CN106767199A - It is a kind of to prevent that spanner is unloaded in the rocket-powered fuse for flying off rotation - Google Patents
It is a kind of to prevent that spanner is unloaded in the rocket-powered fuse for flying off rotation Download PDFInfo
- Publication number
- CN106767199A CN106767199A CN201611261772.6A CN201611261772A CN106767199A CN 106767199 A CN106767199 A CN 106767199A CN 201611261772 A CN201611261772 A CN 201611261772A CN 106767199 A CN106767199 A CN 106767199A
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- China
- Prior art keywords
- rocket
- fixture block
- rotation
- spanner
- unloaded
- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/06—Dismantling fuzes, cartridges, projectiles, missiles, rockets or bombs
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Clamps And Clips (AREA)
Abstract
Prevent that spanner, including main frame, screw rod, fixture block, fixture block set, rocket fixing hanger, rocket are unloaded in the rocket-powered fuse for flying off rotation the invention discloses a kind of；Main frame is rectangular frame structure, short frame two ends are mounted on screw rod, the chute slided for fixture block set is equipped with inside two long margin frames, fixture block set is respectively connected with two screw rods, fixture block set is internal to be provided with fixture block, outside two ends are all provided with chute mouthful, can be in the slide inside two long margin frames of main frame；Rocket fixing hanger is installed, rocket is fixed in cylindrical mounting cylinder, and both sides are reversing device outside the two ends long margin frame of main frame；Two clampings or release of fixture block can be driven by the rotation of screw rod；Rocket fixing hanger can do the fine setting of above-below direction around main frame, so that adjustable rocket produces the lower pressure for needing, prevent spanner from being flown off in rotary course；It is simple structure of the present invention, easy to operate, it is convenient for carrying, work-yard strong adaptability, it is particularly suited for the operation of wild environment and the dismounting of not clear dud fuse.
Description
Technical field
It is particularly a kind of to prevent that spanner is unloaded in the rocket-powered fuse for flying off rotation the invention belongs to field of explosion.
Background technology
Fuse is an important component of ammunition, and rotation is unloaded ammunition fuze and tears relatively common and important in quick-fried work open
Operation, its safety requirements is high, dismounting difficulty is big.Especially for not clear dud, the danger of manual demolition is greatly.It is existing
It is low that spanner automaticity is unloaded in fuse rotation in field, relies primarily on manual operations, inefficiency and to there is greatly safety hidden
Suffer from.Further, since the profile of fuse is mostly the streamlined conical surface, more wasted time and energy during treatment by hand.Therefore, it is necessory to provide
Equipment is unloaded in a kind of brand-new field fuse rotation, to solve above-mentioned technical problem, realizes the work(that remote-controlled operation and automatic rotary are unloaded
Can, improve security and efficiency that work is unloaded in fuse rotation.
Chinese patent ZL201410021860.3 discloses a kind of projectile fuze rotation and unloads equipment and rotation discharging method, Chinese patent
ZL201410277142.2 discloses a kind of small-bore antiaircraft cartridge fuse rotation handler, Chinese patent ZL200620166127.1
A kind of bullet fuse rotary-detaching device is disclosed, the patent that these relevant fuse rotations are unloaded, described being possesses Working gantry, drive division
The more complete equipment such as part is unloaded in part and rotation, mainly using hydraulic-driven, carries out mechanical, electrical, air-liquid coordinated signals, is realized
Automatic rotary is unloaded, and is used safe and efficient.However, equipment described in these patents, it is necessary to condition of work it is higher, and work
Place is generally confined within fixed interior, poor mobility, it is impossible to meet the demand of not clear dud and the explosion-proof explosive operation in field.
The content of the invention
Technical problem solved by the invention is that offer is a kind of prevents that spanner is unloaded in the rocket-powered fuse for flying off rotation, uses
Rocket realizes that remote-controlled operation and automatic rotary are unloaded as driving force, overcomes during prior art fuse rotation in the wild unloads operation
Security and less efficient problem.
The technical solution for realizing the object of the invention is：It is a kind of to prevent that spanner is unloaded in the rocket-powered fuse for flying off rotation, wrap
Include main frame, screw rod, fixture block, fixture block set, rocket fixing hanger, rocket；The short frame two ends of main frame are provided with screw rod, two sides long
Inframe portion is equipped with the chute slided for fixture block set, and fixture block set is respectively connected with two screw rods, and fixture block set is internal to be provided with folder
Block, outside two ends are all provided with chute mouthful, can be in the slide inside two long margin frames of main frame；Outside the two ends long margin frame of the main frame
Portion is provided with rocket fixing hanger, and the mounting cylinder of fixed rocket is provided with rocket fixing hanger, and the rocket is fixed on installation
In cylinder, both sides are reversing device.
