CN102974084A - Method and system for processing natural feathers - Google Patents

Method and system for processing natural feathers Download PDF

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Publication number
CN102974084A
CN102974084A CN201210472126XA CN201210472126A CN102974084A CN 102974084 A CN102974084 A CN 102974084A CN 201210472126X A CN201210472126X A CN 201210472126XA CN 201210472126 A CN201210472126 A CN 201210472126A CN 102974084 A CN102974084 A CN 102974084A
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feather
natural feather
section
blade
bow
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CN102974084B (en
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戴见霖
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Priority to CN201210472126.XA priority Critical patent/CN102974084B/en
Priority to CN201810853371.2A priority patent/CN108905132A/en
Priority to CN201810853305.5A priority patent/CN111282235A/en
Priority to CN201410441121.XA priority patent/CN104208857B/en
Publication of CN102974084A publication Critical patent/CN102974084A/en
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Abstract

The invention relates to a method and a system for processing feature vanes of badminton balls by using natural feathers. The method comprises the following steps of: scanning a natural feather by a detection device to determine a series of physical parameters of the natural feather; providing a clipping model, wherein the clipping model comprises a plurality of preset parameter groups, and each preset parameter group comprises a plurality of preset parameters; comparing the series of physical parameters with the preset parameters in the preset parameter groups in the clipping model so as to match the series of physical parameters with the preset parameter groups to obtain a most appropriate parameter group; and clipping the peduncle and the wings of the natural feather by an energy flow clipping device according to the most appropriate parameter group demand, thereby obtaining a feather vane.

Description

The method and system of processing natural feather
Technical field
The present invention relates to a kind of method of processing of the natural feather for shuttlecock, particularly utilize the method for energy flow cutting feather according to preset model (shape).
The invention still further relates to a kind of system that utilizes energy flow cutting feather according to preset model (shape).
Background technology
Shuttlecock, as its name suggests, feather is the requisite part of shuttlecock.And this feather refers in particular to natural feather, more precisely, is goose feather and duck feather.But natural feather can not directly be brought the making shuttlecock, also must be processed into the feather blade.
Whether a shuttlecock is qualified, a most important criterion, and whether the uniformity that is exactly this shuttlecock is good.Shuttlecock wants the uniformity that reaches desirable, and the first element is exactly: whether the feather blade that forms this shuttlecock has good uniformity.
Because being obstructed by hair and be positioned at mao assistant of stalk both sides, the feather blade consists of, in other words, the uniformity of feather blade, any two assistant in all the feather blades (being generally 16) that refer to implant on the shuttlecock is consistent, and the hair stalk is unanimously.But, same as there not being in the world two identical leaves, there are not in the world two identical natural feathers yet.For feather blade on the shuttlecock, in full accord also need not, so-called uniformity refers to: the shape of the assistant of any two feather blades on shuttlecock, size is substantially the same, the bow of the hair stalk of any two feather blades, camber, thickness, length are substantially the same.
The shape of the assistant of any two feather blades, size are substantially the same, and the length of hair stalk is substantially the same, and this is easy to accomplish by cutting, still will make the bow of the hair stalk of any two feather blades, and camber, thickness are substantially the same, and be just very difficult.In addition, for the feather blade on the shuttlecock, the bow of hair stalk, camber, and the length three must consider simultaneously, because have certain influencing each other between this three.
In traditional shuttlecock manufacture craft, when natural feather is carried out cutting, for the ease of cutting, need to be with stretching, the pressing of described hair stalk, namely in that the hair stalk is under the interim straight state, directly feather is carried out cutting according to straight length and shape that cutting mould is default.This traditional feather cutting method exists two significant deficiency: first defective with by force stretching, the pressing of hair stalk, makes the hair stalk be in interim straightened condition when cutting.By the length that cutting mould is default the hair stalk is carried out cutting, but the hair stalk has toughness, when the bow of hair stalk not being exerted pressure after the cutting, the hair stalk can return to the state that arches under the nature, because the degree that the hair stalk of different feathers arches is different, toughness is also different, the sample attitude that feather after each processing presents comprises that the straight length at hair stalk two ends is not identical yet, this can bring very large impact to mao operation of planting of shuttlecock back, could insert bulb after needing the very large strength of flower that the feather blade is selected, otherwise can cause on a shuttlecock, the top of different feather blades is inconsistent to the height of bulb, every feather blade is away from the tip of bulb, because of bow inconsistent not on same circumference, the spacing of adjacent two feather blades is also different, can affect like this flight stability of shuttlecock; Second defective in the process that the hair stalk is flattened, can be obstructed injury to hair, the possibility that causes the hair stalk to be cut mao mould cut wound because pulling force is inconsistent exists, after the hair stalk had the feather leaf production of damage to become shuttlecock, when shuttlecock was impacted, the hair stalk wrecked easily.
In traditional shuttlecock manufacture craft, mostly can adopt the mould that is contained on the punching hair machine to cut natural feather, need the hand-held feather two ends of workman to carry out cutting to being scheduled to cut the position, the mode of this cutting relies on workman's intuition and experience substantially, especially the judgement of hair stalk rugosity, the starting point that the hair stalk cuts relies on operative employee's range estimation to be determined fully, causes cutting feather blade specification out to have larger difference; In addition, hand-held feather is difficult to also ensure that it all is to be on the same horizontal plane with cutting mould that feather is placed; Simultaneously, the hand-held feather of workman as careless slightly, is prone to accidents to the cutting knife of punching hair machine, and punching hair chance is easy to hurt workman's hand.
In addition, because need to handing the natural feather two ends, the workman carries out cutting to being scheduled to cut the position, so must respectively reserve one section quite long natural feather at the two ends of natural feather, so that the workman can firmly grip natural feather and will make punching hair machine can not hurt hand to guarantee safety, that is to say, treat that section natural feather both sides that cutting obtains have quite long natural feather can not be used for making the feather blade.An original natural feather can be made the feather blade of the different brackets more than two or three in theory, because above-mentioned reason finally may can only obtain a satisfactory feather blade.Originally just existed in the situation of resource-constrained at natural feather, this is undoubtedly a kind of very large waste.
In sum, in the traditional shuttle manufacture craft, to the processing of feather, basic rely on by hand, not only operating efficiency is low, and the feather blade that processes differs greatly, and in addition, in the course of the work, industrial accident occurs easily also.
Summary of the invention
Another object of the present invention provides and a kind of natural feather is processed into the device of the feather blade that shuttlecock uses, and it is advantageous that classification and cutting with feather.
Another object of the present invention provides and a kind of natural feather is processed into the method for the feather blade that shuttlecock uses, and it is advantageous that need not to damage in the situation of feather feather is processed.
Another object of the present invention provides a kind of method that natural feather is processed into the feather blade that shuttlecock uses, it is advantageous that and utilize scanning means, before the cutting feather, to the bow of feather hair stalk, camber, hair color, damage, feather shape, and thickness detects, and then mate suitable preset cutting mould shape and carry out cutting.
Another object of the present invention provides a kind of method that natural feather is processed into the feather blade that shuttlecock uses, need not manually to hand feather processes, feather is without stretching by force, lower fully in the raw, checkout gear scans the clear profile of hair stalk, it is advantageous that and utilize intelligentized energy flow Scissoring device, precisely at the profile along the hair stalk, both sides are cut unnecessary assistant cut totally.Efficient is improved, and the hair stalk totally and not can sustain damage in cutting process.
