CN106643335A

CN106643335A - Feather adhering device for adhering arrow feather on arrow body

Info

Publication number: CN106643335A
Application number: CN201510739141.XA
Authority: CN
Inventors: 朱秀琴
Original assignee: Individual
Current assignee: Individual
Priority date: 2015-11-04
Filing date: 2015-11-04
Publication date: 2017-05-10
Anticipated expiration: 2035-11-04
Also published as: CN106643335B

Abstract

The invention discloses a feather adhering device for adhering arrow feather on an arrow body. The feature adhering device comprises a C type-like frame; the C type-like frame consists of a top surface, a side surface and a bottom surface, the top surface and the side surface of the C type-like frame are hinged, a chassis is machined on the bottom surface of the C type-like frame, a base is fixedly arranged on the chassis, a tail insertion hole is arranged in the chassis and the base in an integral through manner, the base is provided with a clamping component, the clamping component is formed by fixedly connecting two elastic clamping devices with the same structure and a cylindrical frame arranged between the two elastic clamping devices, an axial first arrow hole is formed in the central position of the clamping component and a second arrow hole consistent with the first arrow hole is formed in the top surface of the C type-like frame. The feather adhering device is simple in structure, low in manufacturing cost, convenient to carry, good in stability, wide in use range and high in adhering efficiency.

Description

The viscous plumage device of fletching bonding on rocket body

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 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 viscous plumage device of fletching bonding 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 viscous plumage device of fletching bonding 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, clamp assemblies are set on the base, the 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 axial barbican is provided with the clamp assemblies center, and it is provided with second barbican consistent with first arrow on the top surface of the class c-type framework.

Further, the cylindrical frame is the cylindrical structural surrounded by three structure identical sector solid framework structures, and notch is formed between fan-shaped solid framework described in each two.

Further, it is marked with scale in the described 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, and gap is formed between fan-shaped framework described in each two.

Further, each described fan-shaped framework is by outer arcuate, arc and is connected to the two sides composition of the outer arcuate and the arc side between, and fletching perforation is formed between the adjacent arc side of each two.

Further, it is fixedly connected with return facilities on each described side, the return facilities is by some springs and is connected to the spring plate group of spring outwards into and fletching holes for clamping being formed 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 socket with the circular trough.

The invention has the beneficial effects as follows：First, the present invention is capable of achieving the fletching in three directions on rocket body while bonding, improves bonding efficiency using the clamp assemblies of three-dimensional one by the clamp assemblies of three-dimensional one；Secondly, elastic clamp device is set, fletching is capable of achieving by elastic clamp device and is quickly fixed before bonding, and elastic clamp device can also realize the viscous plumage to different arrow kinds, expand its use range；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 further marked with scale on fan-shaped solid framework, it is ensured that the quick positioning of fletching during viscous plumage, and the accuracy of bonding location.

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- sides, 62- reinforcements, 63- return facilitieses, 631- spring leafs, 632- springs, the perforation of 7- fletchings, 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.

Embodiment：Referring to the drawings the viscous plumage device of fletching bonding on a kind of rocket body shown in 1-5, 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, clamp assemblies are set on the base 3, the clamp assemblies are formed by fixedly connecting by two structure identical elastic clamp devices 6 and the cylindrical frame 5 between two elastic clamp devices 6, the elastic clamp device 6 is correspondingly arranged at the top and bottom position of cylindrical frame 5, the first axial barbican 10 is provided with the clamp assemblies center, and it is provided with second barbican 12 consistent with first barbican 10 on the top surface of the class c-type framework.

In the present invention, the cylindrical frame 5 is the cylindrical structural surrounded by three structure identical sector structures of solid framework 51, notch 52 is formed between fan-shaped solid framework 51 described in each two, in the described fan-shaped solid framework 51 positioned at the both sides of the notch 52 scale is marked with, scale is vertically marked.

In the present invention, the elastic clamp device 6 is the cylindrical structural surrounded by three structure identical sector frameworks 61, fan-shaped framework 61 and the fan-shaped shape of solid framework 51, structure is identical, the inside of fan-shaped framework 61 is hollow-core construction, the design of hollow-core construction is to mitigate weight, material-saving, gap 11 is formed described in each two between fan-shaped framework 61, the correspondence notch 52 of gap 11, each described fan-shaped framework 61 is by outer arcuate 611, arc 612 and two sides 613 being connected between the outer arcuate 611 and the side of the arc 612 edge constitute, reinforcement 62 is also set up between the outer arcuate 611 and the arc 612, the setting of reinforcement 62 can increase the intensity of fan-shaped framework 61, three arcs 612 form first barbican 10, fletching perforation 7 is formed between the adjacent side of the arc 612 of each two, return facilities 63 is fixedly connected with each described side 613, the return facilities 63 is by some springs 632 and is connected to the spring leaf 631 of spring outwards and constitutes, and fletching holes for clamping 8 is formed between two opposite return facilitieses 63, the setting of spring leaf 631 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, ensure the accuracy of fletching bonding angle.

Elastic clamp device 6 is separately positioned on the upper and lower ends of cylindrical frame 5 in the present invention, purpose is easy for fixing the bottom and upper end of viscous plumage position, only reserve specifically viscous plumage position quickly being glued plumage, at the viscous plumage position that the design of notch 52 is just able to make the glue for gluing plumage quickly be squeezed on rocket body 9.

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 clamp 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

1. fletching bonding use glues plumage device 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 clamp assemblies, the clamp assemblies are by two structure identical elastic clamp devices（6）And located at two elastic clamp devices（6）Between cylindrical frame（5）It is formed by fixedly connecting, in the clamp assemblies 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 use glues plumage device on a kind of rocket body according to claim 1, it is characterised in that：The cylindrical frame（5）It is by three structure identical sector solid frameworks（51）The cylindrical structural that structure is surrounded, fan-shaped solid framework described in each two（51）Between form notch（52）.

3. fletching bonding use glues plumage device on a kind of rocket body according to claim 2, it is characterised in that：Positioned at the notch（52）The described fan-shaped solid framework on both sides（51）It is marked with scale.

4. fletching bonding use glues plumage device on a kind of 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 for surrounding, fan-shaped framework described in each two（61）Between form gap（11）.

5. fletching bonding use glues plumage device on a kind of rocket body according to claim 4, it is characterised in that：Each described fan-shaped framework（61）By outer arcuate（611）, arc（612）And it is connected to the outer arcuate（611）With the arc（612）Two sides of the side between（613）Composition, the adjacent arc of each two（612）Fletching perforation is formed between side（7）.

6. fletching bonding use glues plumage device on a kind of rocket body according to claim 5, it is characterised in that：Each described side（613）On be fixedly connected with return facilities（63）, the return facilities（63）By some springs（632）And it is connected to the spring leaf of spring outwards（631）Composition, and two opposite return facilitieses（63）Between formed fletching holes for clamping（8）.

7. fletching bonding use glues plumage device on a kind of rocket body according to claim 4, it is characterised in that：The outer arcuate（611）With the arc（612）Between also set up reinforcement（62）.

8. fletching bonding use glues plumage device on a kind of rocket body according to any one of claim 1-7, 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.