CN105091664B - A kind of dynamic quantitative adjusts bow calibration method - Google Patents

A kind of dynamic quantitative adjusts bow calibration method Download PDF

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CN105091664B
CN105091664B CN201510525380.5A CN201510525380A CN105091664B CN 105091664 B CN105091664 B CN 105091664B CN 201510525380 A CN201510525380 A CN 201510525380A CN 105091664 B CN105091664 B CN 105091664B
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arrow
plane
distance
platform
adjusts
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CN105091664A (en
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忻晟
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Abstract

The present invention provides a kind of dynamic quantitative to adjust bow calibration method, and step is as follows:Bent body sets a datum mark;Plane A residing for one bent body, plane B orthogonal with plane A are provided;There is provided projection P 1 in plane B for the datum mark, position of intersecting point P2, P2 of the ray Q with arrow shaft arrow nest as starting point in free state, home for the arrow shaft and plane B ';According to distance between distance and P1 and P2 ' between P1 and P2, calculate arrow platform offset distance, be calculated by formula:According to counted exWith eyNumerical value, adjust arrow platform both horizontally and vertically deviant, make exWith eyNumerical value be zero.It is an advantage of the current invention that calibration data can be quantified, different shooter's handles can be directed to or posture is specifically changed calibration, layman can grasp at short notice, need not shoot place, simplify calibration steps.