Another object of the present invention provides a kind of method that natural feather is processed into the feather blade that shuttlecock uses, it is advantageous that and utilize intelligentized energy flow Scissoring device, need not manually to hand feather processes, when increasing work efficiency, also avoided when the cutting feather, the workman being produced injury.
Another object of the present invention provides a kind of method that natural feather is processed into the feather blade that shuttlecock uses, it is advantageous that, feather is being added man-hour, the bow that draws after utilizing checkout gear that feather is detected, the data such as camber are classified the feather blade that is processed into automatically, thereby so that the otherness that is classified as between the of a sort feather blade reduces, final so that the feather blade of implanting on same shuttlecock has good uniformity.
Another object of the present invention provides a kind of method that natural feather is processed into the feather blade that shuttlecock uses, it is advantageous that to detect the data that feather draws is according to carrying out cutting and classification, thereby avoided as traditional processing mode, relied on too much workman's experience and the feather blade that causes processing differs greatly.
The physical parameter that another object of the present invention provides a kind of different paragraphs with natural feather detects respectively, according to the survey parameter, utilizes the energy flow of intelligence to cut, and can process at a feather feather blade of many different brackets.
To achieve these goals, the invention discloses the method for utilizing natural feather to be processed into the feather blade of shuttlecock, the method comprises the steps:
(a) by a checkout gear this natural feather is scanned, to determine the series of physical parameter of this natural feather;
(b) provide a Cutting model, this Cutting model comprises a plurality of predefined parameter groups, this predefined parameter group comprises a plurality of predefined parameters separately, these a plurality of predefined parameters in these a plurality of predefined parameter groups in this series of physical parameter and this Cutting model are compared, so that this series of physical parameter matches an only parameter group with these a plurality of predefined parameter groups; With
(c) hair of this natural feather is obstructed according to the requirement of this only parameter group by energy flow Scissoring device and assistant carries out cutting, thereby obtain this feather blade.
According to one embodiment of present invention, described series of physical parameter comprises at least one in width, camber and the bow of the color of the shape of the length of described natural feather, described assistant, described assistant, described hair stalk.
According to one embodiment of present invention, described predefined parameter comprises the width range, camber scope and the bow scope of hair stalk section of end of color, the hair stalk implantation section of the shape of the length range of the corresponding described feather blade that need to obtain by cutting, described assistant section, described assistant section.
According to one embodiment of present invention, described step (b) comprises step; By an intelligent processor the described a plurality of predefined parameters in the described a plurality of predefined parameter groups in described series of physical parameter and the described Cutting model are mated; Described step (c) comprises step: described intelligent processor starts described energy flow Scissoring device and carries out cutting with hair stalk and assistant to described natural feather.
According to one embodiment of present invention, also be used for starting described checkout gear so that described natural feather is detected at intelligent processor described in the described step (a), and collect described series of physical parameter.
According to one embodiment of present invention, described checkout gear is a kind of three-dimensional scanner, and described a plurality of predefined parameters characterize with 3-D graphic.
According to one embodiment of present invention, described checkout gear comprises a scanning element and a fixed cell, described fixed cell is used for described natural feather unsettled fixing in described scanning element, and described scanning element is used for scanning the described series of physical parameter of described natural feather.
According to one embodiment of present invention, described checkout gear comprises the combination of camber checkout gear with the bow checkout gear of two dimension of two dimension, and the method that described camber checkout gear and described bow checkout gear calculate by two dimension respectively obtains camber and the bow of described natural feather.
According to one embodiment of present invention, in described step (a), when described checkout gear detects the described hair stalk of described natural feather and described assistant damage is arranged, when being not enough to make described feather blade, stop the detection to described series of physical parameter.
According to one embodiment of present invention, after described step (c), also comprise a step: the described feather blade that will have the identical parameters group is classified as a class and collects.
According to one embodiment of present invention, in described step (c), when behind the described camber of the described hair stalk that determines described natural feather and the described bow and with described Cutting model in described optimum parameter group in described camber scope and described bow commensurate in scope after, obtain the first assistant section and the second assistant section shape separately of the hair stalk section both sides of described natural feather, then size and position carry out cutting with the energy flow Scissoring device to described natural feather.
According to one embodiment of present invention, in described method, the described hair of determining first described natural feather obstructs the point with a preset width, with as the first cutting position, along described hair stalk gradually thin direction find the described feather blade that described natural feather will be made to have the second cutting position of a predetermined length, obtain will being made in the described natural feather one section natural feather of described feather blade between described the first cutting position and described the second cutting position.
According to one embodiment of present invention, in described method, the described hair of determining first described natural feather obstructs the point with a preset width, with as the first cutting position, take the central point of described the first cutting position as the center of circle, take a length of presetting as radius, obstruct gradually thick direction along described hair and find the second cutting position, obtain will being made in the described natural feather one section natural feather of described feather blade between described the first cutting position and described the second cutting position, described default length namely is the straight length of described feather blade two-end-point.
According to one embodiment of present invention, take the central point of described the first cutting position as the center of circle, take a length of presetting as radius, along described hair stalk gradually thick/thin direction make sphere, the intersection point of the center line of described sphere and described hair stalk is the 5th intersection point, find the disc vertical with the line of the 5th intersection point with the central point of described the first cutting position at described sphere, crossing the 3rd intersection point and the 4th intersection point of obtaining of the described assistant of described disc and this section natural feather, will with the central point of described the first cutting position, a parallel plane plane at described the 3rd intersection point and described the 4th intersection point place is defined as the first plane, the plane vertical with described the first plane is defined as the second plane, the described camber that will be made into this section natural feather of described feather blade characterizes with the bending that described hair stalk produces on described the first plane, and the described bow that will be made into this section natural feather of described feather blade characterizes with the bending that described hair stalk produces on described the second plane.
According to one embodiment of present invention, in described step (a), the described camber that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: described one section natural feather is obtained one first predetermined lines to described the first plane projection, described camber represents with such camber rate, and described camber rate is the ratio of the straight length of the length of the described first predetermined lines of obtaining of projection and described feather blade two-end-point.
According to one embodiment of present invention, in described step (a), the described bow that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: described one section natural feather is obtained one second predetermined lines to described the second plane projection, described bow represents with such bow rate, and described bow rate is the ratio of the straight length of the length of the described second predetermined lines of obtaining of projection and described feather blade two-end-point.
According to one embodiment of present invention, in described step (a), the described bow that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: this section natural feather that will be made into described feather blade obtains one first predetermined lines to described the first plane projection, on the described first predetermined lines, get respectively four points, head and the tail two positions primary importance and the second place, and the 3rd position and the 4th position that are respectively adjacent to 2 of head and the tail, connect described primary importance and described the 3rd position obtains first straight line, connect the described second place and described the 4th position obtains second straight line, described the first straight line and described the second straight line intersect camber angle of formation, and the size at this camber angle is used for weighing the described camber of the hair stalk section of the described feather blade that will make.
According to one embodiment of present invention, in described step (a), the described bow that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: this section natural feather that will be made into described feather blade obtains one second predetermined lines to described the second plane projection, on the described second predetermined lines, get respectively four points, head and the tail two positions primary importance and the second place, and be respectively adjacent to head and the tail 2 and the 3rd position and the 4th position, connect described primary importance and described the 3rd position obtains one article of the 3rd straight line, connect the described second place and described the 4th position obtains one article of the 4th straight line, described the first straight line and described the second straight line intersect bow angle of formation, and the size at described bow angle is used for weighing the described bow of the hair stalk section of the described feather blade that will make.
