CN202158810U - Synchronous disassembling die for shell fuse and fuse seat ring - Google Patents
Synchronous disassembling die for shell fuse and fuse seat ring Download PDFInfo
- Publication number
- CN202158810U CN202158810U CN2011202026050U CN201120202605U CN202158810U CN 202158810 U CN202158810 U CN 202158810U CN 2011202026050 U CN2011202026050 U CN 2011202026050U CN 201120202605 U CN201120202605 U CN 201120202605U CN 202158810 U CN202158810 U CN 202158810U
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- Prior art keywords
- seat ring
- fuse
- fuse seat
- fixture
- dismantled
- 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
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- 230000001360 synchronised effect Effects 0.000 title abstract 2
- 230000004308 accommodation Effects 0.000 claims abstract description 6
- 230000007246 mechanism Effects 0.000 claims description 8
- 238000005728 strengthening Methods 0.000 claims 1
- 235000011464 Pachycereus pringlei Nutrition 0.000 description 3
- 240000006939 Pachycereus weberi Species 0.000 description 3
- 235000011466 Pachycereus weberi Nutrition 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 239000003721 gunpowder Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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Abstract
The utility model discloses a synchronous dismantlement mould of shell fuse and fuse seat ring, this shell has installed a fuse device of compriseing fuse body and fuse seat ring in the front end, this dismantlement mould mainly sets up fixing device on dismounting device, and dismounting device is equipped with an accommodation space that supplies fuse body holding, when the fuse body puts into the accommodation space, the fixed part of establishing on the fixing device can be with the constant head tank reciprocal anchorage on the fuse seat ring, accomplish fixed back then rotate the dismantlement mould, at this moment, utilize the reciprocal anchorage of fixed part and constant head tank, make fuse seat ring dismantled and take off and then be demolishd simultaneously under the influence that does not receive any angular rotation state with its fuse body that is connected, dismantle because of direct to fuse seat ring, the event can effectively avoid touching the fuse body, and then reduce the danger of detonating by a wide margin.
Description
Technical field
The utility model relates to a kind of projectile fuze dismounting mould, relate in particular to a kind of can fast Demolition, safe and avoid fuze stock to have the projectile fuze of any rotation and fuse seat ring to dismantle mould synchronously.
Background technology
Shell in the past must have fuse, gunpowder and the fire in a stove before fuel is added can make shell pull the trigger ejaculation and blast smoothly; But when shell does not use all the year round; Then can make situation such as fuse corrosion, gunpowder humidity, shell must be destroyed or equipment that will can't use is dismantled again and reformed because of making moist, but because shell has high risk; If unloading process very causes blast so that casualties easily because of misoperation; Fuse with two-part is an example, because of long-term not use can make the part corrosion of fuse thread and then the degree of difficulty of increase personnel in the operation of dismounting fuse.
Therefore, how to solve the problem that above-mentioned shell is dismantled dangerous property, be always the relevant industries personnel the anxious key of waiting to study improvement.
Summary of the invention
Problem to shell dismounting high risk; The utility model provides a kind of projectile fuze and fuse seat ring to dismantle mould synchronously, utilizes interfixing of fixed part and locating slot, the fuse seat ring is disassembled takes off; The fuze stock that is connected on the fuse seat ring does not then receive any angle rotation influence and directly dismounting; Can effectively avoid touching fuze stock because of directly dismantling to the fuse seat ring,, thus the danger of igniting significantly reduced.
For realizing above-mentioned purpose; The technical scheme that the utility model adopts is: the shell front end is equiped with a fuze mechanism of being made up of fuze stock and fuse seat ring; This dismounting mould comprises: provision for disengagement; This provision for disengagement is provided with one and supplies the ccontaining accommodation space of above-mentioned fuze stock, and provision for disengagement is connected with fixture, and fixture is provided with at least one and supplies the fixing fixed part of locating slot on the fuse seat ring.
The beneficial effect of the utility model is: this provision for disengagement simple structure, be easy to the assembling, building block is a changeable type; During dismounting fuse seat ring, fuze stock can not produce displacement, and therefore the security of dismounting is higher; Can effectively improve the processing safety and the operating efficiency of projectile fuze dismounting.
