CN102221313A - 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
- CN102221313A CN102221313A CN2011101615724A CN201110161572A CN102221313A CN 102221313 A CN102221313 A CN 102221313A CN 2011101615724 A CN2011101615724 A CN 2011101615724A CN 201110161572 A CN201110161572 A CN 201110161572A CN 102221313 A CN102221313 A CN 102221313A
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- Prior art keywords
- seat ring
- fuze
- fuse seat
- fuse
- fixture
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- 230000001360 synchronised effect Effects 0.000 title abstract 2
- 230000007246 mechanism Effects 0.000 claims description 8
- 230000004308 accommodation Effects 0.000 claims description 4
- 238000005728 strengthening Methods 0.000 claims 1
- 238000005474 detonation Methods 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 4
- 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 invention discloses a synchronous disassembling mould for shell fuze and fuze seat ring, the front end of the shell is provided with a fuze device composed of a fuze body and a fuze seat ring, the disassembling mould is mainly provided with a fixing device on the disassembling device, the disassembling device is provided with an accommodating space for accommodating the fuze body, when the fuze body is arranged in the accommodating space, a fixing part arranged on the fixing device can be mutually fixed with a positioning groove on the fuze seat ring, the disassembling mould is rotated after the fixation is finished, at the moment, the fuze seat ring is disassembled and taken down, the fuze body connected with the fuze seat ring is disassembled at the same time without being influenced by any angle rotation state by utilizing the mutual fixation of the fixing part and the positioning groove, and the fuze seat ring is directly disassembled, so the fuze body can be effectively prevented from being touched, and further the risk of detonation is greatly reduced.
Description
Technical field
The present invention relates to a kind of projectile fuze dismounting mould, relate in particular to a kind ofly can remove fast, 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 situations such as fuse corrosion, gunpowder humidity because of making moist, shell must be destroyed or equipment that will can't use is dismantled again and reformed, but because shell has high risk, if unloading process causes blast because of misoperation is very easy so that casualties, fuse with two-part is an example, the long-term not use of cause 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 at shell dismounting high risk, the invention provides a kind of projectile fuze and the fuse seat ring is dismantled mould synchronously, utilize interfixing of fixed part and locating slot, the fuse seat ring is disassembled to be taken off, the fuze stock that is connected on the fuse seat ring then is not subjected to any angle rotation influence and directly dismounting, can effectively avoid touching fuze stock because of directly dismantling at the fuse seat ring,, thus the danger of igniting significantly reduced.
For achieving the above object, the technical solution used in the present invention 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 a ccontaining accommodation space of the above-mentioned fuze stock of confession, provision for disengagement is connected with fixture, and fixture is provided with at least one for the fixing fixed part of the locating slot on the fuse seat ring.
The invention has the beneficial effects as follows: 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 embodiment of the invention 1;
Fig. 2 is the generalized section of the embodiment of the invention 1;
Fig. 3 is that cardon is made in the assembling of the embodiment of the invention 1;
Fig. 4 is that cardon is made in the rotation of the embodiment of the invention 1;
Fig. 5 is that cardon is made in the dismounting of the embodiment of the invention 1;
Fig. 6 is the structure assembling schematic diagram of the embodiment of the invention 2;
Fig. 7 is the structure assembling schematic diagram of the embodiment of the invention 3;
Fig. 8 is one of planar gesture schematic diagram of the embodiment of the invention 3;
Fig. 9 be the embodiment of the invention 3 the planar gesture schematic diagram 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
The present invention is further described below in conjunction with drawings and Examples.
Embodiment 1:
As Fig. 1, shown in Figure 2, projectile fuze provided by the invention and fuse seat ring are dismantled mould synchronously, shell 1 is equiped with a fuze mechanism 10 of being 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 is provided with one for the ccontaining accommodation space 202 of fuze stock 102, provision for disengagement 20 is connected with a fixture 22, fixture 22 is provided with at least one for the fixed part 220 that the locating slot on the fuse seat ring 104 1040 is fixed, 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 at fuse seat ring 104, the fuze stock 102 that is connected on the fuse seat ring 104 then is not subjected to any angle rotation influence and directly dismounting, effectively avoiding touching fuze stock 102, and then significantly reduce the danger of igniting.
As 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 to wear, Fixed latches 5 can adopt the spring positioning ball, but 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 to provision for disengagement 20 application of forces and rotation, because fuze stock 102 and fuse seat ring 104 on the fuze mechanism 10 are interconnective, therefore utilize this fixture 22 directly to dismantle at fuse seat ring 104, the fuze stock 102 that is connected on the fuse seat ring 104 then is not subjected to any angle rotation influence and directly dismounting, therefore engaging by 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 mode of the provision for disengagement 20 of dismounting mould 2 and fixture 22 utilization assemblings constitutes, 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 be connected and fixed provision for disengagement 20 and fixture 22.Utilize aforementioned manner, when provision for disengagement 20 is rotated, provision for disengagement 20 can produce great torsion with fixture 22, therefore by first connector, 3 energy efficient hardening provision for disengagement 20 and fixtures 22, avoid separating or loosening because of the relation of torsion, in addition, by second connector 4 provision for disengagement 20 and fixture 22 are locked mutually again, in order to strengthen the locking effect.