According to one embodiment of present invention, in described step (a), the described bow that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: this section natural feather that will be made into described feather blade obtains second a predetermined curve bar to described the second plane projection, on the described second predetermined lines, get respectively two points, head and the tail two positions primary importance and the second place, and the projection on described the second plane of the point of this section natural feather bow maximum obtains the 3rd position, connect described primary importance and described the 3rd position obtains one article of the 5th straight line, connect described primary importance and the described second place and obtain one article of the 6th straight line, described the 5th straight line and described the 6th straight line intersect bow angle of formation, and the size at described bow angle is used for weighing the described bow of the hair stalk section of the described feather blade that will make.
According to one embodiment of present invention, in described step (a), the described camber that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: will be made into this section natural feather of described feather blade to described the first plane projection, head and the tail 2 points that connect the projection of this section natural feather, obtain the first lines, and have on the point of the first cutting position of described preset width and the described one section natural feather towards described hair stalk gradually thin/thick direction the point of a vicinity is arranged, connect at these 2 and obtain second lines, the angle between described the first lines and described the second lines is used for characterizing the camber of the described feather blade that will make.
According to one embodiment of present invention, in described step (a), the described camber that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: will be made into this section natural feather of described feather blade to described the second plane projection, head and the tail 2 points that connect the projection of this section natural feather, obtain the first lines, and have on the point of the first cutting position of described preset width and the described one section natural feather towards described hair stalk gradually thin/thick direction the point of a vicinity is arranged, connect at these 2 and obtain second lines, the angle between described the first lines and described the second lines is used for characterizing the bow of the described feather blade that will make.
The described bow that according to one embodiment of present invention, will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: the described hair stalk between the described first cutting position of this section natural feather and described the second cutting position along the front or the ratio of the physical length of the center line at the back side and the length of the described feather blade that will make be used for characterizing described camber; Described hair stalk between the described first cutting position of this section natural feather and described the second cutting position is used for characterizing described bow along the ratio of the physical length of the center line of assistant hair tonic face and the length of the described feather blade that will make.
Correspondingly, the invention provides a kind of system that carries out said method, this system comprises;
A checkout gear is to scan and to obtain the series of physical parameter of this natural feather to this natural feather;
A Cutting model, it stores a plurality of parameter group that comprise one group of predefined parameter;
An energy flow Scissoring device is to be used for that hair stalk and the assistant of this natural feather are carried out cutting;
With an intelligent processor, this intelligent processor operationally is connected with this Cutting model and this energy flow Scissoring device, this series of physical parameter that this checkout gear is obtained and this group predefined parameter in this Cutting model compare to match an only parameter group, then this intelligent processor starts this energy flow Scissoring device, this natural feather is cut into this feather blade of this group predefined parameter with this only parameter group.
Below, will be further described by specific embodiment, yet embodiment only is giving an example of alternative embodiment of the present invention that its disclosed feature only is used for explanation and sets forth technical scheme of the present invention, the protection domain that is not intended to limit the present invention.
Description of drawings
Figure 1A is the structural representation of the camber of a feather of signal.
Figure 1B is the structural representation of the bow of a feather of signal.
The natural feather that Fig. 2 illustrates according to a preferred embodiment of the present invention is processed into the schematic diagram that the feather blade also further is processed into shuttlecock.
Fig. 3 illustrates the schematic diagram according to the 3-D scanning of the natural feather of above preferred embodiment of the present invention.
Fig. 4 illustrates the schematic diagram according to the natural feather system of processing of above preferred embodiment of the present invention.
Fig. 5 illustrates the schematic diagram according to the stalk of the cutting hair in the natural feather processing technology of above preferred embodiment of the present invention step.
Fig. 6 illustrates the schematic diagram according to the cutting assistant step in the natural feather processing technology of above preferred embodiment of the present invention.
Fig. 7 A illustrates according to the hair stalk cutting position of definite natural feather of second preferred embodiment of the present invention schematic diagram with the step of the feather blade that obtains predetermined length
Fig. 7 B illustrates the schematic diagram according to the step of the camber of definite feather blade of second preferred embodiment of the present invention.
Fig. 7 C illustrates the schematic diagram according to the step of the bow of definite feather blade of above-mentioned second preferred embodiment of the present invention.
Fig. 8 A illustrates the schematic diagram according to the step of the camber of definite feather blade of the 3rd preferred embodiment of the present invention.
Fig. 8 B illustrates the schematic diagram according to the step of the bow of definite feather blade of above-mentioned the 3rd preferred embodiment of the present invention.
Fig. 8 C illustrates the schematic diagram according to the step of the bow of definite feather blade of the distortion embodiment of above-mentioned the 3rd preferred embodiment of the present invention.
Fig. 9 A illustrates the schematic diagram according to the step of the camber of definite feather blade of the 4th preferred embodiment of the present invention.
Fig. 9 B illustrates the schematic diagram according to the step of the bow of definite feather blade of above-mentioned the 4th preferred embodiment of the present invention.
Figure 10 illustrates the schematic diagram of the step of the camber of definite feather blade of above-mentioned the 5th preferred embodiment according to the present invention and bow.
Figure 11 illustrates according to the hair stalk cutting position of definite natural feather of the 6th preferred embodiment of the present invention schematic diagram with the step of the feather blade that obtains predetermined length.。
Figure 12 illustrates the structural representation of the shuttlecock that natural feather according to a preferred embodiment of the invention is made into.
Figure 13 illustrates the structural representation of the traditional shuttle that natural feather according to a preferred embodiment of the invention is made into.
Figure 14 illustrates the schematic flow sheet according to the natural feather processing method of first preferred embodiment of the present invention.
The specific embodiment
According to claim of the present invention and the disclosed content of specification, technical scheme of the present invention literary composition specific as follows is described.
In order more to clearly demonstrate, to the bow of feather, camber defines first for we.
Shown in Figure 1A and Figure 1B is a crude natural feather 10, be generally goose feather or duck feather, it comprises the assistant 12 on hair stalk 11 and hair stalk 11 both sides, hair stalk 11 has four faces, we are defined as positive 10a with it, back side 10b, left side 10c and right side 10d, wherein, we will have the left side 10c of assistant 12 hair tonics and right side 10d to be referred to as assistant hair tonic face.Hair stalk 11 more level and smooth one sides are called positive 10a, and hair stalk 11 significantly outside outstanding one side is called back side 10a.Along the left side 10c of described mao of stalk 11 in assistant hair tonic face or the bending of right side 10d direction generation, be defined as camber, hair stalk 11 as shown in Figure 1B, is defined as bow along the bendings of positive 10a or the generation of back side 10b direction.Can say that also described camber is the bending that described hair stalk 11 occurs at horizontal plane, described bow is the bending that described hair stalk 11 occurs at vertical plane.
In Figure 1A and 1B, the x axle, the y axle, the z axle can represent respectively three directions in the three-dimensional system of coordinate, the skew that the hair stalk 11 that camber refers to natural feather 10 produces on the direction on the plane at x axle and y axle place, and the skew that the hair stalk 11 that bow refers to natural feather 10 produces on the direction on the plane at x axle and z axle place.
A natural feather 10 can be cut at least one feather blade 100, and typically, a natural feather 10 can be cut into two feather blades 100, and the feather blade 100 that obtains will be for making a shuttlecock 1000, as shown in Figure 2.Wherein, after natural feather 10 is processed to feather blade 100, will have roughly the same predetermined length, width, many feather blades 100 of camber and bow etc. are picked out and are made shuttlecock 1000.That is to say, in order to guarantee the uniformity of shuttlecock 1000, must guarantee the uniformity of the physical parameter of feather blade 100.