Description

A kind of dynamic quantitative adjusts bow calibration method
Technical field
The present invention relates to the method that dynamic quantitative adjusts bow calibration altogether.
Background technology
Arrow Zhi Zuowei elongate resilient structure, when quickly being promoted by bowstring, arrow shaft is squeezed and " stock unstability " occurs, Natural resiliency attempts to recover original form again simultaneously, and therefore arrow props up after being launched until stopping this period one flown completely Directly constantly vibrate in oneself is as the vibrations plane of reference frame.And in order to improve fire accuracy further stabilized flight attitude, use It is designed to have the aerodynamic characteristics of propeller blade structure in the stabilizer " fletching " that the accurate arrow shot props up afterbody, make arrow Awing can do rapid circular movement along own axes, thus this kind of arrow prop up in flight course can by " thrust ", " vibration ", " gyroscopic procession " producing after " rotation " and rotation 4 makes a concerted effort to arrange.Therefore arrow Zhi Feihang macroscopic view becomes parabolic motion, microcosmic Become complicated spiral vibrating.
Bow as the transmitting main body propped up of arrow in the fabrication process due to the error accumulation after multiple part combination, in coupling not With purposes, the different arrow of diameter, length, quality, elasticity props up.So that the geometry of machinery center of bent body can be deviateed " in transmitting The heart ", if geometric center of only bending low replaces launching centre.Arrow prop up flight course easily occur arrow prop up swing and take aim at tool scale cannot Corresponding with shooting distance, firing dispersion was once big.So all bow-arrows for accurate shooting have to pass through " zero " to find very Positive launching centre,
And this operation must pass through serial of methods constantly groping property adjustment by professional, and eventually through penetrating Handss determine zero result after repeatedly reality is shot.After equipment is zeroed and pays, during other shooter, different shooter's handle postures differ Cause or kinestate not good it is possible to lead to be zeroed unsuccessfully, further increase debug time.
Existing three kinds of existing common methods:Static method, broken paper method, polished rod-plumage arrow method.
In said method, " static method " return-to-zero-time is the shortest low in pulling force under conditions of having professional equipment, bow and arrow equipment Basic shooting demand can be met under conditions of energy is excellent.Shortcoming is that bow and arrow equipment does not stress in debugging, is in free shape State.And " launching centre " essence that in actual shooting course, " static method " is obtained is geometry of machinery center.This position is arrow Zhi Sudu is maximum and position that will leave bowstring.Now arrow props up and obtains enough kinetic energy.Arrow platform can not constrain what arrow propped up Movement locus, and arrow propped up at the initial stage accelerating(Arrow platform, arrow nest energy stability contorting arrow prop up the critical period of movement locus)It is in Bowstring angle, arculae deformation, the maximum position of bent body stress.Because shooter can lead in the difference launching handle posture when arrow props up Launching centre deviates geometric center, leads to and actual transmission center deviation, causes flight path that arrow props up and sets up result Larger deviation occurs, is only used as zero means the most rough.
Must also be repaiied by tediously long " broken paper method " and " polished rod-plumage arrow method " for the high accuracy zero in athletics sports project Just.Because archery action differs greatly, when shooter's handle is also occurred when different from point of application when being zeroed to the point of application of bent body Deviation, or even occur completely offseting from scope and lead to be zeroed unsuccessfully.So existing tune bow method needs commissioning staff to have athlete The professional and technical personnel of rank and shooter's cooperation.The adjustment time length of a set of bow and arrow equipment and precision are with the experience of commissioning staff And proficiency level.Cannot carry out in batches being quantified with process, subjectivity is strong.
Content of the invention
For solving above-mentioned technical problem, a kind of dynamic quantitative adjusts bow calibration method, and step is as follows:
Bent body sets a datum mark;
Plane A residing for one bent body, plane B orthogonal with plane A are provided;
There is provided projection P 1 in plane B for the datum mark, arrow shaft in free state, home with arrow shaft arrow nest be The ray Q of point and position of intersecting point P2, P2 of plane B ',
According to distance between distance and P1 and P2 ' between P1 and P2, calculate arrow platform offset distance,
Described arrow platform offset distance is by following computing formula(Hereinafter referred to as " formula 1 ")Obtain
Wherein, exIt is the trunnion axis offset displacement of arrow platform, eyIt is the vertical axises offset distance of arrow platform, axIt is P2 ' P2 relatively Horizontal displacement distance, ayIt is P2 ' the vertical displacement distance of P2 relatively, BH is arrow nest and horizontal range in plane A for the nocking point, DL is shooter's tentering, and S is the distance of nocking point and plane B, and k is the vertical dimension of P2 and P2 '.
A when setting P2 ' is on the right side of P2xIt is positive number, a during left sidexIt is negative;
A when setting P2 ' is above P2yIt is positive number, a during lower sectionyIt is negative;
By axAnd aySubstitute in described computing formula, draw exWith eyNumerical value,
exThen arrow platform level adjusts > 0 to the left | ex| distance, if exThen arrow platform level adjusts to the right < 0 | ex| distance,
eyThen arrow platform adjusts > 0 vertically downward | ey| distance, if eyThen arrow platform adjusts < 0 vertically upward | ey| distance,
Repeat the step that aforementioned dynamic quantitative adjusts bow calibration method, until exWith eyIt is all 0.
Described datum mark is the bent body fiducial emitter that is spirally connected on the decoupling rod of bent body front end, and emitter can project straight line Light source;Described ray Q is to install an arrow shaft collimation emitter at arrow nest, and emitter can project the line light overlapping with arrow shaft Source.
It is an advantage of the current invention that:
1. calibration data can be quantified;
2. stress and position relationship when simulation bow, arrow are launched completely;
3. can specifically be changed calibration for different shooter's handles or posture;
4. layman can grasp at short notice;
5. place need not be shot, simplify calibration steps.
Brief description
Fig. 1 is the schematic perspective view of bow;
Fig. 2 is schematic diagram during bow and arrow free state;
Fig. 3 is schematic diagram during bow and arrow home;
Fig. 4 is free state principle schematic of the present invention;
Fig. 5 is home principle schematic of the present invention;
Fig. 6 is close-up schematic view when bent body is unloaded;
Fig. 7 is close-up schematic view when bent body is hocked the arrow;
