CN103302162A - Mould positioning method based on feature distance - Google Patents

Mould positioning method based on feature distance Download PDF

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CN103302162A
CN103302162A CN2013102364915A CN201310236491A CN103302162A CN 103302162 A CN103302162 A CN 103302162A CN 2013102364915 A CN2013102364915 A CN 2013102364915A CN 201310236491 A CN201310236491 A CN 201310236491A CN 103302162 A CN103302162 A CN 103302162A
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mold
clamp
equipment
mould
coordinate
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CN103302162B (en
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彭静文
万敏
李卫东
张乐
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Beihang University
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Abstract

一种基于特征距离的模具定位方法,该方法有五大步骤如下:一:模具初始摆放(1)放置垫块,(2)放置模具;二:运动设备(1)确定坐标,(2)设备反解,(3)驱动设备;三:测量计算(1)距离测量,(2)几何计算;四:模具定位计算;五:修正数控代码进行拉形。该方法根据ACB FET系列数控横拉机的设备特点,利用夹钳位置反解拉形机运动参数,驱动设备运动,利用夹钳特征点与模具特征点的距离,计算模具特征点的坐标与空间位置,再根据模具位置,重新设计拉形数控代码,实现精确的蒙皮拉形。该方法制定的模具摆放流程,能够增大模具摆放的误差冗余,减少模具摆放时间和定位工装使用,提高飞机蒙皮拉形生产效率。

Figure 201310236491

A mold positioning method based on characteristic distance, the method has five major steps as follows: 1: Initial placement of the mold (1) place the block, (2) place the mold; 2: move the equipment (1) determine the coordinates, (2) equipment Anti-solution, (3) drive equipment; three: measurement calculation (1) distance measurement, (2) geometric calculation; four: mold positioning calculation; five: correct NC code for drawing. According to the equipment characteristics of the ACB FET series CNC horizontal drawing machine, the method uses the position of the clamp to reverse the motion parameters of the drawing machine to drive the equipment to move, and uses the distance between the clamp feature point and the mold feature point to calculate the coordinates and space of the mold feature point Position, and then according to the position of the mold, redesign the drawing CNC code to achieve accurate skin drawing. The mold placement process formulated by the method can increase the error redundancy of the mold placement, reduce the mold placement time and the use of positioning tooling, and improve the production efficiency of aircraft skin drawing.

Figure 201310236491

Description

一种基于特征距离的模具定位方法A Die Positioning Method Based on Feature Distance

(一)技术领域(1) Technical field

本发明涉及一种飞机蒙皮零件在拉伸成形过程中确定模具摆放位置的定位方法。特别涉及使用ACB FET系列的数控拉伸成形机在进行横向拉伸成形前模具摆放位置的定位方法。属于航空飞机制造技术领域。The invention relates to a positioning method for determining the placing position of a mold in the stretch forming process of an aircraft skin part. In particular, it involves the positioning method of the mold placement position before transverse stretch forming using the CNC stretch forming machine of the ACB FET series. The invention belongs to the technical field of aviation aircraft manufacturing.

(二)背景技术(2) Background technology

蒙皮零件是构成和维持飞机气动外形的外表零件。拉伸成形(简称拉形)是一种有模具的包覆成形的工艺方法,是飞机蒙皮类零件成形的主要成形方式之一。拉形通过设备夹钳将毛料的两边夹紧,利用模具和夹钳的运动,使毛料产生不均匀的拉伸变形而包覆模具使毛料与模具贴合。Skin parts are exterior parts that form and maintain the aerodynamic shape of an aircraft. Stretch forming (referred to as stretch forming) is a process method of overmolding with a mold, and it is one of the main forming methods for forming aircraft skin parts. The two sides of the wool are clamped by the clamp of the equipment, and the movement of the mold and the clamp is used to make the wool produce uneven stretching deformation, and the mold is covered to make the wool and the mold fit.

拉形的工艺参数主要有毛料的延伸率和夹钳的包覆角度,通过工艺参数与拉形模具的实际形状,计算得到夹钳的运动轨迹(如图1)。ACB FET系列数控拉形机是法国ACB GEC ALSTHOM公司生产的横向拉形机,该系列拉形机的结构相似,按照吨位分为FET400、FET600、FET1200等。采用数控拉形机进行蒙皮拉形,利用设备对夹钳运动轨迹的精确控制,实现精确的成形过程。飞机蒙皮拉形模具的尺寸从十几厘米到十几米,大型的蒙皮零件的拉形模具重量也多达百吨。对于大型的拉形模具安装,通常是用行吊将模具吊起,再由多人同时辅助将模具安装到拉形设备指定位置进行生产。要将模具放置到预先设置的位置常常需要进行多次放置和微调,安装也经常持续数小时,而且最终的摆放位置也存在较大偏差。模具摆放位置的不确定性,成为影响蒙皮成形质量的不确定因素,从而影响蒙皮拉形的成形精度。因此需要一种快速定位模具的方法来定位模具实际摆放位置,并针对当时模具摆放位置,修正工艺参数和数控代码,使夹钳运动轨迹符合实际情况,使拉形过程更加准确,保证零件成形质量。The process parameters of the drawing mainly include the elongation of the wool and the cladding angle of the clamp. Through the process parameters and the actual shape of the drawing die, the movement track of the clamp is calculated (as shown in Figure 1). ACB FET series CNC stretching machine is a horizontal stretching machine produced by ACB GEC ALSTHOM in France. The structure of this series of stretching machines is similar. According to the tonnage, it is divided into FET400, FET600, FET1200 and so on. The skin stretching is carried out by the numerical control stretching machine, and the precise control of the movement track of the clamp by the equipment is used to realize the precise forming process. The size of the aircraft skin stretching die ranges from a dozen centimeters to more than a dozen meters, and the weight of the stretching die for large skin parts is as much as 100 tons. For the installation of large-scale drawing molds, the mold is usually lifted by a crane, and then multiple people assist to install the mold to the designated position of the drawing equipment for production. Getting molds into pre-set positions often required multiple placements and fine-tuning, setups often lasted hours, and final placements varied widely. The uncertainty of the placement of the mold becomes an uncertain factor affecting the quality of skin forming, thereby affecting the forming accuracy of skin stretching. Therefore, a method for quickly locating the mold is needed to locate the actual position of the mold, and according to the position of the mold at that time, correct the process parameters and numerical control codes, so that the movement track of the clamp conforms to the actual situation, making the drawing process more accurate, and ensuring the quality of the parts Forming quality.

