CN106643335B - The viscous plumage device of fletching bonding on rocket body - Google Patents
The viscous plumage device of fletching bonding on rocket body Download PDFInfo
- Publication number
- CN106643335B CN106643335B CN201510739141.XA CN201510739141A CN106643335B CN 106643335 B CN106643335 B CN 106643335B CN 201510739141 A CN201510739141 A CN 201510739141A CN 106643335 B CN106643335 B CN 106643335B
- Authority
- CN
- China
- Prior art keywords
- fletching
- viscous
- bonding
- class
- rocket body
- 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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Classifications
-
- 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
-
- 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
- F42B6/04—Archery arrows
- F42B6/06—Tail ends, e.g. nocks, fletching
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Packaging Of Annular Or Rod-Shaped Articles, Wearing Apparel, Cassettes, Or The Like (AREA)
- Media Introduction/Drainage Providing Device (AREA)
Abstract
The invention discloses the viscous plumage device of fletching bonding on rocket body, including class c-type framework, class c-type framework is by top surface, side and bottom surface composition, it is articulated and connected between the top surface of class c-type framework and side, chassis is machined with the bottom surface of class c-type framework, base is fixed with chassis, integrally insertion is provided with afterbody spliced eye with chassis interior on chassis, clamp assemblies are set on base, clamp assemblies are formed by fixedly connecting by two structure identical elastic clamp devices and the cylindrical frame between two elastic clamp devices, the first barbican of axial direction is provided with clamp assemblies center, and second barbican consistent with the first arrow is provided with the top surface of class c-type framework；The present invention is simple in construction, low manufacture cost, is easy to carry, and stability is good, and use range is wide, is bonded efficiency high.
Description
Technical field
The present invention relates to the viscous plumage device of fletching bonding 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 wooden arrow
For cost of parts at 3 yuan or so, both gaps are larger.Also, the phenomenon of quick-fried arrow happens occasionally during due to archery, so archery hobby
Person is larger to the demand for gluing plumage device.It is well known, however, that viscous plumage device typically use aluminum or cast iron materials, not only price is very
High, device bulky complex, it is not easy remote way and carries, and may be only available for same arrow kind and glue plumage, flexibility is poor, secondly,
Fletching bonding angle it is whether accurate, directly affect the technology of archery, therefore, how fast and accurately to focus on fletching bonding angle
Degree and at present still unsolved technical barrier, again, existing viscous plumage device less varieties, function is single, can only be bonded one every time
Individual fletching, bonding efficiency is low, influences the mood of archery people, wastes the time of archery people.
The content of the invention
For above-mentioned problem, the present invention is intended to provide the viscous plumage of fletching bonding on a kind of rocket body of three-dimensional one
Device.
To achieve these goals, the technical solution adopted in the present invention is as follows：
Fletching bonding viscous plumage device, including class c-type framework on a kind of rocket body, the class c-type framework by top surface, side and
Bottom surface forms, and is articulated and connected between the top surface of the class c-type framework and side, is machined with the bottom surface of the class c-type framework
Chassis, base is fixed with the chassis, integrally insertion is provided with afterbody spliced eye with the chassis interior on the chassis, in institute
State and clamp assemblies are set on base, the clamp assemblies are described in as two structure identical elastic clamp devices and located at two
Cylindrical frame between elastic clamp device is formed by fixedly connecting, and the first of axial direction is provided with the clamp assemblies center
Barbican, and second barbican consistent with first arrow is provided with the top surface of the class c-type framework.
Further, the cylindrical frame is that the cylinder surrounded by three structure identical sector solid framework structures is tied
Structure, notch is formed between fan-shaped solid framework described in each two.
Further, it is marked with scale in the fan-shaped solid framework positioned at the notch both sides.
Further, the elastic clamp device is the cylindrical structural surrounded by three structure identical sector frameworks, often
Gap is formed between two fan-shaped frameworks.
Further, each fan-shaped framework by outer arcuate, arc and is connected to the outer arcuate and described interior
Two sides of the arc-shaped side edges between are formed, and fletching perforation is formed between the adjacent arc side of each two.
Further, return facilities is fixedly connected with each side, the return facilities is by some springs and company
The spring plate groups of spring outwards is connected on into and forming fletching holes for clamping between two opposite return facilitieses.
Further, reinforcement is also set up between the outer arcuate and the arc.
Further, circular trough is set in the chassis, and the base of the base coordinates with the circular trough to be socketed.