Fig. 8 is free state arrow nest close-up schematic view;
Fig. 9 is home arrow nest close-up schematic view;
Figure 10 is that arrow nest collimates, datum mark collimates two emitters and emits beam and constitutes geometric figure on X-plane;
Figure 11 is that arrow nest collimates, datum mark collimates two emitters and emits beam and constitutes geometric figure on Y plane;
Figure 12 is subpoint P1, schematic diagram in plane B for intersection point P2 and P2 ';
Description of reference numerals:
1- arculae;2;Bent body;3- bowstring;4- arrow platform;5- bent body front end decoupling rod;6- arrow nest collimates emitter;7- bends low Fiducial emitter;A- plane A;B- plane B;Pr- arrow platform position;Pc- bent body leading portion decoupling rod screw;O- free state arrow nest position Put;O '-home arrow nest position.R- datum mark is to the ray of plane B;Q- arrow nest is to the ray of plane B;BH- arrow nest with take Horizontal range in plane A for the arrow point;DL- shooter's tentering;S- nocking point and the distance of plane B;K-P2 vertical with P2 ' away from From.
Specific embodiment
Embodiment one:
For adjusting arrow platform zero launching centre step:
1st, shown bent body reference generator 7 is threaded in bent body leading portion decoupling rod screw 5, reference generator 7 of bending low Go out coaxially conllinear with bent body leading portion decoupling rod screw 5 and in bent body plane A ray R, ray R points to apart from distance as S's Plane B.B is orthogonal with plane A for its midplane, and ray R is vertical with plane B, casts P1 in plane B;
2nd, arrow nest collimates the arrow nest O point that generator 6 is placed on bowstring 3, and the simulation arrow shaft with coupling arrow shaft profile is placed On arrow platform 4, and send the ray Q coaxially conllinear with mating arrow shaft, cast P2 to distance in plane B of S;
3rd, adjusting arrow platform horizontal level makes P1 overlap as zero original position in plane B vertical direction with P2;
4th, tuner becomes preshot preliminary activities, and bow, in not pulling open free state, makes P1,2 points of P2 is perpendicular to ground, P1 Distance to P2 is K;
5th, tuner becomes fire, by position to and keep home, delay after the relative position of measuring point P1 and point P2 ' Slow play is returned bowstring and is completed simulated gunnery action;
6th, the horizontal level making P1 and P2 ' is ax, upright position is ay- k,
A when setting P2 ' is on the right side of P2xIt is positive number, a during left sidexIt is negative;
A when setting P2 ' is above P2yIt is positive number, a during lower sectionyIt is negative;
7th, by axAnd aySubstitute into " formula 1 " respectively and calculate exWith eyNumerical value;
8、exThen arrow platform level adjusts > 0 to the left | ex| distance, if exThen arrow platform level adjusts to the right < 0 | ex| distance,
eyThen arrow platform adjusts > 0 vertically downward | ey| distance, if eyThen arrow platform adjusts < 0 vertically upward | ey| distance,
9th, after adjusting, the step of repeat step 3-7, until exWith eyIt is all 0.
(Formula 1)
In formula:
Wherein, exIt is the trunnion axis offset displacement of arrow platform, eyIt is the vertical axises offset distance of arrow platform, axIt is P2 ' P2 relatively Horizontal displacement distance, ayIt is P2 ' the vertical displacement distance of P2 relatively, BH is arrow nest and horizontal range in plane A for the nocking point, DL is shooter's tentering, and S is the distance of nocking point and plane B, and k is the vertical dimension of P2 and P2 '.
By the e obtainingxAnd eyValue adjust arrow platform, realize adjustment arrow and prop up that flight path is orthogonal with " plane B ", that is, arrow props up Parabola is done along own axes flight during flight.During equipment stress condition identical with actual shooting, arrow can be simulated and prop up transmitting State.And by penetrating itself, whether the bow and arrow equipment that really to be zeroed meets itself action can be adjusted to the grip handle point of application, simplify Adjust bow zero process.
Because Pc and Pr has a fixed range, so having one between P1 and P2 all the time apart from K, K for constant is The vertical line distance of Pc to Pr.
In order to avoid the action change when drawing for the shooter makes bent body rock the position of 2 points of disturbance records, therefore setting P1 point The displacement connection of and be regarded as reference position of bending low, so P1 and P2, P2 ' change in location only and Pr, O, O ', as long as wherein meet O, O ', the line of Pr be that ray Q is parallel with ray R, in very large range(6mm)Change the upright position of Pr and O to impact not Significantly.The tension force of arculae up and down of the archery equipment designing for precision fire can individually be adjusted, and upper and lower arculae tension force Difference can answer appreciable impact, and its relation is that upper arculae tension force enhancing P2 ' displacement is downward;Upper arculae tension force reduces P2 ' displacement upwards; Lower arculae tension force strengthens P2 ' displacement upwards;It is downward that lower arculae tension force reduces P2 ' displacement.
Embodiment two:
For laminated bow wheel group synchronous debugging step:
1st, same(" for adjusting arrow platform zero launching centre step ")1~4 in embodiment one;
2nd, the vertical displacement relation of the corresponding P2 ' of upper and lower cam set peripheral speed is that overhead cam group speed is more than lower cam set then P2 ' direction of displacement is upwards;Overhead cam group speed is less than lower cam set P2 ' direction of displacement is downward;
3rd, adjust and tighten up or loosen secondary cable;
, there is not vertical displacement to P2 ' in content in the 4th, repeating 1.
The vertical displacement of laminated bow P2 ' is mainly affected by upper and lower cam set, and upper lower whorl group controls its circle by a plurality of pair cable Circular velocity is only relevant with cam set initial position, and the tension force of the arculae up and down of laminated bow can individually voluntarily be adjusted, and it is poor that band is adjusted Different vertical displacement impact in 5% on P2 ' is not notable.
Embodiment three:
Whether reverse judgement step for after bent body and arculae stress:
With(" for adjusting arrow platform position zero launching centre step ")1~2 in embodiment one, order is less than apart from S 10m;
Adjusting arrow platform 4 horizontal level post debugging person becomes shooting to hold bow action, in not pulling open free state, makes the phase of P1 and P2 Position is overlapped in vertical direction;
Tuner becomes shooting to hold bow action, in pulling open and putting in place to emission state, records numerical value;
Change in value therein meets " formula 1 " functional relationship, then the bowstring line of O and O ' and plane A when pulling is put down OK, that is, bow and arrow equipment arculae and bent body under stress condition does not twist, in good condition, if not meeting above-mentioned relation, shows O is intersected with plane A with the line of O ', arrow prop up when being accelerated by bowstring with bend low not parallel, have side force, arrow props up flight attitude to be had Beat is inclined to.