(三)发明内容(3) Contents of the invention

1、目的:1. Purpose:

本发明的目的是提供一种基于特征距离的模具定位方法。该方法根据数控拉形设备的特点,利用夹钳上特征点的精确坐标,测量与模具上特征点的相对距离,确定模具摆放的位置误差,对设备加工数控代码进行修正,提高成形的准确性和零件的质量。The purpose of the present invention is to provide a mold positioning method based on characteristic distance. According to the characteristics of the CNC drawing equipment, the method uses the precise coordinates of the feature points on the clamp to measure the relative distance to the feature points on the mold, determines the position error of the mold, corrects the CNC code for equipment processing, and improves the accuracy of forming. and the quality of parts.

2、技术方案:2. Technical solution:

本发明一种基于特征距离的模具定位方法,其步骤如下:A kind of mold positioning method based on characteristic distance of the present invention, its steps are as follows:

步骤一:模具初始摆放Step 1: Initial Mold Placement

蒙皮零件拉伸成形模具的初始摆放是将实际模具放置在拉形设备的坐标系中,是进行模具定位测量和拉形过程的准备工作,如图2所示;The initial placement of the stretch forming mold for skin parts is to place the actual mold in the coordinate system of the stretching equipment, which is the preparation for the positioning measurement of the mold and the stretching process, as shown in Figure 2;

在工厂的实际生产过程中,模具摆放在标准垫块上,与垫块一同放置在拉形设备的坐标系中。标准垫块是工厂自制的标准件,按高度和垫块所能承的模具重量进行区分。模具初始摆放首先根据蒙皮拉形模具外形尺寸和质量,选择标准垫块;然后按照工厂工艺规程摆放垫块和模具,测量垫块顶面水平度,确保垫块放置水平。记录垫块高度H与模具特征点距模具底面高度h。In the actual production process of the factory, the mold is placed on the standard block, and placed together with the block in the coordinate system of the drawing equipment. The standard block is a standard part made by the factory, which is distinguished by the height and the weight of the mold that the block can bear. The initial placement of the mold first selects the standard block according to the outer dimension and quality of the skin pulling mold; then places the block and the mold according to the factory process regulations, and measures the levelness of the top surface of the block to ensure that the block is placed horizontally. Record the height H of the pad and the height h between the feature point of the mold and the bottom surface of the mold.

步骤二:运动设备Step Two: Sports Equipment

运动设备是将ACB FET系列横拉机的设备夹钳运动到指定位置,使夹钳特征点与模具特征点处于是同一水平面内,便于距离测量。The moving equipment is to move the equipment clamp of ACB FET series horizontal drawing machine to the designated position, so that the clamp feature point and the mold feature point are in the same horizontal plane, which is convenient for distance measurement.

(1)确定坐标(1) Determine the coordinates

确定夹钳特征点在测量时所在的坐标位置,由垫块的高度与模具特征点距模具底面的距离,确定模具特征点所在水平面的高度(Z坐标);通过模具的外形尺寸和理论摆放的空间位置,确定夹钳特征点在X轴上的位置(X坐标);根据夹钳特征点在夹钳上的位置,能得到夹钳特征点的Y坐标,如图3所示;Determine the coordinate position of the clamp feature point during measurement, and determine the height (Z coordinate) of the horizontal plane where the mold feature point is located based on the height of the pad and the distance between the mold feature point and the bottom surface of the mold; through the external dimension of the mold and the theoretical placement Determine the position of the clamp feature point on the X axis (X coordinate); according to the position of the clamp feature point on the clamp, the Y coordinate of the clamp feature point can be obtained, as shown in Figure 3;

(2)设备反解(2) Device anti-solution

ACB FET系列横拉机的运动反解是通过夹钳特征点的坐标位置,根据拉形设备的机构特点求解出并联机构上各个作动筒的长度,即设备的运动参数。ACBFET系列数控横拉机主要用于飞机蒙皮零件横拉成形,拉形机的外形如图4所示;该设备呈左右对称结构,每侧一个直钳口夹钳,两个横向作动筒,两个纵向作动筒,组成两对四杆并联机构,机构简图如图5所示;夹钳的空间位置与姿态由四个作动筒的伸长共同确定;进行定位测量时,为了简化运动反解的计算过程,设定夹钳轴线与Y轴平行,因此只需计算夹钳在ZX平面内的位置,即只需计算Z作动筒和A作动筒的伸长量,如图6所示;The motion inverse solution of the ACB FET series horizontal drawing machine is to solve the length of each actuator on the parallel mechanism, that is, the motion parameters of the equipment, through the coordinate position of the clamp feature point and according to the mechanical characteristics of the drawing equipment. ACBFET series CNC horizontal drawing machine is mainly used for horizontal drawing forming of aircraft skin parts. , two longitudinal actuating cylinders form two pairs of four-bar parallel mechanisms. Simplify the calculation process of the motion inverse solution, set the axis of the clamp to be parallel to the Y axis, so only need to calculate the position of the clamp in the ZX plane, that is, only need to calculate the elongation of the Z actuator and the A actuator, such as As shown in Figure 6;

(3)驱动设备(3) Drive equipment

将ACB FET系列横拉机反解得到的拉形机各个作动筒的伸长量,输入数控横拉机控制系统界面驱动设备运动,使夹钳运动到指定位置,用于进行距离测量。The elongation of each actuator of the stretching machine obtained by reverse analysis of the ACB FET series horizontal stretching machine is input into the interface of the CNC horizontal stretching machine control system to drive the equipment to move, so that the clamp moves to the designated position for distance measurement.