The beneficial effects of the invention are as follows：First, the present invention passes through the folder of three-dimensional one using the clamp assemblies of three-dimensional one
Holding component can realize the fletching in three directions on rocket body while be bonded, and improve bonding efficiency；Secondly, elastic clamping is set to fill
Put, can realize that fletching is quickly fixed before bonding by elastic clamp device, and elastic clamp device can also be realized to not
With the viscous plumage of arrow kind, its use range is expanded；Again, the viscous plumage device that the present invention designs is simple in construction, low manufacture cost, is easy to
Carry, and the stability of viscous plumage during viscous plumage can be ensured using class c-type framework；In addition, also marked on fan-shaped solid framework
There is scale, ensure the fast positioning of the fletching during viscous plumage, and the accuracy of bonding location.
Brief description of the drawings
Fig. 1 is schematic front view of the present invention.
Fig. 2 is clamp assemblies internal structure schematic diagram of the present invention.
Fig. 3 is the enlarged drawing of D parts in Fig. 2.
Fig. 4 is the schematic internal view on chassis of the present invention.
Fig. 5 is the schematic diagram of cylindrical frame of the present invention.
Wherein：1- " C " type framework, 2- chassis, 21- circular troughs, 3- bases, 4- afterbody spliced eyes, 5- cylindrical frames,
51- sector solid frameworks, 52- notches, 6- elastic clamp devices, 61- sector frameworks, 611- outer arcuates, 612- arcs, 613-
Side, 62- reinforcements, 63- return facilitieses, 631- spring leafs, 632- springs, the perforation of 7- fletchings, 8- fletching holes for clamping, 9- arrows
Body, the barbicans of 10- first, 11- gap, the barbicans of 12- second.
Embodiment
In order that one of ordinary skill in the art is better understood on technical scheme, below in conjunction with the accompanying drawings and
Embodiment is further described to technical scheme.
Embodiment：Referring to the drawings fletching bonding viscous plumage device, including class c-type framework 1, institute on a kind of rocket body shown in 1-5
State class c-type framework 1 to be made up of top surface, side and bottom surface, the side and bottom surface of the class c-type framework 1 are integrally cast, institute
State and be articulated and connected between the top surface of class c-type framework 1 and side by jointed shaft, its top surface and bottom surface are parallel to each other, using class c-type
Framework 1 is in order to improve the stability during whole viscous plumage, because class c-type framework 1 includes two phases as the main body of viscous plumage device
Mutually parallel top surface and bottom surface, it is convenient that rocket body 9 is placed between top surface and bottom surface, add on the bottom surface of the class c-type framework 1
Work has chassis 2, and base 3 is fixed with the chassis 2, and circular trough 21, the base of the base 3 are set in the chassis 2
Coordinate with the circular trough 21 and be socketed, the convex tendon with the mutual cooperation clamping of circular trough 21 is machined with base 3, passes through convex tendon and circle
The close fit of shape groove 21, achievable base 3 are detachably connected with chassis 2, the chassis 2 and the inside of base 3 one
Insertion is provided with afterbody spliced eye 4, and the afterbody of rocket body 9 can be plugged in afterbody spliced eye 4 by rocket body 9 when being bonded fletching, ensures
The stability of the bottom of rocket body 9, and it is without damage, clamp assemblies are set on the base 3, and the clamp assemblies are by two structures
Identical elastic clamp device 6 and the cylindrical frame 5 between two elastic clamp devices 6 be fixedly connected and
Into the elastic clamp device 6 is correspondingly arranged at the top and bottom position of cylindrical frame 5, at the clamp assemblies center
Position is provided with the first barbican 10 of axial direction, and is provided with the top surface of the class c-type framework consistent with first barbican 10
The second barbican 12.
In the present invention, the cylindrical frame 5 is the circle surrounded by three structures of structure identical sector solid framework 51
Column construction, notch 52 is formed between fan-shaped solid framework 51 described in each two, in the fan positioned at the both sides of notch 52
Shape solid framework 51 is marked with scale, and scale vertically marks.
In the present invention, the elastic clamp device 6 is that the cylinder surrounded by three structure identical sector frameworks 61 is tied
Structure, fan-shaped framework 61 is identical with the fan-shaped shape of solid framework 51, structure, and the inside of fan-shaped framework 61 is hollow-core construction, hollow-core construction
Design be to mitigate weight, save material, gap 11,11 corresponding notch of gap formed between fan-shaped framework 61 described in each two
52, each fan-shaped framework 61 by outer arcuate 611, arc 612 and is connected to the outer arcuate 611 and the inner arc
Two sides 613 of the side of shape 612 between are formed, and reinforcement is also set up between the outer arcuate 611 and the arc 612
62, the setting of reinforcement 62 can increase the intensity of fan-shaped framework 61, and three arcs 612 form first barbican 10,
Fletching perforation 7 is formed between the adjacent side of the arc 612 of each two, is fixedly connected with back on each side 613
Range device 63, the return facilities 63 is by some springs 632 and is connected to the spring leafs 631 of spring outwards and forms, and two
Fletching holes for clamping 8 is formed between the individual opposite return facilities 63, the setting of spring leaf 631 can ensure that fletching is injecting arrow
The route that takes the air line can be remained when in plumage holes for clamping 8, is not tilted to both sides, ensures the accuracy of fletching bonding angle.