Claims (2)

1. a kind of dynamic quantitative adjusts bow calibration method it is characterised in that step is as follows:
Bent body sets a datum mark;
Plane A residing for one bent body, plane B orthogonal with plane A are provided;
Projection P 1 in plane B for the datum mark is provided, arrow shaft in free state, home with arrow shaft arrow nest as starting point Ray Q is respectively P2, P2 with the position of intersecting point of plane B ',
According to distance between distance and P1 and P2 ' between P1 and P2, calculate arrow platform offset distance,
Described arrow platform offset distance is obtained by following computing formula:
Wherein, exIt is the trunnion axis offset displacement of arrow platform, eyIt is the vertical axises offset distance of arrow platform, axIt is the P2 ' level of P2 relatively Shift length, ayIt is P2 ' the vertical displacement distance of P2 relatively, BH is arrow nest and horizontal range in plane A for the nocking point, and DL is Shooter's tentering, S is the distance of nocking point and plane B, and k is the vertical dimension of P2 and P2 ';
A when setting P2 ' is on the right side of P2xIt is positive number, a during left sidexIt is negative;
A when setting P2 ' is above P2yIt is positive number, a during lower sectionyIt is negative;
By axAnd aySubstitute in the computing formula described in claim 1, draw exWith eyNumerical value;
exThen arrow platform level adjusts > 0 to the left | ex| distance, if exThen arrow platform level adjusts to the right < 0 | ex| distance,
eyThen arrow platform adjusts > 0 vertically downward | ey| distance, if eyThen arrow platform adjusts < 0 vertically upward | ey| distance,
After adjustment, repeat the above steps, until exWith eyIt is all 0.
2. dynamic quantitative according to claim 1 adjusts bow calibration method it is characterised in that described datum mark is before bent body Be spirally connected on the decoupling rod of end a bent body fiducial emitter, and emitter can project linear light source;Described ray Q is to install one at arrow nest Arrow shaft collimates emitter, and emitter can project the linear light source overlapping with arrow shaft.
CN201510525380.5A 2015-08-25 2015-08-25 A kind of dynamic quantitative adjusts bow calibration method Expired - Fee Related CN105091664B (en)

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4476846A (en) * 1981-07-27 1984-10-16 Carville Kenneth D Adjustable arrow support
US4993397A (en) * 1989-08-28 1991-02-19 Alfred Cryar Apparatus for calibrating archery bows
US5121736A (en) * 1991-05-14 1992-06-16 Hawk Gary L Archery bow sighting-tuning apparatus
US6366344B1 (en) * 1999-03-12 2002-04-02 Jerry W. Lach Dual beam laser sighting aid for archery bows
US6526666B1 (en) * 2001-09-21 2003-03-04 Archer's Concept's Inc. Accu-center
US8387604B1 (en) * 2009-06-07 2013-03-05 Michael Burl Terzo Compound bow

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8657709B2 (en) * 2009-04-09 2014-02-25 Clean-Shot Archery, Inc. Arrowhead with laser

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4476846A (en) * 1981-07-27 1984-10-16 Carville Kenneth D Adjustable arrow support
US4993397A (en) * 1989-08-28 1991-02-19 Alfred Cryar Apparatus for calibrating archery bows
US5121736A (en) * 1991-05-14 1992-06-16 Hawk Gary L Archery bow sighting-tuning apparatus
US6366344B1 (en) * 1999-03-12 2002-04-02 Jerry W. Lach Dual beam laser sighting aid for archery bows
US6526666B1 (en) * 2001-09-21 2003-03-04 Archer's Concept's Inc. Accu-center
US8387604B1 (en) * 2009-06-07 2013-03-05 Michael Burl Terzo Compound bow

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