步骤三:测量计算Step 3: Measure and calculate

测量过程是测量夹钳各个特征点到模具各特征点的距离,然后经过几何计算,得到特征点的坐标。The measurement process is to measure the distance from each feature point of the clamp to each feature point of the mold, and then obtain the coordinates of the feature points through geometric calculation.

(1)距离测量(1) Distance measurement

在左侧(X为负的一侧)、右侧(X为正的一侧)两个夹钳上分别标记两个特征点,记为PL1、PL2和PR1、PR2;在模具上标记两个特征点,记为TL和TR。分别测量PL1、PL2到TL的距离和PR1、PR2到TR的距离,如图7所示。由于普通的测量方法,如卷尺、长绳等,误差较大,采取更高精度的测量手段进行测量,如三坐标测量仪、激光跟踪仪等,能够提高模具定位精度;Mark two feature points on the two clamps on the left side (the side where X is negative) and the right side (where X is positive), which are denoted as P L1 , P L2 and P R1 , P R2 ; Mark two feature points on , denoted as T L and T R . Measure the distances from P L1 and P L2 to T L and the distances from P R1 and P R2 to T R respectively, as shown in Fig. 7 . Due to the large error of common measurement methods, such as tape measure, long rope, etc., the use of higher precision measurement methods, such as three-coordinate measuring instrument, laser tracker, etc., can improve the mold positioning accuracy;

(2)几何计算(2) Geometric calculation

在步骤二驱动设备运动之后,夹钳上特征点与模具特征点处于同一高度的水平面内,因此模具定位计算可利用平面几何的求解方法,计算模具特征点的坐标,如图8所示。After step 2 drives the equipment to move, the feature points on the clamp and the feature points of the mold are in the horizontal plane at the same height, so the mold positioning calculation can use the solution method of plane geometry to calculate the coordinates of the feature points of the mold, as shown in Figure 8.

由图8看出,以左侧为例,模具特征点TL的具体坐标可由以PL1为圆心,LL1为半径的圆与以PL2为圆心,LL2为半径的圆的交点确定,同理可以确定右侧模具特征点TR的具体坐标。It can be seen from Figure 8 that, taking the left side as an example, the specific coordinates of the mold feature point T L can be determined by the intersection of a circle with P L1 as the center and L L1 as the radius and a circle with P L2 as the center and L L2 as the radius. Similarly, the specific coordinates of the right mold feature point T R can be determined.

步骤四:模具定位计算Step 4: Die positioning calculation

通过测量计算得到的模具特征点的具体坐标,与模具特征点理论坐标进行比较计算,得出模具顶面垫块放置平面内的平移向量与转动角度,如图9所示。The specific coordinates of the mold feature points obtained through measurement and calculation are compared and calculated with the theoretical coordinates of the mold feature points, and the translation vector and rotation angle in the plane where the pad block on the top surface of the mold is placed are obtained, as shown in Figure 9.

步骤五:修正数控代码进行拉形Step 5: Correct the NC code for drawing

由步骤四计算得到的变换参数,将理论模具变换到实际模具摆放位置,以新的模具位置为基准,应用工艺参数生成与实际模具位置相符的设备数控代码。将拉形设备数控代码输入ACB FET横向拉形机,对拉形机进行空载运行,检查设备运动是否与所设计的工艺参数相符。检查无误后,进行蒙皮拉形。From the transformation parameters calculated in step 4, the theoretical mold is transformed into the actual mold placement position, and the new mold position is used as the benchmark, and the process parameters are applied to generate the equipment CNC code that matches the actual mold position. Input the CNC code of the drawing equipment into the ACB FET horizontal drawing machine, run the drawing machine with no load, and check whether the movement of the equipment is consistent with the designed process parameters. After the check is correct, carry out skin pulling.

通过上述五个步骤,实现拉形模具空间位置的快速定位。通过模具实际位置来修正拉形轨迹的方法,让蒙皮零件的拉伸成形过程符合实际情况,使因模具摆放位置偏差对零件成形精度的影响得以小,减少了定位工装的使用,保证飞机蒙皮零件生产的精度。Through the above five steps, the rapid positioning of the spatial position of the drawing die is realized. The method of correcting the stretching track through the actual position of the mold makes the stretching forming process of the skin part conform to the actual situation, so that the influence of the deviation of the mold placement on the forming accuracy of the part is minimized, the use of positioning tools is reduced, and the aircraft is guaranteed The precision with which skinned parts are produced.

其中,步骤二中所述的通过夹钳特征点的坐标求解设备运动参数的方法,利用设备机构特点与数控拉形设备的精确控制能力,实现了通过夹钳运动轨迹生成数控代码,对拉形过程进行精确控制。Among them, the method of solving the motion parameters of the equipment through the coordinates of the feature points of the clamps described in step 2 uses the characteristics of the equipment mechanism and the precise control ability of the CNC drawing equipment to realize the generation of CNC codes through the movement trajectory of the clamps. The process is precisely controlled.

其中,步骤三中所述的测量特征点间距离来确定模具特征点位置的方法,通过简单的测量和几何计算,实现模具空间位置确定。该方法简单实用,便于实施。Wherein, the method for determining the position of the feature point of the mold by measuring the distance between the feature points described in step 3 realizes the determination of the spatial position of the mold through simple measurement and geometric calculation. The method is simple, practical and easy to implement.