As shown in Figure 2, a natural feather 10 with hair stalk 11 and assistant 12 is cut into the feather blade 100 with mao stalk section 110 and assistant section 120, the hair stalk section 110 of one end of feather blade 100 is formed with an implantation section 111, to be used for implanting the locating slot that holds of a feather implanted device, this feather implanted device comprises at least a bulb and forms other necessary parts of a shuttlecock.The both sides of these implantation section 111 parts do not have assistant.Feather blade 100 is cut into the width W of implantation section 111 ends that have predetermined length L and be scheduled to.In Fig. 2, this length L refers to the axial distance along x, and this width W refers to the axial distance along y.In general, this length L and this width W determine that according to actual needs for example in a typical example, length L is 47mm, and width W is 2.1mm.As shown in Figure 2, the implantation section 111 of feather blade 100 also can be cut into has predetermined length, and this need to further determine according to the concrete structure of the degree of depth of implanting and this feather implanted device.That is to say that in certain embodiments, implantation section 111 can be an implant head with short length, its needs can be implanted corresponding this and hold locating slot and get final product.And in other embodiment, implantation section 111 has long length, and its end is used for implanting corresponding this and holds locating slot, and other part is fastened with retaining elements such as reinforcements in a shuttlecock 1000.
As Fig. 3 to Figure 6 shows that according to a preferred embodiment of the present invention be processed into the schematic diagram of feather blade 100 from natural feather 10.In this preferred embodiment, at first 30 pairs of described feathers 10 of intelligent processor 20 checkout gears of startup detect, as shown in Figure 3, system according to feather processing of the present invention, in a three-dimensional detection model, can draw length, width, bow, the camber of the hair stalk 11 of feather, and the data such as the width of assistant 12, shape and color.Underproof feather namely is detected in this step, and for example assistant 12 has damage or hair stalk 11 that damage is arranged.The color of assistant 12 determines afterwards that after testing whether needing bleaching process etc., the natural feather 10 that color is close can be classified as a class collects.
Intelligent processor 20 and a Cutting model 40 link, and Cutting model 40 is comprised of several parameter group, and each parameter group is comprised of a plurality of parameters.The width range 42 of the end of these parameters such as the length range 41 that can comprise the feather blade 100 that need to obtain by cutting, hair stalk implantation section 111, camber scope 43 and bow scope 44, the shape 45 of assistant section and the color 46 of assistant section etc. of hair stalk section 110, every parameter has predetermined scope, then these data analysis of the natural feather 10 that checkout gear 30 is obtained, if these data drop in certain parameter group in the existing pre-determined model, then carry out cutting natural feather 10 according to the requirement of this parameter group.
It is worth mentioning that the value range of the parameters in each parameter group is to determine according to actual needs, so can go as required natural feather 10 is cut into required feather blade 100.Also can according to the actual conditions of natural feather 10, by this step it be classified as that class that is fit to cutting.
As shown in Figure 4, this system also comprises an energy flow Scissoring device 50, after intelligent processor 20 compares the parameters in a plurality of parameter group of the data of natural feather 10 and the Cutting model 40 of default feather blade, then Auto-matching goes out the with it parameter group of immediate the sort of Cutting model 40, then intelligent processor 20 sends instruction to energy flow Scissoring device 50, described energy flow Scissoring device 50 will carry out cutting to described feather 10 according to the data of described feather leaf model, forms at last the feather blade 100 that approaches with corresponding Cutting model.This energy flow can be laser or other high-pressure fluids such as water.In the present embodiment, energy flow Scissoring device 50 is laser cutting machines.
Be the schematic diagram of cutting hair stalk 11 as shown in Figure 5, after having chosen suitable cutting position, carry out cutting along predetermined cutting position, obtain having the feather blade 100 of the terminal width W of predetermined length L and implantation section 111.It is worth mentioning that the predetermined length L does not here refer to mao length of stalk section 110, because hair stalk section 110 is that certain bending is arranged, in the present embodiment, predetermined length L refers to axial length.These two parameters determine than being easier in threedimensional model, only need to scan on each site of hair stalk 11 of natural feather 10 width with and the length of crossing in the axial direction get final product.As shown in FIG., the cutting in this step only need to determine that two cutting positions at feather blade 100 head and the tail two ends get final product.
The schematic diagram of cutting assistant 12 as shown in Figure 6, before cutting assistant 12, need to determine camber and the bow of natural feather 10, when 30 pairs of natural feathers of In service inspection device 10 carry out 3-D scanning, preferably make the positive 10a of natural feather 10 all facing one direction, certainly, checkout gear 30 also can be designed to distinguish positive back side 10a and the 10b of natural feather 10.The assistant section 120 of feather blade 100 comprises the first assistant section 121 and the second assistant section 122 that lays respectively at mao stalk section 110 both sides, the camber that determines the feather blade and bow and with Cutting model 40 in a certain parameter group coupling after, obtain the first assistant section 121 and the second assistant section 122 shape separately, cutting is carried out with energy flow Scissoring device 50 in size and position then.
It is worth mentioning that the terminal width W place of implantation section 111 that is to say the position of natural feather 10 initial crop, finding width W at natural feather 10 is that the position of predetermined value such as 2.1mm is relatively to be easy to.The predetermined length L of feather blade 100 determines easily.Determine that natural feather 10 can make the feather blade 100 of which kind of type, prior parameter is its camber and bow.In Cutting model 40, camber scope 43 and the bow scope 44 of hair stalk 110 can be the data that quantize, such as angle.Also can be a series of 3-D graphic, these 3-D graphic be by scanning the taxonomy database of a large amount of natural feather 10 and the corresponding feather blade 100 rear foundation that make.In use, only the natural feather 10 of actual measurement need to be compared with the figure in the Cutting model 40 and get final product.The camber scope 43 of hair stalk 110 and bow scope 44 are further can specifically describe in the example exposure below of the data that quantize.
As shown in figure 14, according to this preferred embodiment of the present invention, the method that natural feather 10 is processed into the feather blade 100 of shuttlecock 1000 comprises the steps:
(a) scan by 30 pairs of natural feathers 10 of a checkout gear, to determine the series of physical parameter of natural feather 10;
(b) a plurality of predefined parameters in a plurality of predefined parameter groups in this serial physical parameter and the Cutting model 40 are compared, so that this serial physical parameter matches an only parameter group with these a plurality of predefined parameter groups; With
(c) according to the requirement of this only parameter group natural feather 10 is carried out cutting by an energy flow Scissoring device 50, thereby obtain feather blade 100.
The feather blade 100 with identical parameters group according to above-mentioned steps obtains can automatically be placed to together.That is to say that described method also comprises step: the feather blade 100 that will have the identical parameters group is sorted out collection.
Correspondingly, in step (a), this serial physical parameter includes but not limited to the length of natural feather 10, the width of hair stalk 11, and hair obstructs 11 camber, and the bow of hair stalk 11, can certainly comprise the shape of assistant 12, size, color and luster etc.
In step (b), these a plurality of predefined parameters include but not limited to the width range 42, camber scope 43 and the bow scope 44 of hair stalk 110 of end of length range 41, the hair stalk implantation section 111 of the feather blade 100 that obtains by cutting.Shape 45 and the color 46 that can also comprise the assistant section of feather blade 100.