Description of drawings
Fig. 1 is the schematic perspective view of the utility model embodiment 1;
Fig. 2 is the generalized section of the utility model embodiment 1;
Fig. 3 is that cardon is made in the assembling of the utility model embodiment 1;
Fig. 4 is that cardon is made in the rotation of the utility model embodiment 1;
Fig. 5 is that cardon is made in the dismounting of the utility model embodiment 1;
Fig. 6 is the structure assembling sketch map of the utility model embodiment 2;
Fig. 7 is the structure assembling sketch map of the utility model embodiment 3;
Fig. 8 is one of planar gesture sketch map of the utility model embodiment 3;
Fig. 9 be the utility model embodiment 3 the planar gesture sketch map two;
Among the figure: 1 shell, 10 fuze mechanisms, 102 fuze stocks, 104 fuse seat rings, 1040 locating slots, 2 dismounting moulds, 20 provisions for disengagement; 202 accommodation spaces, 204 first connect the hole, 22 fixtures, 220 fixed parts, 222 perforatings, 224 second connect the hole, 226 inner ring bodies; 2260 perforation, 2262 slotted eyes, 228 outer ring bodies, 2280 pushing portions, 2282 inclined-planes, 2284 plug the hole; 3 first connectors, 4 second connectors, 5 Fixed latches, 6 latches, 60 springs, 7 keepers.
The specific embodiment
Below in conjunction with accompanying drawing and embodiment the utility model is further specified.
Embodiment 1:
Like Fig. 1, shown in Figure 2; Projectile fuze that the utility model provides and fuse seat ring are dismantled mould synchronously; Shell 1 is equiped with the fuze mechanism 10 be made up of fuze stock 102 and fuse seat ring 104 in front end; This dismounting mould 2 comprises: a provision for disengagement 20, provision for disengagement 20 are provided with one and supply the ccontaining accommodation space 202 of fuze stock 102, and provision for disengagement 20 is connected with a fixture 22; Fixture 22 is provided with at least one fixed part 220 that supplies the locating slot 1040 on the fuse seat ring 104 to fix, and fixture 22 is provided with the perforating 222 that wears in order to the Fixed latches 5 with fixed fuse seat ring 104 more than in addition.Utilize this fixture 22 directly to dismantle to fuse seat ring 104; The fuze stock 102 that is connected on the fuse seat ring 104 does not then receive any angle rotation influence and directly dismounting; Effectively avoiding touching fuze stock 102, and then significantly reduce the danger of igniting.
Like Fig. 3, Fig. 4 and shown in Figure 5; Dismounting mould 2 is made of one piece for provision for disengagement 20 and fixture 22; The fixed part 220 that is provided with on the fixture 22 is in order to can effectively locate the usefulness of the locating slot 1040 on the fuse seat ring 104 when dismounting mould 2 carries out sheathed fuze stock 102 and fixed fuse seat ring 104; In addition; Perforating 222 on the fixture 22 is more than the odd number, Fixed latches 5 is set in the hole wears, but Fixed latches 5 can adopt spring positioning ball, any elasticity or fixture; And utilize the Fixed latches 5 that perforating 222 is installed additional that fixture 22 is fixed with fuse seat ring 104 effectively, come off to prevent to rotate time dismounting mould 2 and fuze mechanism 10.
Behind fixture 22 fixed positions; Then,, therefore utilize this fixture 22 directly to dismantle to fuse seat ring 104 because the fuze stock 102 on the fuze mechanism 10 is interconnective with fuse seat ring 104 to provision for disengagement 20 application of forces and rotation; The fuze stock 102 that is connected on the fuse seat ring 104 does not then receive any angle rotation influence and directly dismounting; Therefore through the engaging of fixture 22 and fuse seat ring 104, can not only take off fuze mechanism 10 fast, more can significantly promote the security of removal efficiency and unloading process; To avoid touching fuze stock 102, reduce the danger of igniting.