3、优点及功效:3. Advantages and effects:

本发明基于数控拉形设备的一种飞机蒙皮拉形模具定位方法,是根据数控拉形机的特点,通过拉形机的运动参数得到夹钳特征点的坐标,测量夹钳特征点与模具特征点的距离,计算得到模具特征点的坐标对模具摆放位置进行修正,再根据修正后的模具位置,按工艺参数重新设计拉形数控代码,以实现精确的蒙皮拉伸成形。本方法制定了飞机蒙皮拉形生产过程中的模具摆放流程,增大了模具摆放的误差冗余,减少模具摆放时间和定位工装的使用,提高了飞机蒙皮拉形生产效率;并通过测量对模具位置进行修正,使数控代码更符合当前情况,能够提高蒙皮零件的成形质量,降低废品率,使蒙皮横向拉形更易于实现数字化生产。The present invention is based on the positioning method of a kind of aircraft skin stretching mold of numerical control stretching equipment, is according to the characteristic of numerical control stretching machine, obtains the coordinate of clamp characteristic point through the movement parameter of stretching machine, measures clamp characteristic point and mold The distance of the feature points is calculated to obtain the coordinates of the feature points of the mold to correct the position of the mold, and then according to the corrected mold position, redesign the stretching CNC code according to the process parameters to achieve accurate skin stretching. This method formulates the mold placement process in the aircraft skin stretching production process, increases the error redundancy of the mold placement, reduces the mold placement time and the use of positioning tooling, and improves the aircraft skin stretching production efficiency; And the position of the mold is corrected by measurement, so that the NC code is more in line with the current situation, which can improve the forming quality of the skin parts, reduce the scrap rate, and make the horizontal stretching of the skin easier to realize digital production.

(四)附图说明(4) Description of drawings

图1蒙皮拉形加载过程简图Fig.1 Schematic diagram of skin tensile loading process

图2模具放置示意图Figure 2 Schematic diagram of mold placement

图3夹钳运动位置示意图Figure 3 Schematic diagram of clamp movement position

图4ACB FET系列数控横拉机外形示意图Figure 4 Outline schematic diagram of ACB FET series CNC horizontal drawing machine

图5ACB FET设备一侧机构简图Figure 5. Diagram of the mechanism on one side of the ACB FET device

图6ACB FET设备反解示意图Figure 6 ACB FET device reverse solution schematic diagram

图7特征点位置及尺寸测量示意图Figure 7 Schematic diagram of feature point position and size measurement

图8模具定位特征点位置计算示意图Figure 8 Schematic diagram of calculating the position of the mold positioning feature points

图9模具定位变换计算示意图Figure 9 Schematic Diagram of Die Positioning Transformation Calculation

图10本发明所述方法流程图Fig. 10 method flow chart of the present invention

图中符号说明如下:The symbols in the figure are explained as follows:

O:设备坐标系原点X:设备坐标系X轴  Y:设备坐标系Y轴  Z:设备坐标系Z轴TL:模具左侧特征点(X负方向一侧)TR:模具右侧特征点(X正方向一侧)h:模具特征点到模具底面距离H:垫块高度PL:左侧夹钳特征点(X负方向一侧)PR:右侧夹钳特征点(X正方向一侧)W:模具宽度D:夹钳与模具间距A0:A0关节点A:A关节点Y0:Y0关节点Y:Y关节点Z0:Z0关节点Z:Z关节点Z:Z关节点X0:X0关节点X:X关节点X:X关节点OZA:作动筒Z、A平面与夹钳钳口交点OXY:作动筒X、Y平面与夹钳钳口交点PL1:左侧夹钳特征点1PL2:左侧夹钳特征点2PR1:右侧夹钳特征点1PR2:右侧夹钳特征点2勭:设备夹角∠OZAA1AOβ:设备夹角∠OZAA1Z1θ:设备夹角∠AOOZAA1

Figure BDA00003347509400051
:模具左侧特征点理论位置
Figure BDA00003347509400052
:模具右侧特征点理论位置TO:模具特征点连线中点
Figure BDA00003347509400053
:模具特征点连线中点理论位置O: Origin of the equipment coordinate system X: X-axis of the equipment coordinate system Y: Y-axis of the equipment coordinate system Z: Z-axis of the equipment coordinate system T L : Feature points on the left side of the mold (X negative side) T R : Feature points on the right side of the mold (One side in the positive X direction) h: Distance from the mold feature point to the bottom surface of the mold H: Pad height P L : Feature point of the left clamp (on the negative side of X direction) P R : Feature point of the right clamp (in the positive direction of X) One side) W: mold width D: distance between clamp and mold A 0 : A 0 joint point A : A joint point Y 0 : Y 0 joint point Y : Y joint point Z 0 : Z 0 joint point Z : Z joint point Z : Z joint point X 0 : X 0 joint point X : X joint point X : X joint point O ZA : Intersection point of actuator Z, A plane and clamp jaw O XY : Intersection point P of the actuator X, Y plane and the jaw of the clamp P L1 : Feature point 1P of the left clamp L2 : Feature point 2P of the left clamp R1 : Feature point 1P of the right clamp R2 : Right clamp Feature point 2: angle between equipment ∠O ZA A 1 A O β: angle between equipment ∠O ZA A 1 Z 1 θ: angle between equipment ∠A O O ZA A 1
Figure BDA00003347509400051
: The theoretical position of the feature point on the left side of the mold
Figure BDA00003347509400052
: The theoretical position of the feature point on the right side of the mold TO: The midpoint of the line connecting the feature points of the mold
Figure BDA00003347509400053
: The theoretical position of the midpoint of the mold feature point connection line

(五)具体实施方式(5) Specific implementation methods

如图1、图2、图3、图4、图5、图6、图7、图8、图9、图10所示,基于特征距离的模具定位方法,该方法的具体实施步骤如下:As shown in Figure 1, Figure 2, Figure 3, Figure 4, Figure 5, Figure 6, Figure 7, Figure 8, Figure 9, and Figure 10, the specific implementation steps of the mold positioning method based on the characteristic distance are as follows:

步骤一:模具初始摆放Step 1: Initial Mold Placement

蒙皮零件拉伸成形模具初始摆放示意如图2所示,摆放过程可按先后顺序分为放置垫块和放置模具。The initial placement of the stretch forming mold for skin parts is shown in Figure 2. The placement process can be divided into placing cushion blocks and placing molds in sequence.

