower surface dimensional accuracy being separated aftershaping fragmentation can be very high, when assembling with explosive assembly casing, can meet instructions for use.
Spherical fragmentation bonding forming mould of the present invention, can guarantee that the space between fragmentation and fragmentation, between fragmentation and mould is fully filled with glue, ensure the quality of fragmentation bonding forming, and mould can accomplish controllable precise with being separated of fragmentation in knockout course, effectively reduce risk fragmentation integrality being caused to damage, guarantee the integrality of shaping fragmentation.
Claims (3)
1. a spherical fragmentation bonding forming mould, comprise soket head cap screw (1,4,6), encapsulating velar plate (2), enclose cylinder (5) and punch (7), it is characterized in that, also comprise die (3), the described cylinder (5) that encloses is cylinder, the annular end face up and down of cylindrical shell is all processed with the uniform screwed hole of circumference, the upper surface of enclosing cylinder (5) is connected with die (3) by soket head cap screw (4), and the lower surface of enclosing cylinder (5) is connected with punch (7) by soket head cap screw (6); Punch (7) is shell structure, upper surface is parabola, lower surface is taper seat, the edge of punch (7), with circle outward flange (7-3), outward flange (7-3) is processed with uniform screwed hole (7-2) and uniform manhole (7-1); Die (3) is the shell structure with central circular through hole (3-4), upper surface is taper seat, lower surface is parabola, the edge of die (3) is with circle outward flange (3-1), outward flange (3-1) is processed with uniform screwed hole (3-6) and uniform manhole (3-2), manhole (3-4) place, with circle inner flange (3-5), inner flange (3-5) is processed with uniform screwed hole (3-3); The inner flange (3-5) of die (3) is connected with encapsulating velar plate (2) by soket head cap screw (1), encapsulating velar plate (2) is the plectane with central circular boss (2-2), be processed with uniform manhole (2-1) and uniform screwed hole (2-3) along its circumference, the height of round boss (2-2) is identical with inner flange (3-5) thickness of die (3).
2. a kind of spherical fragmentation bonding forming mould as claimed in claim 1, it is characterized in that, the screwed hole (3-3) of described die (3) is positioned at the outer edge place of inner flange (3-5).
3. a kind of spherical fragmentation bonding forming mould as claimed in claim 1, it is characterized in that, described die (3) is equal with punch (7) wall thickness, die (3) with enclose cylinder (5) wall thickness ratio be 1.5 ~ 2:1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510219065.XA CN104827616B (en) | 2015-04-30 | 2015-04-30 | Spherical fragment bonding molding die |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510219065.XA CN104827616B (en) | 2015-04-30 | 2015-04-30 | Spherical fragment bonding molding die |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104827616A true CN104827616A (en) | 2015-08-12 |
| CN104827616B CN104827616B (en) | 2017-01-18 |
Family
ID=53805983
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510219065.XA Expired - Fee Related CN104827616B (en) | 2015-04-30 | 2015-04-30 | Spherical fragment bonding molding die |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104827616B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112393649A (en) * | 2020-09-17 | 2021-02-23 | 河南北方红阳机电有限公司 | Modular assembly method for spherical prefabricated fragment of ammunition warhead |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1816554A1 (en) * | 1967-12-29 | 1969-07-24 | Goodyear Tire & Rubber | Process for the production of shaped articles |
| CN101480826A (en) * | 2009-02-13 | 2009-07-15 | 中国西电电气股份有限公司 | Insulating basin casting mould structure and demoulding method |
| CN102729379A (en) * | 2012-07-19 | 2012-10-17 | 山东安博机械科技股份有限公司 | Manufacture method of polyurethane bearing |
| CN203077524U (en) * | 2012-12-12 | 2013-07-24 | 中国西电电气股份有限公司 | Mould for epoxy basin-type insulator for GIS (Geographic Information System) |
-
2015
- 2015-04-30 CN CN201510219065.XA patent/CN104827616B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1816554A1 (en) * | 1967-12-29 | 1969-07-24 | Goodyear Tire & Rubber | Process for the production of shaped articles |
| CN101480826A (en) * | 2009-02-13 | 2009-07-15 | 中国西电电气股份有限公司 | Insulating basin casting mould structure and demoulding method |
| CN102729379A (en) * | 2012-07-19 | 2012-10-17 | 山东安博机械科技股份有限公司 | Manufacture method of polyurethane bearing |
| CN203077524U (en) * | 2012-12-12 | 2013-07-24 | 中国西电电气股份有限公司 | Mould for epoxy basin-type insulator for GIS (Geographic Information System) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112393649A (en) * | 2020-09-17 | 2021-02-23 | 河南北方红阳机电有限公司 | Modular assembly method for spherical prefabricated fragment of ammunition warhead |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104827616B (en) | 2017-01-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204060970U (en) | A kind of multiple belt carcass cast deformation charge device admittedly pushing away motor for minor diameter | |
| CN109438143B (en) | Reverse casting cladding mould | |
| CN213033614U (en) | Sealing disc mechanism of pipe casting die | |
| CN109400425B (en) | Reverse casting die utensil of coating | |
| CN104827616A (en) | Spherical fragment bonding molding die | |
| CN107695238A (en) | Lid manufacturing process and device on heavy rocket engine negative angle collector | |
| CN110792528B (en) | A kind of multi-ring groove medicine type structure forming combined core mold and process | |
| CN208195328U (en) | Turnup pipe makes tooling | |
| CN202592635U (en) | Positioning device for die embedding piece | |
| CN203061876U (en) | Hot-press sintering die with inner lining | |
| CN115837456B (en) | Thin-wall rotary part casting device and method based on aluminum alloy material | |
| CN203062932U (en) | Vacuum hot-pressing combined die | |
| CN207043791U (en) | A kind of clamping device of lathe process thin wall annular outer cover | |
| CN106424718B (en) | A kind of mold and forming method of machine-shaping titanium aluminium base alloy cavity liner | |
| CN205393536U (en) | Tombarthite permanent magnetism radiation ring's hot briquetting mould | |
| CN206573016U (en) | A kind of making mould of monoblock type spontaneous fission modeling firework effect part | |
| CN218425608U (en) | Accurate wall thickness control device for cold isostatic pressing of tube blank | |
| CN203791478U (en) | Combined Haff elbow forming die | |
| CN210098921U (en) | Inner flange die-casting die of flange die-casting forming machine | |
| CN209830221U (en) | Inner mold for centrifugally casting cylinder sleeve | |
| CN207178678U (en) | A kind of elastic component with sealing function | |
| CN202350680U (en) | Overall compression molded bomb tail of civil rocket bomb | |
| CN105945193A (en) | Bearing support body forging die | |
| CN205519034U (en) | Wire rod disconnect -type wire drawing assembling die | |
| CN205096486U (en) | Titanium alloy casting is with graphite core and casting die utensil |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| EXSB | Decision made by sipo to initiate substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170118 Termination date: 20210430 |