Embodiment 2:
The provision for disengagement 20 of dismounting mould 2 constitutes with the mode of fixture 22 utilization assemblings; As shown in Figure 6; This assembling mode is to utilize more than one first connecting piece 3 to be inserted in first in the provision for disengagement 20 to connect second of hole 204 and fixture 22 and connect hole 224 and connect provision for disengagement 20 and fixture 22 to strengthen, and with more than one second connector 4 to connect fixedly provision for disengagement 20 and fixture 22.Utilize aforementioned manner; When provision for disengagement 20 was rotated, provision for disengagement 20 and fixture 22 can produce great torsion, therefore through first connector, 3 ability efficient hardening provision for disengagement 20 and fixtures 22; Avoid separating or loosening because of the relation of torsion; In addition, through second connector 4 provision for disengagement 20 and fixture 22 are locked each other again, in order to strengthen the locking effect.
Provision for disengagement 20 is connected with fixture 22 with second connector 4 through first connector 3; Again that fixture 22 is fixing and locate mutually with fuse seat ring 104; Through fixture 22 the fuse seat ring is unloaded; With the dismounting of completion fuse seat ring 104, and let fuze stock 102 not receive the purpose that any angle is rotated to be influenced and can directly remove, and the parts of inner consume are changeable type.
Embodiment 3:
Like Fig. 7, Fig. 8 and shown in Figure 9, fixture 22 is divided into inner ring body 226 and outer ring body 228, and wherein inner ring body 226 outer walls are provided with more than one and bore a hole 2260; Supply the latch 6 of a tool spring 60 to insert respectively; And utilize this latch 6 to be fixed in fuse seat ring 104, and outer ring body 228 inwalls are provided with corresponding with each latch 6 and supply to push the pushing portion 2280 of this latch 6, because pushing portion 2280 is provided with an inclined-plane 2282; Can supply latch 6 to move; In addition, the outer ring body 228 set holes 2284 that plug are one of them slotted eyes 2262 that forms corresponding to inner ring body 226, and then positioning piece 7 is inserted into one of them slotted eye 2262 by plugging hole 2284.
When carrying out the disarm device; The latch 6 of one tool spring 60 is inserted inner ring body 226, again inner ring body 226 is connected the back with outer ring body 228 and is fixed in the provision for disengagement 20, after the assembling of completion dismounting mould 2 through first connector 3 and second connector 4; Can inner ring body 226 be positioned fuse seat ring place; At this moment, rotate outer ring body 228, have the pushing portion 2280 on inclined-plane 2282 through outer ring body 228 inwalls; And utilize the conflict of inclined-plane 2282 and latch 6 and then promote latch 6; Through latch 6 fuse seat ring and inner ring body 226 are fixed, and when rotating outer ring body 228, utilize the keepers 7 that plug in the hole 2284 according to each slotted eye 2262 in the inner ring body 226 to realize outer ring body 228 and inner ring body 226 postrotational fixed-site; Can reach through inner ring body 226 and outer ring body 228 and to take off fuze mechanism fast, more can significantly promote removal efficiency and unloading process security.
The above is merely the preferred embodiment of the utility model; Non-so promptly limit to the claim of the utility model; So use simple and easy for it modification of institute of the utility model specification and graphic content and equivalent structure to change such as; All should in like manner be contained in the claim of the utility model, close and give Chen Ming.
Claims (10)
1. projectile fuze and fuse seat ring are dismantled mould synchronously; It is characterized in that: the shell front end is equiped with a fuze mechanism of being made up of fuze stock and fuse seat ring; This dismounting mould comprises: provision for disengagement; This provision for disengagement is provided with one and supplies the ccontaining accommodation space of above-mentioned fuze stock, and provision for disengagement is connected with fixture, and fixture is provided with at least one and supplies the fixing fixed part of locating slot on the fuse seat ring.
2. projectile fuze according to claim 1 and fuse seat ring are dismantled mould synchronously, it is characterized in that described dismounting mould comprises first connector of strengthening provision for disengagement and fixture position more than one.
3. projectile fuze according to claim 1 and fuse seat ring are dismantled mould synchronously, it is characterized in that described dismounting mould comprises second connector that connects fixedly provision for disengagement and fixture more than.
4. projectile fuze according to claim 2 and fuse seat ring are dismantled mould synchronously, it is characterized in that this connector is a latch.
5. projectile fuze according to claim 3 and fuse seat ring are dismantled mould synchronously, it is characterized in that this connector is a bolt.