1、放置垫块1. Place the block

垫块是工厂自制的标准件,按照高度与所能承受的重量划分,其高度和顶部平面满足工艺方案的精度要求。首先根据模具外形尺寸、质量和拉形轨迹确定垫块型号,选择垫块。放置垫块时,按照工艺规程将垫块放置在拉形设备的指定位置上,使垫块的对称平面与设备坐标的YZ平面平行。放置完成后,测量垫块顶部平面的水平度,确保垫块顶面水平。记录垫块的高度H。The spacer is a factory-made standard part, which is divided according to the height and the weight it can bear, and its height and top plane meet the accuracy requirements of the process plan. First, determine the model of the cushion block according to the overall size, quality and drawing track of the mold, and select the cushion block. When placing the block, place the block on the designated position of the pull-shaped equipment according to the process regulations, so that the symmetrical plane of the block is parallel to the YZ plane of the equipment coordinates. After placement, measure the levelness of the top plane of the chock to ensure that the top surface of the chock is level. Record the height H of the chock.

2、放置模具2. Place the mold

放置模具之前,首先测量模具特征点距模具底面的高度h,并检查特征点位置,与模具理论数模进行比较,确保实际模具与数模一致,防止模具因其它原因发生变化,如模具改型、模具刚度不够发生变化等。然后将模具放置在垫块上,尽量使模具的放置在拉形设备的坐标中心,且模具特征平面与设备的坐标平面尽量平行。摆放模具完成后,测量模具底面高度与模具底面水平度,保证模具高度和水平度符合要求。Before placing the mold, first measure the height h of the feature point of the mold from the bottom surface of the mold, check the position of the feature point, and compare it with the theoretical digital model of the mold to ensure that the actual mold is consistent with the digital model and prevent the mold from changing due to other reasons, such as mold modification , The rigidity of the mold is not enough to change, etc. Then place the mold on the block, try to make the mold placed in the coordinate center of the drawing equipment, and the mold feature plane and the coordinate plane of the equipment are as parallel as possible. After placing the mold, measure the height of the bottom surface of the mold and the levelness of the bottom surface of the mold to ensure that the height and levelness of the mold meet the requirements.

步骤二:运动设备Step Two: Sports Equipment

运动设备是将ACB FET系列横拉机的设备夹钳运动到指定位置,使夹钳特征点与模具特征点处于是同一水平面内,便于距离测量。首先确定拉形机夹钳位置坐标,然后根据夹钳位置反解出拉形机运动参数,再驱动拉形机运动将夹钳运动到指定位置。The moving equipment is to move the equipment clamp of ACB FET series horizontal drawing machine to the designated position, so that the clamp feature point and the mold feature point are in the same horizontal plane, which is convenient for distance measurement. First determine the position coordinates of the clamps of the stretching machine, and then decipher the movement parameters of the stretching machine according to the position of the clamps, and then drive the stretching machine to move the clamps to the specified position.

1、确定坐标1. Determine the coordinates

根据图3的示意,确定左右夹钳特征点所需要移动到的坐标位置。设左右夹钳的特征点分别为。由步骤一的测量记录,可知夹钳特征点的Z坐标为垫块高度与模具特征点距模具底面高度之和,即:According to the schematic diagram in FIG. 3 , determine the coordinate positions to which the feature points of the left and right clamps need to move. Let the feature points of the left and right clamps be . From the measurement records of step 1, it can be seen that the Z coordinate of the clamp feature point is the sum of the height of the spacer and the height of the mold feature point from the bottom surface of the mold, namely:

ZZ PP LL == ZZ PP LL == Hh ++ hh -- -- -- (( 11 ))

设模具宽度为W,假设模具是居中摆放,夹钳位置距模具两侧距离为D,即有:Let the mold width be W, assuming that the mold is placed in the center, and the distance between the clamp position and the two sides of the mold is D, that is:

xx PP LL == -- (( WW 22 ++ DD. )) ,, Xx PP RR == (( WW 22 ++ DD. )) -- -- -- (( 22 ))

由式(1)、(2)得到夹钳特征点的坐标。The coordinates of the clamp feature points are obtained from formulas (1) and (2).

2、设备反解2. Reverse solution of equipment

为了简化计算与测量,使距离测量时夹钳的姿态为与Y轴平行,如图5所示,即PL1、OZA、OXY、PL2的x和y坐标相同,作动筒Z和X伸长量相同,作动筒A和Y伸长量相同。In order to simplify the calculation and measurement, the posture of the clamp is parallel to the Y axis when measuring the distance, as shown in Figure 5, that is, the x and y coordinates of P L1 , O ZA , O XY , and P L2 are the same, and the actuator Z and The amount of elongation of X is the same, and the amount of elongation of cylinder A and Y is the same.

进行设备反解计算是根据已知的OZA点坐标,计算出设备作筒的伸长量,以设备左侧即X负方向一侧为例,如图6所示。分析机构简图,看出:The inverse calculation of the equipment is to calculate the elongation of the equipment barrel based on the known coordinates of the O ZA point. Take the left side of the equipment, that is, the side in the negative X direction, as an example, as shown in Figure 6. Analyzing the schematic diagram of the organization, it can be seen that:

(1)已知OZA、A0和Z0的坐标。(1) The coordinates of O ZA , A 0 and Z 0 are known.

(2)A与OZA的距离为一常数SA,A与Z的距离为一常数SZ(2) The distance between A I and O ZA is a constant S A , and the distance between A I and Z I is a constant S Z .

(3)A关节为同轴连接,即∠α与∠β固定不变。(3) A joint is coaxially connected, that is, ∠α and ∠β are fixed.

首先计算作筒A的伸长量,在△A0A1OZA中应用正弦定理,如下:First calculate the elongation of cylinder A, apply the sine law in △A 0 A 1 O ZA , as follows:

∠∠ Oo ZAZA AA 00 AA 11 == sinsin -- 11 (( || Oo ZAZA AA 11 || || AA 00 Oo ZAZA || sinsin αα )) -- -- -- (( 33 ))

∠∠ θθ == ππ ∠∠ αα -- ∠∠ Oo ZAZA AA 00 AA 11 -- -- -- (( 44 ))

由式(3)、(4)得到设备机构中∠θ的值。The value of ∠θ in the equipment mechanism can be obtained from formulas (3) and (4).