The present invention compared with prior art, its remarkable advantage：
(1) with rocket as driving force, can realize that remote-controlled operation and automatic rotary are unloaded by the far distance controlled to rocket,
Improve security and operating efficiency；
(2) design of bearing pin and chute be capable of achieving fixture block self-view change and its main inframe position movement,
It is good to cylinder or taper fuse class spirals adaptability, improve operating efficiency；
(3) by the adjustment of rocket mounting cylinder setting angle, rocket can be made to realize inclined angle up or down, so that
The lower pressure for needing is produced, prevents spanner from being flown off in rotary course and caused danger；
(4) different functions can be realized by the change of semitight hand spiral shell position long：Can be used to seal the effect of rocket,
Long-time beneficial to rocket is preserved；Rocket can also reinforced with the mounting cylinder in rocket fixing hanger, rocket is prevented in work shape
Flying off during state；
(5) conversion of direction of rotation can be easily realized by way of positive and negative is exchanged, waits to revolve for tightening or unclamping
Turn thing.
(6) simple structure of the present invention, easy to operate, is convenient for carrying, and work-yard strong adaptability is particularly suited for field ring
The operation in border and the dismounting of not clear dud fuse.
The present invention is described in further detail below in conjunction with the accompanying drawings.
Brief description of the drawings
Fig. 1 is the structural representation that spanner is unloaded in rocket-powered fuse rotation.
Fig. 2 is fixture block structural representation.
Fig. 3 is that semitight hand spiral shell long is arranged on rocket nozzle position view.
Fig. 4 is that semitight hand spiral shell long is arranged on rocket head position view
1. main frame, 2. screw rod, 3. fixture block, 4. fixture block set, 5. rocket fixing hanger, 6. rocket, 7. fixing bolt, 8. sells
Axle, 9.V type grooves, 10. semitight hand spiral shell long, 11. rocket nozzles
Specific embodiment
It is a kind of to prevent that spanner is unloaded in the rocket-powered fuse for flying off rotation with reference to Fig. 1 to Fig. 4, including：Main frame 1, screw rod 2, fixture block
3rd, fixture block set 4, rocket fixing hanger 5, rocket 6, fixing bolt 7 and bearing pin 8；
The main frame 1 is rectangular frame structure, and structure phase is provided with what the centre at two short frame ends was respectively symmetrically
Same screw rod 2, screw rod 2 is coordinated with main frame 1 by screw thread, and the chutes slided for fixture block set 4 are equipped with inside two long margin frames；
Inside main frame 1, structure identical fixture block set 4 is respectively connected with two screw rods 2；Fixture block set 4 takes the shape of the letter U structure, U-shaped knot
It is connected with screw rod in the middle of structure bottom, inside is provided with fixture block 3, outside two ends are all provided with chute mouthful, can be in 1 two long margin frames of main frame
The slide in portion；The structure of the fixture block 3 is identical, is symmetrically mounted in two fixture block sets 4, and V-groove is equipped with respect to pinching end
9, it is easy to the clamping of clipped object；
Used as preferred embodiment, fixture block 3 covers 4 and is connected by both sides bearing pin 8 and fixture block, and the fixture block 3 can be around pin
Axle 8 rotates, and the bearing pin 8 is symmetrically mounted on fixture block set inside, and fixture block 3 realizes the regulation of self-view by bearing pin 8, to cylinder
Or taper fuse class spirals adaptability is good, improves operating efficiency；
The screw rod 2 is freely rotatable with the connection end of fixture block set 4, and fixture block can be driven with the rotation of main frame 1 by screw rod 2
Set 4 is moved in main frame 1, so as to drive two clampings or release of fixture block 3；
The two ends long margin frames outside intermediate symmetry of the main frame 1 is provided with structure identical rocket fixing hanger 5, described
Rocket fixing hanger 5 is rectangular shaped rim structure, is connected with rocket fixing hanger 5 by fixing two bolts 7；Described two fire
The other end of arrow fixing hanger 5 is mounted on the cylindrical mounting cylinder for fixing rocket 6, the installation site of mounting cylinder it is symmetrical but
Installation direction is opposite；The rocket 6 is fixed in mounting cylinder, and used as rotary power, both sides are reversing device, can promote to form power
Even, help is realized tightening or unclamped；
Used as preferred embodiment, rocket fixing hanger 5 is provided with elongated slot in an installation site for bolt 7 wherein
Hole so that rocket fixing hanger 5 can do the fine setting of above-below direction around the relatively main frame 1 of one of bolt 7；So as to adjustable rocket
6 realize inclined angle up or down, so as to produce the lower pressure of needs, prevent spanner from being flown off in rotary course and occurred
It is dangerous；
Further optimization as the present invention to above-mentioned implementation method, installs the semitight long of sealing rocket on rocket 6
Hand spiral shell 10, the semitight hand spiral shell 10 long is the cylindrical structure of one end closing, and inside is provided with installation screw thread；In spanner inoperative
When, can be screwed on rocket nozzle 11, play a part of to seal rocket, the long-time beneficial to rocket is preserved；When spanner is enabled, can
Rocket head one end is screwed in, rocket 6 is reinforced with the mounting cylinder in rocket fixing hanger 5, flying when preventing rocket in working order
It is de-.