These a plurality of predefined parameter groups are distinguished correspondence requirement to dissimilar feather blades 100 in the manufacturing process of the shuttlecock 1000 of reality.In step (c), natural feather 10 is cut at least one (such as two) shape, size, the feather blade 100 that size is suitable.That is to say that natural feather is cut into has appropriate length L, implantation section 111 terminal width W, hair stalk section 110 cambers, and the feather blade of hair stalk section 120 bows.
Certainly, in step (c), also comprise the cutting to the assistant 12 of natural feather 10, to obtain the assistant section 120 of feather blade 100.The assistant section 120 of feather blade 100 comprises that the first assistant section 121 and 122, the first assistant sections 121 of the second assistant section that are positioned at mao stalk section 110 both sides can have different shapes, size and area with the second assistant section 122.For example, one of them has more flat shape, and another has relatively narrow thin shape.
It is worth mentioning that, in step (a), also comprise the step that natural feather 10 is fixed, that is to say that checkout gear 30 can be a three-dimensional scanner, it comprises a scanning element 31 and a fixed cell 32, natural feather 10 is fixed in the scanning element 31 by a fixed cell 32, thereby detects its parameters in scanning element 31.In an example, the hair stalk 11 of natural feather 10 is held so that natural feather 10 unsettled placements, thereby can detect natural feather 10 from all directions.
In addition, in the method, can be by 20 pairs of detecting steps of an intelligent processor (a), coupling step (b), and the operation of cutting step (c) is controlled.That is to say, intelligent processor 20 operationally with checkout gear 30, Cutting model 40, energy flow Scissoring device 50 is connected, thereby to send the operational order startup and to close checkout gear 30, carry out comparing with every physical parameter of the natural feather 10 of measuring and mating according to the parameter group of Cutting model 40, thereby and the hair stalk 10 of 50 pairs of feathers 10 of operating energy stream Scissoring device and assistant 12 carry out cutting and obtain having suitable hair stalk section 110 and the feather blade 100 of assistant section 120.It is worth mentioning that above-mentioned each step also can be to be arranged on the streamline, each step is furnished with separately central processing unit and operates, and mutually can transmission of information between these central processing units, such as various parameter informations and operational order.
Shown in Fig. 4 is the system that carries out said method, and correspondingly, this system comprises;
A checkout gear 30 is to scan and to obtain the series of physical parameter of natural feather to natural feather 10;
A Cutting model 40, it stores a plurality of parameter group that comprise one group of predefined parameter;
An energy flow Scissoring device 50 is to be used for that hair stalk 11 and the assistant 12 of natural feather 10 are carried out cutting;
With an intelligent processor 20, intelligent processor 20 operationally is connected with Cutting model 40 and energy flow Scissoring device 50, this serial physical parameter that checkout gear 30 is obtained and this group predefined parameter in the Cutting model 40 compare to match an only parameter group, then intelligent processor 20 starts energy flow Scissoring device 50, natural feather 10 is cut into the feather blade 100 of this group predefined parameter with this only parameter group.
Intelligent processor 20 can also operationally be connected with checkout gear 30, starting and to close checkout gear 30, and if necessary, adjust the angle of checkout gear 30, from different directions natural feather 10 is scanned, to obtain the full detail of natural feather 10.
Checkout gear 30 comprises a scanning element 31 and a fixed cell 32, and fixed cell 32 is used for natural feather 10 is fixed on scanning element 31, and fixing mode so that scanning element 31 can scan and detect natural feather 10 in all directions.
Such as Fig. 7 A, shown in 7B and the 7C, according to second preferred embodiment of the present invention, parameters in the Cutting model 40 can be the data that quantize, that is to say that the length range 41 of feather blade 100, the width range 42 that hair obstructs the end of implantation section 111, camber scope 43 and the bow scope 44 of hair stalk 110 all are the number ranges of determining, rather than represent with the solid figure of one group of three-dimensional.Certainly in the above embodiments, the numerical value also determined of these parameters.It is worth mentioning that the camber of the hair stalk 11 of natural feather 10 and bow detect respectively and finished by bending detector and the bow survey device of two dimension.That is to say, finish the detection of physical parameter and determine by the combination of the checkout gear of two two dimensions.
Shown in Fig. 7 A, find first the hair of natural feather 10 to obstruct the position of a preset width W on 11, for example this preset width is 2.1mm, so just determined the first cutting position A1 on the natural feather 10, then from this first cutting position A1, obtain a predetermined length L, in Fig. 7 A, find in the following method cutting position A2.Take the central point of the first cutting position A1 as the center of circle, take default length L as radius, towards hair stalk 11 gradually thin direction find the crosspoint, be the second cutting position A2, the distance between the two cutting positions is L, for example L can be 47mm.Between them this section natural feather 10 will be made a feather blade 100 in subsequent step.It is worth mentioning that the physical length of the hair stalk 11 that this predetermined length L does not refer to is because hair stalk 11 is crooked.Certainly, in other Cutting model 40, the physical length that may use feather blade 100 is used as determining the parameter of cutting scheme.After having determined these two cutting position A1 and A2, intelligent processor 20 operating energies stream Scissoring device 50 gets off this section natural feather 10 cutting from the whole natural feather 10 along these two cutting position A1 and A2, to be used for following process.
Shown in Fig. 7 A and 7B, the camber of this section natural feather 10 determines that by the following method camber refers to the bending that occurs on the plane P direction..This plane defines and illustrates by following method.As shown in FIG., take the central point of the first cutting position A1 as the center of circle, take default length L 2 as radius, towards hair stalk 11 gradually thin direction make sphere, this sphere is the 5th intersection point A5 with the intersection point of the center line of hair stalk 11, find the disc vertical with the line of the 5th intersection point A5 with the central point of the first cutting position A1 at this sphere, the assistant of this disc and this section natural feather 10 12 intersects and obtains the 3rd intersection point A3, and the 4th intersection point A4.A3 and A4 lay respectively at the both sides of hair stalk 11, the central point of described the first cutting position A1, form a plane P with the 3rd intersection point A3 and the 4th intersection point A4, will be made into this section natural feather 10 of feather blade 100 to plane P or first plane P 1 projection parallel with plane P, projection obtains one first predetermined lines, and its length is S1.This moment, feather blade 100 camber represented with such camber rate, and this camber rate is the ratio of the length L of the length S1 of the described first predetermined lines of obtaining of projection and feather blade 100.
Shown in Fig. 7 C, the bow of this section natural feather 10 determines by the following method, and in three-dimensional system of coordinate, camber refers to the bending that occurs in x axle and z axial plane direction.As shown in FIG., will be made into this section natural feather 10 of feather blade 100 to the vertical plane P2 projection of the first plane P 1, and obtain one second predetermined lines, its length is S2.This moment, feather blade 100 bow represented with such bow rate, and this bow rate is the ratio of the length L of the length S2 of these the second predetermined lines of obtaining of projection and feather blade 100.It is worth mentioning that in above-mentioned testing process, these natural feathers 10 all are sent to checkout gear 30 towards a direction, for example positive 10a up.
After obtaining the camber and bow that represents with camber rate and bow rate respectively, intelligent processor 20 is analyzed this camber and this bow, with with Cutting model 40 in parameter group in corresponding camber scope 43 and bow scope 44 compare to match an only parameter group, thereby this section feather 10 sorted out and in follow-up cutting step, carried out cutting by an energy flow Scissoring device 50 according to this only parameter group.