由向量

Figure BDA00003347509400063
顺时针旋转∠θ可得向量
Figure BDA00003347509400064
的方向,又SA为向量
Figure BDA00003347509400065
的长度,确定向量
Figure BDA00003347509400071
即可得到点A的坐标。具体计算如下:by vector
Figure BDA00003347509400063
Rotate ∠θ clockwise to get the vector
Figure BDA00003347509400064
direction, and S A is the vector
Figure BDA00003347509400065
length, determine the vector
Figure BDA00003347509400071
The coordinates of point A I can be obtained. The specific calculation is as follows:

Oo ZAZA AA 11 →&Right Arrow; == coscos θθ sinsin θθ -- sinsin θθ coscos θθ Oo ZAZA AA 00 →&Right Arrow; || Oo ZAZA AA 00 || SS AA -- -- -- (( 55 ))

AA 11 →&Right Arrow; == Oo ZAZA →&Right Arrow; ++ Oo ZAZA AA 11 →&Right Arrow; -- -- -- (( 66 ))

同理,计算出Z的坐标,如下:Similarly, the coordinates of Z are calculated as follows:

AA 11 ZZ 11 →&Right Arrow; == coscos ββ -- sinsin ββ sinsin ββ coscos ββ AA 11 Oo ZAZA →&Right Arrow; SS AA SS ZZ -- -- -- (( 77 ))

ZZ 11 →&Right Arrow; == AA 11 →&Right Arrow; ++ AA 11 ZZ 11 →&Right Arrow; -- -- -- (( 88 ))

由式(5)、(6)、(7)、(8)计算出设备机构关节点A和Z的坐标。The coordinates of joint points A and Z of the equipment mechanism are calculated from formulas (5), (6), (7) and (8).

由设备的对称性,同理求解出设备另一侧的关节点坐标。至此ACB FET设备所有关节点坐标已求解,完成机构反解。作筒伸长量可由关节点到作动筒铰支端的距离与作动筒零位时的长度之差计算得到。Based on the symmetry of the device, the coordinates of the joint points on the other side of the device are similarly calculated. So far, the coordinates of all relevant nodes of the ACB FET equipment have been solved, and the inverse solution of the mechanism has been completed. The elongation of the working cylinder can be calculated from the difference between the distance from the joint point to the hinge end of the working cylinder and the length of the working cylinder at zero position.

3、 驱动设备3. Drive equipment

将计算得到ACB FET系列横拉机各作动筒伸长量输入ACB FET拉形机控制面版,驱动设备运动,使夹钳运动到指定位置,并对夹钳位置进行检查,确定与理论设计位置吻合。Input the calculated elongation of each actuator of the ACB FET series horizontal stretching machine into the control panel of the ACB FET stretching machine, drive the equipment to move, move the clamp to the specified position, and check the position of the clamp to determine and theoretical design The location matches.

步骤三:测量计算Step 3: Measure and calculate

1、距离测量1. Distance measurement

检查夹钳与模具位置无误后,测量夹钳特征点与模具特征点的距离,如图7所示。根据X方向将模具与夹钳分为左侧即X负方向一侧和右侧即X正方向一侧。分别测量左侧夹钳两个特征点PL1、PL2到模具左侧一端的特征点TL的距离与右侧夹钳两个特征点PR1、PR2到模具右侧一端的特征点TR的距离,并将记录测量距离。After checking that the positions of the clamp and the mold are correct, measure the distance between the feature points of the clamp and the feature points of the mold, as shown in Figure 7. According to the X direction, the mold and clamp are divided into the left side, which is the negative X direction side, and the right side, which is the positive X direction side. Measure the distance from the two feature points P L1 and P L2 of the left clamp to the feature point T L on the left end of the mold and the distance from the two feature points P R1 and P R2 of the right clamp to the feature point T on the right end of the mold R and will record the measured distance.

2、几何计算2. Geometric calculation

如图8所示,根据已知的夹钳特征点的坐标和测量得到的距离,计算模具特征点的坐标,计算方法如下:As shown in Figure 8, the coordinates of the mold feature points are calculated according to the known coordinates of the clamp feature points and the measured distance, and the calculation method is as follows:

模具左侧特征点 T L ( x T L , y T L , Z T L ) T : Feature points on the left side of the mold T L ( x T L , the y T L , Z T L ) T :

P L 1 ( x P L 1 , y P L 1 , Z P L 1 ) T 为圆心,LL1为半径的圆的方程为by P L 1 ( x P L 1 , the y P L 1 , Z P L 1 ) T The equation of a circle whose center is L and L1 is radius is

(( TT LL -- PP LL 11 )) TT (( TT LL -- PP LL 11 )) == LL LL 11 22 -- -- -- (( 99 ))

P L 2 ( X P L 2 , y P L 2 , Z P L 2 ) T 为圆心,LL1为半径的圆的方程为by P L 2 ( x P L 2 , the y P L 2 , Z P L 2 ) T The equation of a circle whose center is L and L1 is radius is

Figure BDA00003347509400081
Figure BDA00003347509400081

由于点PL1、PL2、TL处于同一高度平面内,即:Since the points P L1 , P L2 , and T L are in the same height plane, that is:

ZZ TT LL == ZZ PP LL 11 == ZZ PP LL 22 -- -- -- (( 1111 ))

联立方程,得到关于点

Figure BDA00003347509400083
的两个解,取
Figure BDA00003347509400084
较大的解为真解,即模具左侧特征点的解。Simultaneous equations, get about the point
Figure BDA00003347509400083
The two solutions of , take
Figure BDA00003347509400084
The larger solution is the true solution, that is, the solution of the feature point on the left side of the mold.

同理解得模具右侧特征点的解 T R ( x T R , y T R , Z T R ) T . The solution to the feature points on the right side of the mold is understood in the same way T R ( x T R , the y T R , Z T R ) T .