Further optimization as the present invention to above-mentioned implementation method, mark has 6 installations on the two sides of main frame 1
Direction of rotation afterwards, can point out the installation of the tow sides of the main frame 1 of operator；Positive and negative the two of main frame 1 can as needed be adjusted
Face installation direction, so as to adjust the direction of rotation of rocket 6, gig is treated for tightening or unclamping；
In other implementation method, the main frame 1 and rocket fixing hanger 5 can also be circular or other shapes,
The short frame and long margin frame of the main frame 1, so as to constitute rectangular configuration, can may also be circular arc with length identical straight flange mount structure
Border structure, constitutes the structure of circular configuration or other shapes, and the inside of main frame 1 is by welding or bolt or the overall affixed cunning of cutting
Slot structure；Setting angle can be fixed by single bolt 7 and adjusted to circular rocket fixing hanger 5；
In other implementation methods, the rocket mounting cylinder at least two can at least install two rockets 6,
Multiple rockets 6 can be as needed installed, the turning pair of rocket 6 can be increased；
It is of the present invention to prevent that spanner is unloaded in the rocket-powered fuse for flying off rotation, due to its simple structure, easy to operate, appearance
It is portable, the features such as safe and reliable, the working environment of complexity can be adapted to, it is especially suitable for field operation；It is simultaneously of the present invention
The rocket-powered fuse for preventing flying off rotation unload spanner, can also be applied to the helicitic texture device of other cylinders or vertebra shape, such as fill
Screw thread on the tank or pipe of dangerous thing.
Claims (10)
1. it is a kind of to prevent that spanner is unloaded in the rocket-powered fuse for flying off rotation, it is characterised in that including main frame (1), screw rod (2), fixture block
(3), fixture block set (4), rocket fixing hanger (5), rocket (6)；The short frame two ends of main frame (1) are provided with screw rod (2), and two long
The chute slided for fixture block set (4) is equipped with inside frame, fixture block set (4), fixture block set are respectively connected with two screw rods (2)
(4) internal to be provided with fixture block (3), outside two ends are all provided with chute mouthful, can be in the slide inside (1) two long margin frame of main frame；
Rocket fixing hanger (5) is installed, rocket fixing hanger is provided with fixation on (5) outside the two ends long margin frame of the main frame (1)
The mounting cylinder of rocket, the rocket (6) is fixed in mounting cylinder, and both sides are reversing device.
2. spanner is unloaded in a kind of rocket rotation for preventing flying off according to claim 1, it is characterised in that：The main frame (1) is
Rectangular frame shape structure, is equipped with the chute slided for fixture block set (4) inside two long margin frames.
3. spanner is unloaded in a kind of rocket rotation for preventing flying off according to claim 1, it is characterised in that the main frame (1) it is short
Frame and long margin frame can may also be arcuate border structure and constitute circle with length identical straight flange mount structure so as to be constituted rectangular configuration
The structure of shape structure or other shapes, by welding or bolt or the overall affixed sliding groove structure of cutting inside main frame (1).
4. spanner is unloaded in a kind of rocket rotation for preventing flying off according to claim 1, it is characterised in that：The fixture block (3) can
Around bearing pin (8) rotation；Fixture block (3) structure is identical, is symmetrically mounted in two fixture block sets (4), is all provided with respect to pinching end
There is the V-groove (9) for being easy to clamp clipped object.
5. spanner is unloaded in a kind of rocket rotation for preventing flying off according to claim 1, it is characterised in that the rocket is fixed and hung
Ear (5) is rectangular shaped rim structure, is connected with rocket fixing hanger (5) by fixing two bolts (7)；A bolt wherein
(7) rocket fixing hanger (5) is provided with long slot bore in installation site so that rocket fixing hanger (5) can be around one of bolt
(7) relatively main frame (1) does the fine setting of above-below direction.