Elastic clamp device 6 is separately positioned on to the upper and lower ends of cylindrical frame 5, it is therefore an objective to which being easy to will be viscous in the present invention
The bottom and upper end of plumage position are fixed, and are only reserved and are specifically glued plumage position quickly glue plumage, the design of notch 52 is exactly
In order to make the glue of viscous plumage quickly be squeezed into the viscous plumage opening position on rocket body 9.
During work, rocket body 9 is downwardly into from the second barbican 10, and the bottom of rocket body 9 is injected in chassis 2 just,
Then fletching is placed in elastic clamp device 6 since three notches 52 successively, the spring leaf being oppositely arranged by two panels
631 by each fletching to be correctly bonded direction clamping, three fletchings proceed by bonding after sandwiched is good successively, are bonded completion
Afterwards, class c-type framework 1 is dug upwards, takes out the rocket body 9 of bonding fletching, then the top surface of class c-type framework 1 is resetted, is
Plumage is glued next time to be ready.
Claims (7)
1. the viscous plumage device of fletching bonding on rocket body, it is characterised in that：Including class c-type framework（1）, the class c-type framework（1）By pushing up
Face, side and bottom surface composition, 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 clamp assemblies, the clamp assemblies are by two
Individual structure identical elastic clamp device（6）And located at two elastic clamp devices（6）Between cylindrical frame（5）
It is formed by fixedly connecting, the first barbican of axial direction is provided with the clamp assemblies center（10）, and in the class c-type framework
（1）Top surface on be provided with and first barbican（10）The second consistent barbican（12）, the cylindrical frame（5）It is by three
Individual structure identical sector solid framework（51）The cylindrical structural that structure surrounds, fan-shaped solid framework described in each two（51）It
Between form notch（52）.
2. the viscous plumage device of fletching bonding on rocket body according to claim 1, it is characterised in that：Positioned at the notch（52）
The fan-shaped solid framework on both sides（51）It is marked with scale.
3. the viscous plumage device of fletching bonding on rocket body according to claim 1, it is characterised in that：The elastic clamp device
（6）It is by three structure identical sector frameworks（61）The cylindrical structural surrounded, fan-shaped framework described in each two（61）Between
Form gap（11）.
4. the viscous plumage device of fletching bonding on rocket body according to claim 3, it is characterised in that：Each fan-shaped framework
（61）By outer arcuate（611）, arc（612）And it is connected to the outer arcuate（611）With the arc（612）Side
Two sides between（613）Composition, the adjacent arc of each two（612）Fletching perforation is formed between side（7）.
5. the viscous plumage device of fletching bonding on rocket body according to claim 4, it is characterised in that：Each side（613）
On be fixedly connected with return facilities（63）, the return facilities（63）By some springs（632）And it is connected to spring outwards
Spring leaf（631）Composition, and two opposite return facilitieses（63）Between formed fletching holes for clamping（8）.
6. the viscous plumage device of fletching bonding on rocket body according to claim 5, it is characterised in that：The outer arcuate（611）With
The arc（612）Between also set up reinforcement（62）.
7. the viscous plumage device of fletching bonding on the rocket body according to claim any one of 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 |
|---|---|---|---|
| CN201510739141.XA CN106643335B (en) | 2015-11-04 | 2015-11-04 | The viscous plumage device of fletching bonding on rocket body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510739141.XA CN106643335B (en) | 2015-11-04 | 2015-11-04 | The viscous plumage device of fletching bonding on rocket body |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106643335A CN106643335A (en) | 2017-05-10 |
| CN106643335B true CN106643335B (en) | 2018-02-09 |
Family
ID=58850679
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510739141.XA Expired - Fee Related CN106643335B (en) | 2015-11-04 | 2015-11-04 | The viscous plumage device of fletching bonding on rocket body |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106643335B (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 CN201510739141.XA patent/CN106643335B/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 |
|---|---|
| CN106643335A (en) | 2017-05-10 |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180209 Termination date: 20191104 |
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| CF01 | Termination of patent right due to non-payment of annual fee |