步骤四:模具定位计算Step 4: Die positioning calculation

由上一步骤得到模具特征点坐标 T L ( X T L , y T L , Z T L ) T T R ( x T R , y T R , Z T R ) T , 通过与模具特征点的理论值进行比较,计算出理论模具位置到实际模具位置之间的变换关系,如图9所示。在平面内的模具位置变换通过一次平移和一次旋转变换实现,变换参数计算如下:Obtain the mold feature point coordinates from the previous step T L ( x T L , the y T L , Z T L ) T and T R ( x T R , the y T R , Z T R ) T , By comparing with the theoretical value of the mold feature points, the transformation relationship between the theoretical mold position and the actual mold position is calculated, as shown in Figure 9. The mold position transformation in the plane is realized by a translation and a rotation transformation, and the transformation parameters are calculated as follows:

TL与TR连线中点TO的坐标:The coordinates of the midpoint T O of the line connecting T L and T R :

(( xx TT Oo ,, ythe y TT Oo ,, ZZ TT Oo )) TT == [[ (( xx TT LL ,, ythe y TT LL ,, ZZ TT LL )) TT ++ (( xx TT RR ,, ythe y TT RR ,, ZZ TT RR )) TT ]] // 22

Figure BDA00003347509400089
Figure BDA000033475094000810
连线中点
Figure BDA000033475094000811
的坐标:
Figure BDA00003347509400089
and
Figure BDA000033475094000810
midpoint
Figure BDA000033475094000811
coordinate of:

(( xx TT 00 Oo ,, ythe y TT 00 Oo ,, ZZ TT 00 Oo )) TT == [[ (( xx TT 00 LL ,, ythe y TT 00 LL ,, ZZ TT 00 LL )) TT ++ (( xx TT 00 RR ,, ythe y TT 00 RR ,, ZZ TT 00 RR )) TT ]] // 22

平移向量

Figure BDA000033475094000813
translation vector
Figure BDA000033475094000813

TT →&Right Arrow; == TT Oo TT Oo 00 →&Right Arrow; -- -- -- (( 1414 ))

旋转角度θ:Rotation angle θ:

θθ == coscos -- 11 (( TT LL TT RR .. →&Right Arrow; TT LL Oo TT RR Oo →&Right Arrow; || TT LL TT RR || →&Right Arrow; ** || TT LL Oo TT RR Oo →&Right Arrow; || )) -- -- -- (( 1515 ))

旋转轴向量

Figure BDA000033475094000816
axis of rotation vector
Figure BDA000033475094000816

RR →&Right Arrow; == TT LL Oo TT RR Oo →&Right Arrow; ×× TT LL TT RR →&Right Arrow; -- -- -- (( 1616 ))

步骤五:修正数控代码进行拉形Step 5: Correct the NC code for drawing

由上一步骤计算得到的变换参数,将理论模具变换到实际模具摆放位置,以新的模具位置为基准,应用工艺参数生成与实际模具位置相符的设备数控代码。将拉形设备数控代码输入ACB FET横向拉形机,对拉形机进行空载运行,检查设备运动是否与所设计的工艺参数相符。检查无误后,进行蒙皮拉形。From the transformation parameters calculated in the previous step, the theoretical mold is transformed to the actual mold placement position, and the new mold position is used as a benchmark, and the process parameters are applied to generate the equipment CNC code that matches the actual mold position. Input the CNC code of the drawing equipment into the ACB FET horizontal drawing machine, run the drawing machine with no load, and check whether the movement of the equipment is consistent with the designed process parameters. After the check is correct, carry out skin pulling.

Claims (3)