6. projectile fuze according to claim 1 and fuse seat ring are dismantled mould synchronously, it is characterized in that described fixture is provided with the perforating that the Fixed latches of an above fixed fuse seat ring wears.
7. projectile fuze according to claim 1 and fuse seat ring are dismantled mould synchronously; It is characterized in that described fixture comprises an inner ring body and an outer ring body; The inner ring body outer wall is provided with that the latch that supplies a tool spring more than is respectively inserted and the perforation of fixed fuse seat ring, and the outer ring body inwall is provided with corresponding with each latch and supplies to push the pushing portion of latch.
8. projectile fuze according to claim 7 and fuse seat ring are dismantled mould synchronously, it is characterized in that described inner ring body is provided with an above slotted eye.
9. projectile fuze according to claim 7 and fuse seat ring are dismantled mould synchronously, it is characterized in that described outer ring body is provided with one and supplies the hole that plugs that a keeper plugs.
10. projectile fuze according to claim 7 and fuse seat ring are dismantled mould synchronously, it is characterized in that described pushing portion is provided with an inclined-plane that supplies latch to move.
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW100206934U TWM415290U (en) | 2011-04-20 | 2011-04-20 | Ammunition fuze and fuze ring synchronous disassembly mold |
| TW100206934 | 2011-04-20 | ||
| TW100113668A TW201243269A (en) | 2011-04-20 | 2011-04-20 | Jig for simultaneously removing shell fuze and fuze seat ring |
| TW100113668 | 2011-04-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202158810U true CN202158810U (en) | 2012-03-07 |
Family
ID=44777938
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011202026050U Expired - Fee Related CN202158810U (en) | 2011-04-20 | 2011-06-16 | Synchronous disassembling die for shell fuse and fuse seat ring |
| CN2011101615724A Pending CN102221313A (en) | 2011-04-20 | 2011-06-16 | Synchronous disassembling die for shell fuse and fuse seat ring |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011101615724A Pending CN102221313A (en) | 2011-04-20 | 2011-06-16 | Synchronous disassembling die for shell fuse and fuse seat ring |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN202158810U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102221313A (en) * | 2011-04-20 | 2011-10-19 | 崔修武 | Synchronous disassembling die for shell fuse and fuse seat ring |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103776316B (en) * | 2014-01-18 | 2015-08-19 | 尹晓春 | Projectile fuze revolves the equipment of unloading and revolves discharging method |
| CN104482818B (en) * | 2014-11-24 | 2016-06-29 | 河南中南工业有限责任公司 | A kind of medium caliber shell disassembles production line automatically |
| CN107310124B (en) * | 2017-08-18 | 2023-09-05 | 苏州爱得华塑化有限公司 | Quick assembly disassembly's cable material mould |
| CN107322901B (en) * | 2017-08-18 | 2023-09-08 | 苏州爱得华塑化有限公司 | Cable material mould capable of being quickly disassembled and assembled |
| CN113607009B (en) * | 2021-06-30 | 2023-05-09 | 湖南云箭集团有限公司 | Spanner structure for side direction dismounting ammunition fuze |
| CN114322681B (en) * | 2021-12-13 | 2023-06-02 | 中铁十九局集团轨道交通工程有限公司 | Fuse intercepting device convenient to operate |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL3174C (en) * | 1914-07-30 | |||
| JP2658713B2 (en) * | 1991-04-30 | 1997-09-30 | ダイキン工業株式会社 | Temperature switch for high-speed flying objects |
| TWM379752U (en) * | 2009-07-10 | 2010-05-01 | xiu-wu Cui | Mold for detaching shell detonator and device for preventing detonator seat ring from being peeled off |
| CN202158810U (en) * | 2011-04-20 | 2012-03-07 | 崔修武 | Synchronous disassembling die for shell fuse and fuse seat ring |
-
2011
- 2011-06-16 CN CN2011202026050U patent/CN202158810U/en not_active Expired - Fee Related
- 2011-06-16 CN CN2011101615724A patent/CN102221313A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102221313A (en) * | 2011-04-20 | 2011-10-19 | 崔修武 | Synchronous disassembling die for shell fuse and fuse seat ring |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102221313A (en) | 2011-10-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120307 Termination date: 20120616 |