Be depicted as according to the 3rd preferred embodiment of the present invention such as Fig. 8 A and 8B, after in similar above-mentioned the second embodiment, obtaining one section natural feather 10 for the preparation of feather blade 100, shown in Fig. 8 A, this section natural feather 10 that will be made into feather blade 100 obtains the described first predetermined lines to 1 projection of the first plane P, on these first predetermined lines, get respectively four points, head and the tail two positions primary importance M1 and second place M2, and the 3rd position M3 and the 4th position M4 that are respectively adjacent to 2 M1 of head and the tail and M2, connect primary importance M1 and the 3rd position M3 and obtain first straight line, connect second place M2 and the 4th position M4 and obtain second straight line, this first straight line and the second straight line intersect camber α of formation, and this angle [alpha] namely is used for weighing the camber of the hair stalk section 110 of the feather blade 100 that will make.
Shown in Fig. 8 B, this section natural feather 10 that will be made into feather blade 100 obtains the described second predetermined lines to 2 projections of the second plane P, on these second predetermined lines, get respectively four points, head and the tail two positions primary importance N1 and second place N2, and the 3rd position N3 and the 4th position N4 that are respectively adjacent to 2 N1 of head and the tail and N2, connect primary importance N1 and the 3rd position N3 and obtain one article of the 3rd straight line, connect second place N2 and the 4th position N4 and obtain one article of the 4th straight line, the 3rd straight line and the 4th straight line intersect bow angle β of formation, and this angle beta namely is used for weighing the bow of the hair stalk section 110 of the feather blade 100 that will make.
Be depicted as according to the 4th preferred embodiment of the present invention such as Fig. 9 A and 9B, after in similar above-mentioned the second embodiment, obtaining one section natural feather 10 for the preparation of feather blade 100, shown in Fig. 9 A, will be made into this section natural feather 10 of feather blade 100 to 1 projection of the first plane P, the head and the tail O1 and O2 2 points that connect the projection of the feather blade 100 that this section natural feather 10 namely will make, obtain first lines, and preset width is the point that a vicinity is arranged towards hair stalk 11 thinner directions on the point of W and the natural feather 10, for example some projection on this plane of contiguous 1～5mm obtains two some O1, O3, connect at these 2 and obtain second lines, angle ε between described the first lines and described the second lines, the camber of the feather blade 100 that will make exactly.
Shown in Fig. 9 B, this section natural feather 10 that will be made into feather blade 100 connects head and the tail O1 ' and O2 ' 2 points of the projection of the feather blade 100 that this section natural feather 10 namely will make to plane P 2 projections, obtain first lines, and preset width is the point that a vicinity is arranged towards hair stalk 11 thinner directions on the point of W and the natural feather 10, for example some projection on this plane of contiguous 1～5mm obtains two some O1 ', O3 ', connect at these 2 and obtain second lines, angle γ between described the first lines and described the second lines, the camber of the feather blade 100 that will make exactly.It is worth mentioning that this contiguous some O3 ' also can be that this section natural feather 10 reaches that of maximum bow place.
In addition, being worth one, what say is as shown in figure 10, the camber of feather blade 100 also can represent with such bow rate, this bow rate is the ratio along the length L of the physical length L1 of the center line of assistant hair tonic face 10c or 10d and feather blade 100 of the hair stalk 11 between two cutting positions of this section natural feather 10, the camber of feather blade 100 also can represent with such camber rate, and this camber rate is the ratio along the length L of the physical length L2 of positive 10a or back side 10b and feather blade 100 of the hair stalk 11 between two cutting positions of this section natural feather 10.
Be the method according to the processing natural feather 10 of the 6th preferred embodiment of the present invention as shown in figure 11.Shown in Figure 10 A, finding preset width at natural feather 10 first is the position of W, to be defined as the first cutting position B1.Then, also can find in the following method cutting position B2.Take the central point of the first cutting position B1 as the center of circle, take default length L as radius, towards hair stalk 11 gradually thick direction find the crosspoint, be the second cutting position B2.That is to say that in this preferred embodiment, the length of the feather blade 100 that will make determines that with said method this default length L namely is considered as the length of feather blade 100.
That is to say, when a natural feather 10 is used to be made into feather blade 100, pass through first above-mentioned detecting step, to obtain its physical parameter, and then with Cutting model 40 in parameter group in parameters compare, so that it is sorted out, then according to the requirement of the predefined parameter group that is referred to natural feather 10 is carried out cutting, to obtain suitable feather blade 100.
It is worth mentioning that, the criterion of this camber and bow can have other mode, three kinds of methods of this that enumerate among the present invention are only as example, those skilled in the art it will also be appreciated that the parameter with other characterizes this camber and bow, but these embodiments that are equal to all should be included within the design of the present invention.
As shown in figure 12, the shuttlecock 1000 that the feather blade 100 that processing method according to the present invention makes is made, shuttlecock 1000 can have the structure of the shuttlecock of any use natural feather, as an example, in the present invention, shuttlecock 1000 comprises 100, one bulbs 1100 of many feather blades, and one is planted mao frame 1200.Bulb 1100 with plant mao frame 1200 and be connected, plant mao frame 1200 and comprise a plurality of mao bars 1210 of planting, each is planted and is provided with an accommodating locating slot 1220, the accommodating locating slot 1220 of every feather blade 100 implanted correspondences on mao bar 1210.The structure of shuttlecock 1000 is in the applicant's formerly Chinese patent application 200910044168.1,201010226568.7,201110028436.8, and crossed exposure in 201110418724.4, the full content of these patents mode by reference all merges in this application.
As shown in figure 13, the shuttlecock 1000 that the feather blade 100 that processing method according to the present invention makes is made, shuttlecock 1000 also can be made traditional two-part shuttlecock 1000, and namely described feather blade 100 is directly installed on the bulb 1100, and plants mao frame 1200 in the middle of not having.
To should be mentioned that especially in the present invention, the method for utilizing natural feather 10 to make feather blade 100 has the incomparable advantage of conventional method.The manufacturing process of feather blade 100 in the past is mainly by manual, rely on intuition and experience to finish, in the present invention, the cutting of natural feather 10 can rely on mass production by machines fully, and the uniformity of feather blade 100 that can guarantee shuttlecock 1000 is very high, this will improve the quality of shuttlecock 1000 widely, and enhance productivity, and reduce production costs.
And natural feather 10 is in the cutting process, and clamping and cutting process rely on machine to carry out, and so just can not occur can hurting the problem of workman's hand in the traditional shuttle manufacturing process.And, obtain in the process of feather blade 100 natural feather 10 cuttings, correspondence on this root natural feather 10 treats that section natural feather both sides of the feather blade 100 that cutting obtains do not need to reserve one section extra natural feather to be used for workman's gripping, so also just eliminated in the traditional handicraft waste to natural feather.Adopt method of cutting out of the present invention, a natural feather 10 can obtain two feather blades 100 with comparalive ease, and even can obtain the feather blade 100 of three or more different brackets.The different brackets here is according to the length of the hair stalk section 110 of feather blade 100, width, and bow, the shape of camber and assistant section 120, size, the parameters such as color and luster are sorted out.
Foregoing be specific embodiments of the invention for example, for the wherein not equipment of detailed description and structure, should be understood to take the existing common apparatus in this area and universal method to be implemented.
The above embodiment of the present invention for the usefulness of explanation technical solution of the present invention, is enumerating of technical solution of the present invention only only simultaneously, is not limited to technical scheme of the present invention and protection domain thereof.Adopt equivalent technologies means, equivalent apparatus etc. the improvement of claims of the present invention and the disclosed technical scheme of specification be will be understood that it is not exceed claims of the present invention and the disclosed scope of specification.

