CN106643336A - Plastic fletching jig for adhering arrow feathers on arrow - Google Patents
Plastic fletching jig for adhering arrow feathers on arrow Download PDFInfo
- Publication number
- CN106643336A CN106643336A CN201510739396.6A CN201510739396A CN106643336A CN 106643336 A CN106643336 A CN 106643336A CN 201510739396 A CN201510739396 A CN 201510739396A CN 106643336 A CN106643336 A CN 106643336A
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- China
- Prior art keywords
- fletching
- plasticity
- base
- rocket body
- arrow
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B6/00—Projectiles or missiles specially adapted for projection without use of explosive or combustible propellant charge, e.g. for blow guns, bows or crossbows, hand-held spring or air guns
- F42B6/02—Arrows; Crossbow bolts; Harpoons for hand-held spring or air guns
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Media Introduction/Drainage Providing Device (AREA)
Abstract
The invention discloses a plastic fletching jig for adhering arrow feathers on an arrow. The plastic fletching jig comprises a C like shaped frame which is composed of a top surface, a side surface and a bottom surface; the top surface of the C like shaped frame is connected with the side surface of the C like shaped frame in a hinging manner; a chassis is processed on the bottom surface of the C like shaped frame and is fixedly provided with a base; a tail part insertion connecting hole is arranged in the chassis and the base in an integral penetrating manner; the base is provided with a three-way insertion connecting component; the three-way insertion connecting component is formed by fixedly connecting two elastic rail clamping devices with a same structure and a cylindrical bracket arranged between the two elastic rail clamping devices; an axial first arrow hole is formed in the center position of the three-way insertion connecting component; and a second arrow hole which is consistent to the first arrow hole is formed in the top surface of the C like shaped frame. The plastic fletching jig is simple in structure, low in manufacturing cost, convenient to carry, good in stability, wide in using range and high in adhesion efficiency.
Description
Technical field
The present invention relates to the fletching bonding viscous plumage device of plasticity on tackle field, more particularly to a kind of rocket body.
Background technology
At present, from market survey, the price of a wooden arrow finished product is typically between 10 to 15 yuan, and the cost of parts of a wooden arrow is at 3 yuan or so, and both gaps are larger.Also, because the phenomenon of quick-fried arrow during archery happens occasionally, so toxophilus is larger to the demand of viscous plumage device.But, known viscous plumage device is typically using aluminum or cast iron materials, not only price is very high, device bulky complex, it is difficult remote way to carry, and may be only available for the viscous plumage of same arrow kind, flexibility is poor, secondly, fletching bonding angle it is whether accurate, directly affect the technology of archery, therefore, the angle for how fast and accurately focusing on fletching bonding is also current still unsolved technical barrier, again, existing viscous plumage device kind is few, single function, every time can only one fletching of bonding, bonding efficiency is low, affect the mood of archery people, waste the time of archery people.
The content of the invention
For above-mentioned problem, the present invention is intended to provide the fletching bonding viscous plumage device of plasticity on a kind of rocket body of three-dimensional one.
To achieve these goals, the technical solution adopted in the present invention is as follows：
The fletching bonding viscous plumage device of plasticity on a kind of rocket body, including class c-type framework, the class c-type framework is by top surface, side and bottom surface constitute, it is articulated and connected between the top surface of the class c-type framework and side, chassis is machined with the bottom surface of the class c-type framework, base is fixed with the chassis, the chassis is provided with afterbody spliced eye with the chassis interior one insertion, three-dimensional connecting element is set on the base, the three-dimensional connecting element is formed by fixedly connecting by two structure identical elastic track clamping devices and the cylindrical stent between two elastic track clamping devices, the first axial barbican is provided with the three-dimensional connecting element center, and it is provided with second barbican consistent with first barbican on the top surface of the class c-type framework.
Further, the cylindrical stent is the cylindrical structural surrounded by three structure identical sector element structures, and notch is formed between sector element described in each two.
Further, it is marked with scale in the sector element positioned at the notch both sides.