Provision for disengagement 20 is connected with fixture 22 with second connector 4 by first connector 3, again that fixture 22 is fixing and locate mutually with fuse seat ring 104, by fixture 22 the fuse seat ring is unloaded, to finish the dismounting of fuse seat ring 104, and allow fuze stock 102 not be subjected to 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:
As Fig. 7, Fig. 8 and shown in Figure 9, fixture 22 is divided into inner ring body 226 and outer ring body 228, wherein inner ring body 226 outer walls are provided with more than one and bore a hole 2260, insert for the latch 6 of a tool spring 60 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 for the pushing portion 2280 that pushes this latch 6, because pushing portion 2280 is provided with an inclined-plane 2282, can move for latch 6, 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, inner ring body 226 is connected the back is fixed in the provision for disengagement 20 by first connector 3 and second connector 4 with outer ring body 228 again, after finishing the assembling of dismounting mould 2, inner ring body 226 can be positioned fuse seat ring place, at this moment, rotation outer ring body 228, the pushing portion 2280 that has inclined-plane 2282 by outer ring body 228 inwalls, and utilize the conflict of inclined-plane 2282 and latch 6 and then promote latch 6, by latch 6 fuse seat ring and inner ring body 226 are fixed, and when rotating outer ring body 228, utilization plug keeper 7 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 by 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 only for the present invention's preferred embodiment, non-so promptly limit to the present invention's claim, so use simple and easy for it modification of institute of specification of the present invention and graphic content and equivalent structure to change such as, all should in like manner be contained in the present invention's the claim, 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 a ccontaining accommodation space of the above-mentioned fuze stock of confession, provision for disengagement is connected with fixture, and fixture is provided with at least one for the fixing fixed part of the 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 is connected and fixed 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 more than one inserts for the latch of a tool spring respectively and the perforation of fixed fuse seat ring, and the outer ring body inwall is provided with corresponding with each latch and for the pushing portion that pushes 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 the hole that plugs that keeper of a confession 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 |
---|---|---|---|
TW100113668 | 2011-04-20 | ||
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 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN102221313A true CN102221313A (en) | 2011-10-19 |
Family
ID=44777938
Family Applications (2)
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 |
CN2011202026050U Expired - Fee Related CN202158810U (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 |
---|---|---|---|
CN2011202026050U Expired - Fee Related CN202158810U (en) | 2011-04-20 | 2011-06-16 | Synchronous disassembling die for shell fuse and fuse seat ring |
Country Status (1)
Country | Link |
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CN (2) | CN102221313A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103776316A (en) * | 2014-01-18 | 2014-05-07 | 尹晓春 | Rotary projectile fuse disassembling equipment and rotary disassembling method |
CN104482818A (en) * | 2014-11-24 | 2015-04-01 | 河南中南工业有限责任公司 | Medium-caliber cannonball automatic disassembly production line |
CN107310124A (en) * | 2017-08-18 | 2017-11-03 | 苏州爱得华塑化有限公司 | A kind of CABLE MATERIALS mould of fast assembling-disassembling |
CN107322901A (en) * | 2017-08-18 | 2017-11-07 | 苏州爱得华塑化有限公司 | A kind of CABLE MATERIALS mould of fast demountable |
CN113607009A (en) * | 2021-06-30 | 2021-11-05 | 湖南云箭集团有限公司 | Wrench for disassembling ammunition fuse at side position |
CN114322681A (en) * | 2021-12-13 | 2022-04-12 | 中铁十九局集团轨道交通工程有限公司 | Fuse intercepting device convenient to operate |
Families Citing this family (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 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191418049A (en) * | 1914-07-30 | 1915-06-03 | Eugene Schneider | Improvements in or relating to Double Acting Fuses for Projectiles. |
JPH0594752A (en) * | 1991-04-30 | 1993-04-16 | Daikin Ind Ltd | Temperature switch for high speed flying body |
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 CN2011101615724A patent/CN102221313A/en active Pending
- 2011-06-16 CN CN2011202026050U patent/CN202158810U/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191418049A (en) * | 1914-07-30 | 1915-06-03 | Eugene Schneider | Improvements in or relating to Double Acting Fuses for Projectiles. |
JPH0594752A (en) * | 1991-04-30 | 1993-04-16 | Daikin Ind Ltd | Temperature switch for high speed flying body |
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 |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103776316A (en) * | 2014-01-18 | 2014-05-07 | 尹晓春 | Rotary projectile fuse disassembling equipment and rotary disassembling method |
CN103776316B (en) * | 2014-01-18 | 2015-08-19 | 尹晓春 | Projectile fuze revolves the equipment of unloading and revolves discharging method |
CN104482818A (en) * | 2014-11-24 | 2015-04-01 | 河南中南工业有限责任公司 | Medium-caliber cannonball automatic disassembly production line |
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 |
CN107310124A (en) * | 2017-08-18 | 2017-11-03 | 苏州爱得华塑化有限公司 | A kind of CABLE MATERIALS mould of fast assembling-disassembling |
CN107322901A (en) * | 2017-08-18 | 2017-11-07 | 苏州爱得华塑化有限公司 | A kind of CABLE MATERIALS mould of fast demountable |
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 |
CN113607009A (en) * | 2021-06-30 | 2021-11-05 | 湖南云箭集团有限公司 | Wrench for disassembling ammunition fuse at side position |
CN114322681A (en) * | 2021-12-13 | 2022-04-12 | 中铁十九局集团轨道交通工程有限公司 | Fuse intercepting device convenient to operate |
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 |
Also Published As
Publication number | Publication date |
---|---|
CN202158810U (en) | 2012-03-07 |
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PB01 | Publication | ||
C10 | Entry into substantive examination | ||
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AD01 | Patent right deemed abandoned |
Effective date of abandoning: 20111019 |
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C20 | Patent right or utility model deemed to be abandoned or is abandoned |