Claims (31)

1. method of utilizing natural feather to be processed into the feather blade of shuttlecock, the method comprises the steps:
(a) by at least one checkout gear described natural feather is detected, to determine the series of physical parameter of described natural feather;
(b) provide a Cutting model, described Cutting model comprises a plurality of predefined parameter groups, described predefined parameter group comprises a plurality of predefined parameters separately, described a plurality of predefined parameters in described a plurality of predefined parameter groups in described series of physical parameter and the described Cutting model are compared, so that described series of physical parameter and described a plurality of predefined parameter group match an only parameter group; With
(c) according to the requirement of described only parameter group hair stalk and the assistant of described natural feather carried out cutting by an energy flow Scissoring device, thereby obtain described feather blade.
2. the method for claim 1 is characterized in that, described series of physical parameter comprises at least one in width, camber and the bow of the color of the shape of the length of described natural feather, described assistant, described assistant, described hair stalk.
3. method as claimed in claim 2, it is characterized in that described predefined parameter comprises the width range, camber scope and the bow scope of hair stalk section of end of color, the hair stalk implantation section of the shape of the length range of the corresponding described feather blade that need to obtain by cutting, described assistant section, described assistant section.
4. the method for claim 1 is characterized in that, described step (b) comprises step; By an intelligent processor the described a plurality of predefined parameters in the described a plurality of predefined parameter groups in described series of physical parameter and the described Cutting model are mated; Described step (c) comprises step: described intelligent processor starts described energy flow Scissoring device and carries out cutting with hair stalk and assistant to described natural feather.
5. method as claimed in claim 4 is characterized in that, also is used for starting described checkout gear so that described natural feather is detected at intelligent processor described in the described step (a), and collects described series of physical parameter.
6. such as arbitrary described method in the claim 1 to 5, it is characterized in that described checkout gear is a kind of three-dimensional scanner, described a plurality of predefined parameters characterize with 3-D graphic.
7. method as claimed in claim 6, it is characterized in that, described checkout gear comprises a scanning element and a fixed cell, described fixed cell is used for described natural feather unsettled fixing in described scanning element, and described scanning element is used for scanning the described series of physical parameter of described natural feather.
8. such as arbitrary described method in the claim 1 to 5, it is characterized in that, described checkout gear comprises the combination of camber checkout gear with the bow checkout gear of two dimension of two dimension, and the method that described camber checkout gear and described bow checkout gear calculate by two dimension respectively obtains camber and the bow of described natural feather.
9. the method for claim 1, it is characterized in that, in described step (a), when described checkout gear detects the described hair stalk of described natural feather and described assistant damage is arranged, when being not enough to make described feather blade, stop the detection to described series of physical parameter.
10. the method for claim 1 is characterized in that, after described step (c), also comprises a step: the described feather blade that will have the identical parameters group is classified as a class and collects.
11. method as claimed in claim 3, it is characterized in that, in described step (c), when behind the described camber of the described hair stalk that determines described natural feather and the described bow and with described Cutting model in described optimum parameter group in described camber scope and described bow commensurate in scope after, obtain the first assistant section and the second assistant section shape separately of the hair stalk section both sides of described natural feather, then size and position carry out cutting with the energy flow Scissoring device to described natural feather.
12. method as claimed in claim 3, it is characterized in that, in described method, the described hair of determining first described natural feather obstructs the point with a preset width, with as the first cutting position, along described hair stalk gradually thin direction find the described feather blade that described natural feather will be made to have the second cutting position of a predetermined length, obtain will being made in the described natural feather one section natural feather of described feather blade between described the first cutting position and described the second cutting position.
13. method as claimed in claim 3, it is characterized in that, in described method, the described hair of determining first described natural feather obstructs the point with a preset width, with as the first cutting position, take the central point of described the first cutting position as the center of circle, take a length of presetting as radius, obstruct gradually thick direction along described hair and find the second cutting position, obtain will being made in the described natural feather that section natural feather of described feather blade between described the first cutting position and described the second cutting position, described default length namely is the straight length of described feather blade two-end-point.
14. such as claim 12 or 13 described methods, it is characterized in that, take the central point of described the first cutting position as the center of circle, take a length of presetting as radius, along described hair stalk gradually thick/thin direction make sphere, the intersection point of the center line between described sphere and described hair described the first cutting position of stalk and described the second cutting position is the 5th intersection point, described sphere find with the central point of described the first cutting position and the 5th intersection point be connected the vertical disc of straight line, crossing the 3rd intersection point and the 4th intersection point of obtaining of the described assistant in the both sides of described disc and this section natural feather, will with the central point of described the first cutting position, a parallel plane plane at described the 3rd intersection point and described the 4th intersection point place is defined as the first plane, the plane vertical with described the first plane is defined as the second plane, the described camber that will be made into this section natural feather of described feather blade characterizes with the bending that described hair stalk produces on described the first plane, and the described bow that will be made into this section natural feather of described feather blade characterizes with the bending that described hair stalk produces on described the second plane.
15. method as claimed in claim 14, it is characterized in that, in described step (a), the described camber that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: described one section natural feather is obtained one first predetermined lines to described the first plane projection, described camber represents with such camber rate, and described camber rate is the ratio of the straight length of the length of the described first predetermined lines of obtaining of projection and described feather blade two-end-point.
16. method as claimed in claim 14, it is characterized in that, in described step (a), the described bow that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: described one section natural feather is obtained one second predetermined lines to described the second plane projection, described bow represents with such bow rate, and described bow rate is the ratio of the straight length of the length of the described second predetermined lines of obtaining of projection and described feather blade two-end-point.
17. method as claimed in claim 14, it is characterized in that, in described step (a), the described bow that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: this section natural feather that will be made into described feather blade obtains one first predetermined lines to described the first plane projection, on the described first predetermined lines, get respectively four points, head and the tail two positions primary importance and the second place, and the 3rd position and the 4th position that are respectively adjacent to 2 of head and the tail, connect described primary importance and described the 3rd position obtains first straight line, connect the described second place and described the 4th position obtains second straight line, described the first straight line and described the second straight line intersect camber angle of formation, and the size at this camber angle is used for weighing the described camber of the hair stalk section of the described feather blade that will make.
18. method as claimed in claim 14, it is characterized in that, in described step (a), the described bow that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: this section natural feather that will be made into described feather blade obtains one second predetermined lines to described the second plane projection, on the described second predetermined lines, get respectively four points, head and the tail two positions primary importance and the second place, and be respectively adjacent to head and the tail 2 and the 3rd position and the 4th position, connect described primary importance and described the 3rd position obtains one article of the 3rd straight line, connect the described second place and described the 4th position obtains one article of the 4th straight line, described the first straight line and described the second straight line intersect bow angle of formation, and the size at described bow angle is used for weighing the described bow of the hair stalk section of the described feather blade that will make.
19. method as claimed in claim 14, it is characterized in that, in described step (a), the described bow that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: this section natural feather that will be made into described feather blade obtains second a predetermined curve bar to described the second plane projection, on the described second predetermined lines, get respectively two points, head and the tail two positions primary importance and the second place, and the projection on described the second plane of the point of this section natural feather bow maximum obtains the 3rd position, connect described primary importance and described the 3rd position obtains one article of the 5th straight line, connect described primary importance and the described second place and obtain one article of the 6th straight line, described the 5th straight line and described the 6th straight line intersect bow angle of formation, and the size at described bow angle is used for weighing the described bow of the hair stalk section of the described feather blade that will make.