Further, the elastic track clamping device is the cylindrical structural surrounded by three structure identical sector entity components, and gap is formed between fan-shaped entity component described in each two.
Further, it is machined with and its arching trajectory identical arc track inside each described fan-shaped entity component, is machined with each described fan-shaped entity component between interior loop-drive, and the adjacent loop of each two and forms fletching perforation.
Further, two-way return facilities is set inside the arc track, in the both ends of the two-way return facilities one connecting spring piece, each described spring leaf is respectively positioned in first barbican, and fletching holes for clamping is formed between two opposite spring leafs in same first barbican.
Further, circular trough is set in the chassis, and the base of the base coordinates socket with the circular trough.
The invention has the beneficial effects as follows：First, the present invention is capable of achieving, by fletching colleague's bonding that three reverse on rocket body, to improve bonding efficiency using the three-dimensional connecting element of three-dimensional one by three-dimensional connecting element；Secondly, elastic track clamping device is set, being capable of achieving fletching by elastic track clamping device can quickly be fixed before bonding, and elastic track clamping device can also realize the viscous plumage to different arrow kinds, expand its scope of application, elastic track clamping device is using fan-shaped entity component, processing arc track in fan-shaped entity component, two-way return facilities is set in arc track, two-way return facilities two ends arrange spring leaf, due to the specification of each direction fletching it is identical, before bonding, dynamics suffered by two-way return facilities two ends is uniform, during clamping, shrink to track interior simultaneously at two ends, can guarantee that each fletching clamps dynamics in clamping process suffered by both sides identical, fletching bonding location is accurate；Again, the viscous plumage device simple structure of present invention design, low manufacture cost is easy to carry, and can ensure the stability that plumage is glued during viscous plumage using class c-type framework；Additionally, being marked with scale in shape unit, it is ensured that the quick positioning of fletching during viscous plumage, there is provided faster direction determine and direction calibration, improve the accuracy of position.
Description of the drawings
Fig. 1 is schematic front view of the present invention.
Fig. 2 is the internal structure schematic diagram of three-dimensional connecting element of the present invention.
Fig. 3 for chassis of the present invention schematic internal view.
Fig. 4 is the schematic diagram of cylindrical stent of the present invention
Wherein：1- " C " type framework, 2- chassis, 3- bases, 31- circular troughs, 4- afterbody spliced eyes, 5- cylindrical stents, 51- arc frames, 52- notches, 6- elastic track clamping devices, 61- sector entity components, 611- solids, loop-drive in 612-, 613- sides, 62- arc tracks, the two-way return facilitieses of 63-, 64- spring leafs, 7- fletchings are bored a hole, 8- fletching holes for clamping, 9- rocket bodies, the barbicans of 10- first, 11- gap, the barbicans of 12- second.
Specific embodiment
In order that one of ordinary skill in the art is better understood on technical scheme, technical scheme is further described with reference to the accompanying drawings and examples.
The viscous plumage device of fletching bonding plasticity on a kind of rocket body that referring to the drawings 1-4 shows，The fletching bonding viscous plumage device of plasticity on a kind of rocket body，Including class c-type framework 1，The class c-type framework 1 is by top surface、Side and bottom surface constitute，The side and bottom surface of the class c-type framework 1 is integrally cast，It is articulated and connected by jointed shaft between the top surface of the class c-type framework 1 and side，Its top surface and bottom surface are parallel to each other，Using class c-type framework 1 as the main body of viscous plumage device be in order to improve whole viscous plumage during stability，Because class c-type framework 1 includes two top surfaces being parallel to each other and bottom surface，It is convenient that rocket body 9 is placed between top surface and bottom surface，Chassis 2 is machined with the bottom surface of the class c-type framework 1，Base 3 is fixed with the chassis 2，Circular trough 21 is set in the chassis 2，The base of the base 3 coordinates socket with the circular trough 21，The convex tendon of the clamping that cooperates with circular trough 21 is machined with base 3，By convex tendon and the close fit of circular trough 21，Achievable base 3 is detachably connected with chassis 2，The chassis 2 is provided with afterbody spliced eye 4 with the inside one insertion of the base 3，Rocket body 9 can be plugged on the afterbody of rocket body 9 in afterbody spliced eye 4 in bonding fletching，Ensure the stability of the bottom of rocket body 9，And it is without damage，Three-dimensional connecting element is set on the base 3，The three-dimensional connecting element is formed by fixedly connecting by two structure identical elastic track clamping devices 6 and the cylindrical stent 5 between two elastic track clamping devices 6，The elastic track clamping device 6 is correspondingly arranged at the top and bottom position of cylindrical stent 5，The first axial barbican 10 is provided with the three-dimensional connecting element center，And it is provided with second barbican 12 consistent with first barbican 10 on the top surface of the class c-type framework 1.