1. mould localization method based on characteristic distance, its step is as follows:
Step 1: mould is initially put
Initially putting of skin part stretch forming mold is that actual mould is placed in the coordinate system of pull-shaped equipment, is the preparation of carrying out mould location survey and Stretch Forming Process;
Die layout together is placed in the coordinate system of pull-shaped equipment with cushion block on the standard cushion block, and the standard cushion block is the homemade standard component of factory, distinguishes by the mold weight that height and cushion block can hold; Mould is initially put at first according to the pull-shaped die boundary dimensions of covering and quality, choice criteria cushion block; Then put cushion block and mould according to the factory technics rules, measure cushion block end face levelness, guarantee cushion block placement level, record cushion block height H and mold feature point are apart from mould bottom surface height h;
Step 2: sports equipment
Sports equipment is that the equipment clamp with ACB FET series transverse stretching machine moves to assigned address, and it is in the same level that clamp characteristic point and mold feature point is in, and is convenient to range measurement;
(1) determines coordinate
Determine the coordinate position at clamp characteristic point place when measuring, by the height of cushion block and the mold feature point distance apart from the mould bottom surface, the height of determining mold feature point place horizontal plane is the Z coordinate; By appearance and size and the theoretical locus of putting of mould, determine that the position of clamp characteristic point on X-axis is the X coordinate; According to the position of clamp characteristic point on clamp, can obtain the Y coordinate of clamp characteristic point;
(2) equipment is counter separates
The anti-solution of motion of ACB FET series transverse stretching machine is the coordinate position by the clamp characteristic point, solves the length of each pressurized strut on the parallel institution according to the mechanical feature of pull-shaped equipment, i.e. the kinematic parameter of equipment; The machine drawing of ACBFET series digital control horizontal is used for that the aircraft skin part is horizontal to pull into shape; This equipment is the left-right symmetry structure, a friction clamp mouth of every side clamp, and two horizontal pressurized struts, two vertical pressurized struts form two pairs of four bar parallel institutions; The locus of clamp and attitude are determined jointly by the elongation of four pressurized struts; Position when measuring, in order to simplify the anti-computational process of separating of motion, set the clamp axis parallel with Y-axis, therefore only need to calculate the position of clamp in the ZX plane, namely only need to calculate the elongation of Z pressurized strut and A pressurized strut;
(3) driving arrangement
The elongation of each pressurized strut of stretching machine, stretching former that the anti-solution of ACB FET series transverse stretching machine is obtained, the interface driving arrangement motion of input digital control horizontal machine drawing control system makes clamp move to assigned address, is used for carrying out range measurement;
Step 3: measure and calculate
Measuring process is to measure each characteristic point of clamp to the distance of each characteristic point of mould, then calculates through how much, obtains the coordinate of characteristic point;
(1) range measurement
In the left side, two clamps in right side, two characteristic points of mark respectively, be designated as P L1, P L2And P R1, P R2; Two characteristic points of mark are designated as T on mould LAnd T R; Measure respectively P L1, P L2To T LDistance and P R1, P R2; To T RDistance;
(2) calculate for how much
After the motion of step 2 driving arrangement, characteristic point and mold feature point is in the horizontal plane of sustained height on the clamp, so the mould location Calculation can be utilized the method for solving of plane geometry, the coordinate of calculating mold feature point;
Take in the left side as example, mold feature point T LConcrete coordinate can be by with P L1Be the center of circle, L L1For the circle of radius and with P L2Be the center of circle, L L2Determine for the intersection point of the circle of radius, in like manner can determine right side mold feature point T RConcrete coordinate;
Step 4: mould location Calculation
The concrete coordinate of the mold feature point that calculates by measurement compares calculating with mold feature point theoretical coordinate, draws translation vector and rotational angle in the die top cushion block holding plane;
Step 5: revise numerical control code and carry out pull-shaped
The transformation parameter that is calculated by step 4, theoretical mould is transformed to the actual mould putting position, take new die location as benchmark, the technique for applying parameter generates the equipment numerical control code that conforms to the actual mould position, with the horizontal stretching machine, stretching former of pull-shaped equipment numerical control code input ACB FET, stretching machine, stretching former is carried out no-load running, whether the checkout facility motion conforms to designed technological parameter, check errorless after, carry out covering pull-shaped;
By above-mentioned five steps, realize the quick location of pull-shaped die space position, revise the method for pull-shaped track by the mould physical location, allow the stretch forming process of skin part tally with the actual situation, make and be able to little on the impact of part forming precision because of the die layout position deviation, reduce the use of positioning tool, guaranteed the precision that the aircraft skin part is produced.
2. a kind of mould localization method based on characteristic distance according to claim 1, it is characterized in that: the method for finding the solution the equipment moving parameter at the coordinate that passes through the clamp characteristic point described in the step 2, utilize the accurate control ability of equipment mechanism characteristics and numerical controlled stretch forming equipment, realized by clamp trace generator numerical control code Stretch Forming Process accurately being controlled.
3. a kind of mould localization method based on characteristic distance according to claim 1, it is characterized in that: distance is determined the method for mold feature point position between the measurement characteristic point described in the step 3, by simple measurement and how much calculating, realize the die space location positioning, the method is simple and practical, is convenient to implement.
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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6532786B1 (en) * 2000-04-19 2003-03-18 D-J Engineering, Inc. Numerically controlled forming method
CN101510083A (en) * 2009-04-01 2009-08-19 北京航空航天大学 Airplane covering transversal stretch forming loading track designing and numerical control code generating method
CN101515181A (en) * 2009-04-07 2009-08-26 北京航空航天大学 Method for designing loading trajectory of airplane skin lengthwise stretch forming and generating numerical control codes
CN101894181A (en) * 2010-06-30 2010-11-24 上海飞机制造有限公司 A Design Method of Loading Trajectory of VTL NC Skin Stretching Machine
CN102445921A (en) * 2010-09-30 2012-05-09 成都飞机工业(集团)有限责任公司 Method for designing loading track for multi-pass roll bending of wall plate and generating numerical control code

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6532786B1 (en) * 2000-04-19 2003-03-18 D-J Engineering, Inc. Numerically controlled forming method
CN101510083A (en) * 2009-04-01 2009-08-19 北京航空航天大学 Airplane covering transversal stretch forming loading track designing and numerical control code generating method
CN101515181A (en) * 2009-04-07 2009-08-26 北京航空航天大学 Method for designing loading trajectory of airplane skin lengthwise stretch forming and generating numerical control codes
CN101894181A (en) * 2010-06-30 2010-11-24 上海飞机制造有限公司 A Design Method of Loading Trajectory of VTL NC Skin Stretching Machine
CN102445921A (en) * 2010-09-30 2012-05-09 成都飞机工业(集团)有限责任公司 Method for designing loading track for multi-pass roll bending of wall plate and generating numerical control code

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
韩金全等: "飞机复杂蒙皮拉形模具型面设计方法", 《北京航空航天大学学报》 *

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105711107A (en) * 2016-03-25 2016-06-29 哈尔滨飞机工业集团有限责任公司 Method for reversely seeking locating basis of automatic belt laying machine
US10475205B2 (en) 2017-09-13 2019-11-12 National Tsing Hua University Positioning and measuring system based on flexible feature image scale
CN110084779A (en) * 2019-03-04 2019-08-02 南京航空航天大学 A kind of extraction of aircraft thickness covering end surface features point and denoising method based on laser scanning
CN113020388A (en) * 2021-02-08 2021-06-25 中国重型机械研究院股份公司 Four-degree-of-freedom transverse skin stretcher
CN113020389A (en) * 2021-02-08 2021-06-25 中国重型机械研究院股份公司 Skin stretcher
CN113020387A (en) * 2021-02-08 2021-06-25 中国重型机械研究院股份公司 Skin stretcher with three-rotation one-movement characteristic
CN113020389B (en) * 2021-02-08 2022-10-18 中国重型机械研究院股份公司 Skin stretcher
CN113020387B (en) * 2021-02-08 2023-03-10 中国重型机械研究院股份公司 Skin stretcher with three transfer and one transfer characteristics
CN113020388B (en) * 2021-02-08 2023-03-10 中国重型机械研究院股份公司 Four-degree-of-freedom transverse skin stretcher
CN115870394A (en) * 2022-12-29 2023-03-31 吉林大学 Joint-like freedom degree controllable push-pull mechanism for flexible stretch forming machine
CN115870394B (en) * 2022-12-29 2023-10-24 吉林大学 Controlled push-pull mechanism with simulated joint degree of freedom for flexible stretch forming machines

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