20. method as claimed in claim 14, it is characterized in that, in described step (a), the described camber that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: will be made into this section natural feather of described feather blade to described the first plane projection, head and the tail 2 points that connect the projection of this section natural feather, obtain the first lines, and have on the point of the first cutting position of described preset width and the described one section natural feather towards described hair stalk gradually thin/thick direction the point of a vicinity is arranged, connect at these 2 and obtain second lines, the angle between described the first lines and described the second lines is used for characterizing the camber of the described feather blade that will make.
21. method as claimed in claim 14, it is characterized in that, in described step (a), the described camber that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: will be made into this section natural feather of described feather blade to described the second plane projection, head and the tail 2 points that connect the projection of this section natural feather, obtain the first lines, and have on the point of the first cutting position of described preset width and the described one section natural feather towards described hair stalk gradually thin/thick direction the point of a vicinity is arranged, connect at these 2 and obtain second lines, the angle between described the first lines and described the second lines is used for characterizing the bow of the described feather blade that will make.
22. method as claimed in claim 14, it is characterized in that the described bow that will be made into one section natural feather of described feather blade in the described natural feather is determined by the following method: the described hair stalk between the described first cutting position of this section natural feather and described the second cutting position along the front or the ratio of the physical length of the center line at the back side and the length of the described feather blade that will make be used for characterizing described camber; Described hair stalk between the described first cutting position of this section natural feather and described the second cutting position is used for characterizing described bow along the ratio of the physical length of the center line of assistant hair tonic face and the length of the described feather blade that will make.
23. method as claimed in claim 6 is characterized in that, in described method, a described natural feather is made the described feather blade that obtains at least two different brackets.
24. method as claimed in claim 7 is characterized in that, in described method, a described natural feather is made and is obtained at least three described feather blades.
25. one kind is processed into the system of the feather blade of shuttlecock with natural feather, described system comprises;
A checkout gear is to scan and to obtain the series of physical parameter of described natural feather to described natural feather;
A Cutting model, it stores a plurality of parameter group that comprise one group of predefined parameter;
An energy flow Scissoring device is to be used for that hair stalk and the assistant of described natural feather are carried out cutting; With
An intelligent processor, described intelligent processor operationally is connected with described Cutting model and described energy flow Scissoring device, the described series of physical parameter that described checkout gear is obtained and described group of predefined parameter in the described Cutting model compare to match an only parameter group, then described intelligent processor starts described energy flow Scissoring device, described natural feather is cut into the described feather blade of described group of predefined parameter with described only parameter group.
26. system as claimed in claim 25 is characterized in that, described checkout gear is a kind of three-dimensional scanner, and described a plurality of predefined parameters characterize with 3-D graphic.
27. system as claimed in claim 26, it is characterized in that, described checkout gear comprises a scanning element and a fixed cell, described fixed cell is used for described natural feather unsettled fixing in described scanning element, and described scanning element is used for scanning the described series of physical parameter of described natural feather.
28. system as claimed in claim 25, it is characterized in that, described checkout gear comprises the combination of camber checkout gear with the bow checkout gear of two dimension of two dimension, and the method that described camber checkout gear and described bow checkout gear calculate by two dimension respectively obtains camber and the bow of described natural feather.
29. system as claimed in claim 25 is characterized in that, described series of physical parameter comprises at least one in width, camber and the bow of the color of the shape of the length of described natural feather, described assistant, described assistant, described hair stalk.
30. system as claimed in claim 29, it is characterized in that described predefined parameter comprises the width range, camber scope and the bow scope of hair stalk section of end of color, the hair stalk implantation section of the shape of the assistant section of the length range of the corresponding described feather blade that need to obtain by cutting, described feather blade, described assistant section.
31. system as claimed in claim 25 is characterized in that, described intelligent processor also is used for starting described checkout gear so that described natural feather is detected, and collects described series of physical parameter.
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CN201810853305.5A CN111282235A (en) 2012-11-20 2012-11-20 Method and system for processing natural feather
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104436593A (en) * 2013-09-12 2015-03-25 戴见霖 Intelligent processing system and method for feather pieces of shuttlecock
WO2017044671A1 (en) * 2015-09-09 2017-03-16 Anand Syam Prasad Modifying natural feathers for use in sporting goods
CN110743146A (en) * 2019-11-12 2020-02-04 亚顿国际有限公司 Plastic feather piece of badminton

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101703833A (en) * 2009-08-21 2010-05-12 戴见霖 Badminton
CN201871202U (en) * 2009-12-08 2011-06-22 戴见霖 Shuttlecock blade
JP2011218093A (en) * 2010-04-14 2011-11-04 Nanshin Kagaku Kogyo Kk Shuttlecock for badminton, feather for shuttlecock, and method for manufacturing the same
CN202920928U (en) * 2012-11-20 2013-05-08 戴见霖 System for processing natural feathers

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101530661B (en) * 2008-03-11 2011-01-26 张文广 Special man-made feather for badminton and badminton made thereby
JP5170459B2 (en) * 2009-08-18 2013-03-27 美津濃株式会社 Artificial feather for shuttlecock, shuttlecock for badminton, and manufacturing method thereof
JP5661535B2 (en) * 2011-03-30 2015-01-28 美津濃株式会社 Artificial feather for shuttlecock, shuttlecock for badminton, and manufacturing method thereof
CN102294114A (en) * 2011-06-23 2011-12-28 吴志刚 Artificial feather
CN202460028U (en) * 2012-02-09 2012-10-03 美津浓株式会社 Artificial feather for shuttlecock and shuttlecock for badminton
CN202490402U (en) * 2012-02-09 2012-10-17 美津浓株式会社 Artificial feather for shuttlecock and shuttlecock for badminton
CN109806562A (en) * 2012-08-11 2019-05-28 安徽三才体育用品有限公司 A kind of manufacturing method of shuttlecock

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101703833A (en) * 2009-08-21 2010-05-12 戴见霖 Badminton
CN201871202U (en) * 2009-12-08 2011-06-22 戴见霖 Shuttlecock blade
JP2011218093A (en) * 2010-04-14 2011-11-04 Nanshin Kagaku Kogyo Kk Shuttlecock for badminton, feather for shuttlecock, and method for manufacturing the same
CN202920928U (en) * 2012-11-20 2013-05-08 戴见霖 System for processing natural feathers

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104436593A (en) * 2013-09-12 2015-03-25 戴见霖 Intelligent processing system and method for feather pieces of shuttlecock
CN104436593B (en) * 2013-09-12 2019-05-07 戴见霖 A kind of slice of shuttlecock intelligent machining system and method
WO2017044671A1 (en) * 2015-09-09 2017-03-16 Anand Syam Prasad Modifying natural feathers for use in sporting goods
CN108136254A (en) * 2015-09-09 2018-06-08 沙姆·普拉萨德·阿南德 It is modified to the natural feather used in sports goods
JP2018534005A (en) * 2015-09-09 2018-11-22 シャム プラサド アナンドＡＮＡＮＤ， Ｓｙａｍ Ｐｒａｓａｄ Modification of natural feathers for use in exercise equipment
US10240284B2 (en) 2015-09-09 2019-03-26 Syam Anand Modifying natural feathers for use in sporting goods
US10415180B2 (en) 2015-09-09 2019-09-17 Syam Anand Modifying natural feathers for use in sporting goods
US11332880B2 (en) 2015-09-09 2022-05-17 Durabird Modifying natural feathers for use in sporting goods
CN110743146A (en) * 2019-11-12 2020-02-04 亚顿国际有限公司 Plastic feather piece of badminton

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