6. spanner is unloaded in a kind of rocket rotation for preventing flying off according to claim 1, it is characterised in that rocket fixing hanger (5)
It is circular, can be fixed by single bolt (7) and adjustment setting angle.
7. spanner is unloaded in a kind of rocket rotation for preventing flying off according to claim 1, it is characterised in that pacified on rocket (6)
The semitight hand spiral shell (10) long of dress sealing rocket, when spanner inoperative is unloaded in rocket rotation, can be screwed on rocket nozzle (11)；In fire
When arrow rotation is unloaded spanner and enabled, rocket head one end can be screwed in.
8. spanner is unloaded in a kind of rocket rotation for preventing flying off according to claim 1, it is characterised in that main frame (1) two sides
On mark have prompting operator rocket (6) install after direction of rotation.
9. spanner is unloaded in a kind of rocket rotation for preventing flying off according to claim 1, it is characterised in that the rocket mounting cylinder
It it is two, installation site is symmetrical but installation direction is opposite.
10. spanner is unloaded in a kind of rocket rotation for preventing flying off according to claim 1, it is characterised in that the rocket mounting cylinder
At least two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611261772.6A CN106767199B (en) | 2016-12-30 | 2016-12-30 | It is a kind of to prevent that spanner is unloaded in the rocket-powered fuse flown off rotation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611261772.6A CN106767199B (en) | 2016-12-30 | 2016-12-30 | It is a kind of to prevent that spanner is unloaded in the rocket-powered fuse flown off rotation |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106767199A true CN106767199A (en) | 2017-05-31 |
| CN106767199B CN106767199B (en) | 2018-06-12 |
Family
ID=58954844
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611261772.6A Active CN106767199B (en) | 2016-12-30 | 2016-12-30 | It is a kind of to prevent that spanner is unloaded in the rocket-powered fuse flown off rotation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106767199B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110332859A (en) * | 2019-07-19 | 2019-10-15 | 湖北三江航天红林探控有限公司 | A kind of general clamping device suitable for fuse assembly |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3210090A1 (en) * | 1982-03-19 | 1983-10-06 | Karl Schwabenbauer | Bomb-fuse removal unit |
| CN1670466A (en) * | 2005-04-30 | 2005-09-21 | 中国人民解放军总装备部军械技术研究所 | Portable fuse disassembling and combining machine |
| KR100872053B1 (en) * | 2007-06-07 | 2008-12-05 | 국방과학연구소 | Wrench provided socket to assemble or disassemble bomb-fuse |
| RU2011131465A (en) * | 2011-07-26 | 2013-02-10 | Федеральное государственное унитарное предприятие "Производственное объединение "Завод имени Серго" | METHOD FOR DISMANTLING THE HEAD EXPLOSION CARTRIDGE FOR THE GRANOMETER AND INSTALLATION FOR ITS IMPLEMENTATION |
| CN206450143U (en) * | 2016-12-30 | 2017-08-29 | 南京神行者机电科技有限公司 | It is a kind of to prevent that spanner is unloaded in the rocket-powered fuse flown off rotation |
-
2016
- 2016-12-30 CN CN201611261772.6A patent/CN106767199B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3210090A1 (en) * | 1982-03-19 | 1983-10-06 | Karl Schwabenbauer | Bomb-fuse removal unit |
| CN1670466A (en) * | 2005-04-30 | 2005-09-21 | 中国人民解放军总装备部军械技术研究所 | Portable fuse disassembling and combining machine |
| KR100872053B1 (en) * | 2007-06-07 | 2008-12-05 | 국방과학연구소 | Wrench provided socket to assemble or disassemble bomb-fuse |
| RU2011131465A (en) * | 2011-07-26 | 2013-02-10 | Федеральное государственное унитарное предприятие "Производственное объединение "Завод имени Серго" | METHOD FOR DISMANTLING THE HEAD EXPLOSION CARTRIDGE FOR THE GRANOMETER AND INSTALLATION FOR ITS IMPLEMENTATION |
| CN206450143U (en) * | 2016-12-30 | 2017-08-29 | 南京神行者机电科技有限公司 | It is a kind of to prevent that spanner is unloaded in the rocket-powered fuse flown off rotation |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110332859A (en) * | 2019-07-19 | 2019-10-15 | 湖北三江航天红林探控有限公司 | A kind of general clamping device suitable for fuse assembly |
| CN110332859B (en) * | 2019-07-19 | 2024-01-16 | 湖北三江航天红林探控有限公司 | Universal clamping device suitable for fuse assembly |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106767199B (en) | 2018-06-12 |
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