In the present invention, the cylindrical stent 5 is the cylindrical structural surrounded by three structures of structure identical sector element 51, notch 52 is formed described in each two between sector element 51, scale is marked with the sector element 51 positioned at the both sides of the notch 52, scale is vertically marked, and reference mark can quickly determine the bonding location of fletching.
In the present invention，The elastic track clamping device 6 is the cylindrical structural surrounded by three structure identical sector entity components 61，Gap 11 is formed described in each two between fan-shaped entity component 61，It is machined with inside each described fan-shaped entity component 61 and its arching trajectory identical arc track 62，Interior loop-drive 612 is machined with each described fan-shaped entity component 61，And fletching perforation 7 is formed between the adjacent loop 612 of each two，Two-way return facilities 63 is set inside the arc track 62，In the both ends of the two-way return facilities 63 one connecting spring piece 64，Each described spring leaf 64 is respectively positioned in first barbican 10，And fletching holes for clamping 8 is formed between two opposite spring leafs 64 in same first barbican 10，The setting of spring leaf 64 ensure that fletching can remain the route that takes the air line when injecting in fletching holes for clamping 8，Do not incline to both sides or bend，Ensure the accuracy of fletching bonding angle.
Elastic railway clamping device 6 is separately positioned on the upper and lower side of cylindrical stent 5 in the present invention, elastic track clamping device 6 is made up of three structure identical sector entity components 61, cylindrical stent 5 is made up of three structure identical sector elements 51, and the upper end of each sector element 51, lower end corresponds to respectively a fan-shaped entity component 61, first barbican 10 is through elastic track clamping device 6 and cylindrical stent 5, thickness of the thickness of the fan-shaped entity component 61 more than the sector element 51, purpose is to increase the diameter of the first barbican 10 inside the sector element 51, so that hole is bigger during bonding fletching, more convenient bonding.
During work, rocket body 9 is downwardly into from the second barbican 10, and just inject the bottom of rocket body 9 in chassis 2, then from three notches 52 start to be placed on fletching in elastic track clamping device 6 successively, the spring leaf 631 being oppositely arranged by two panels is clamped each fletching with correct bonding direction, three fletchings are after successively sandwiched is good, proceed by bonding, after the completion of bonding, class c-type framework 1 is dug upwards, the rocket body 9 of bonding fletching is taken out, then the top surface of class c-type framework 1 resets, be ready in next viscous plumage.
Claims (7)
1. fletching bonding glues plumage device with plasticity on a kind of rocket body, it is characterised in that：Including class c-type framework（1）, the class c-type framework（1）It is made up of top surface, side and bottom surface, the class c-type framework（1）Top surface and side between be articulated and connected, in the class c-type framework（1）Bottom surface on be machined with chassis（2）, the chassis（2）On be fixed with base（3）, the chassis（2）With the base（3）Internal one insertion is provided with afterbody spliced eye（4）, in the base（3）Upper setting three-dimensional connecting element, the three-dimensional connecting element is by two structure identical elastic track clamping devices（6）And located at two elastic track clamping devices（6）Between cylindrical stent（5）It is formed by fixedly connecting, in the three-dimensional connecting element center the first axial barbican is provided with（10）, and in the class c-type framework（1）Top surface on be provided with and first barbican（10）The second consistent barbican（12）.
2. fletching bonding glues plumage device with plasticity on a kind of rocket body according to claim 1, it is characterised in that：The cylindrical stent（5）It is by three structure identical sector elements（51）The cylindrical structural that structure is surrounded, sector element described in each two（51）Between form notch（52）.
3. fletching bonding glues plumage device with plasticity on a kind of rocket body according to claim 2, it is characterised in that：Positioned at the notch（52）The sector element on both sides（51）It is marked with scale.
4. fletching bonding glues plumage device with plasticity on a kind of rocket body according to claim 1, it is characterised in that：The elastic track clamping device（6）It is by three structure identical sector entity components（61）The cylindrical structural for surrounding, fan-shaped entity component described in each two（61）Between form gap（11）.
5. fletching bonding glues plumage device with plasticity on a kind of rocket body according to claim 4, it is characterised in that：In each fan-shaped entity component（61）Inside is machined with and its arching trajectory identical arc track（62）, each described fan-shaped entity component（61）On be machined with interior loop-drive（612）, and the adjacent loop of each two（612）Between formed fletching perforation（7）.
6. fletching bonding glues plumage device with plasticity on a kind of rocket body according to claim 5, it is characterised in that：In the arc track（62）Inside arranges two-way return facilities（63）, in the two-way return facilities（63）Both ends one connecting spring piece（64）, each described spring leaf（64）It is respectively positioned on first barbican（10）It is interior, and same first barbican（10）Two interior opposite spring leafs（64）Between formed fletching holes for clamping（8）.
7. fletching bonding glues plumage device with plasticity on a kind of rocket body according to any one of claim 1-6, it is characterised in that：On the chassis（2）Interior setting circular trough（21）, the base（3）Base and the circular trough（21）Coordinate socket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510739396.6A CN106643336B (en) | 2015-11-04 | 2015-11-04 | Fletching bonding glues plumage device with plasticity on rocket body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510739396.6A CN106643336B (en) | 2015-11-04 | 2015-11-04 | Fletching bonding glues plumage device with plasticity on rocket body |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106643336A true CN106643336A (en) | 2017-05-10 |
| CN106643336B CN106643336B (en) | 2018-02-09 |
Family
ID=58850735
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510739396.6A Expired - Fee Related CN106643336B (en) | 2015-11-04 | 2015-11-04 | Fletching bonding glues plumage device with plasticity on rocket body |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106643336B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3024017A (en) * | 1959-08-17 | 1962-03-06 | Stanton Lon | Fletching jig for arrows |
| CN203163616U (en) * | 2012-12-27 | 2013-08-28 | 北京百慕航材高科技股份有限公司 | Arrow shaft feather bonding device |
| CN204202495U (en) * | 2014-10-27 | 2015-03-11 | 南京工程学院 | A kind of sticky plumage device |
| CN104457440A (en) * | 2014-11-18 | 2015-03-25 | 谭美俊 | Horizontal feather sticking device used for sticking arrow feathers |
| CN104482811A (en) * | 2014-11-18 | 2015-04-01 | 谭美俊 | Vertical fletching jig for arrow feather fletching |
-
2015
- 2015-11-04 CN CN201510739396.6A patent/CN106643336B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3024017A (en) * | 1959-08-17 | 1962-03-06 | Stanton Lon | Fletching jig for arrows |
| CN203163616U (en) * | 2012-12-27 | 2013-08-28 | 北京百慕航材高科技股份有限公司 | Arrow shaft feather bonding device |
| CN204202495U (en) * | 2014-10-27 | 2015-03-11 | 南京工程学院 | A kind of sticky plumage device |
| CN104457440A (en) * | 2014-11-18 | 2015-03-25 | 谭美俊 | Horizontal feather sticking device used for sticking arrow feathers |
| CN104482811A (en) * | 2014-11-18 | 2015-04-01 | 谭美俊 | Vertical fletching jig for arrow feather fletching |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106643336B (en) | 2018-02-09 |
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Granted publication date: 20180209 Termination date: 20191104 |
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