• <tr id="yyy80"></tr>
  • <sup id="yyy80"></sup>
  • <tfoot id="yyy80"><noscript id="yyy80"></noscript></tfoot>
  • 99热精品在线国产_美女午夜性视频免费_国产精品国产高清国产av_av欧美777_自拍偷自拍亚洲精品老妇_亚洲熟女精品中文字幕_www日本黄色视频网_国产精品野战在线观看 ?

    Method for Measuring Residual Stresses Induced by Boring in Internal Surface of Tube and Its Validation with XRD Method*

    2014-04-24 10:54:08MengLonghui孟龍暉HeNing何寧YangYinfei楊吟飛ZhaoWei趙威RongBin戎斌

    Meng Longhui(孟龍暉),He Ning(何寧)***,Yang Yinfei(楊吟飛),Zhao Wei(趙威),Rong Bin(戎斌)

    1.College of Mechanical and Electrical Engineering,Nanjing University of Aeronautics of Astronautics,Nanjing,210016,P.R.China;2.Shanghai Aircraft Manufacturing Co.,Ltd.,Shanghai,200436,P.R.China

    1 Introduction

    Residual stresses exist in most parts after machining,whose values are hard to accurately measure in most cases.Metal cutting is a process with high temperature,high strain,high strain rate,and large elastic-plastic deformations[1-2],and residual stresses exist in the superficial layer,whose depth is commonly no more than 0.2mm.However,the gradient in the thin layer is very high along the depth direction.The residual stresses can be attributed to several factors such as mechanical stresses,thermal stresses and phase transformations[3-4].The residual stresses induced by machining in the surface layer are an important factor that affects the workpieces stat-ics strength,fatigue strength,corrosion resistance,service life,geometric and dimension stability[5-7].Wang,et al.[8]studied the deformations caused by residual stresses generated by milling in aluminum alloy,and Miao,et al.[9]improved the surface property by shot peening.Generally speaking,the residual stresses play an important role in in-service performance of machined parts.Therefore,it is significant to measure the residual stresses induced by machining and reduce their harmful effects.

    During the past years,different methods for measuring residual stresses have been developed.They can mainly be classified as destructive,semi-destructive and non-destructive techniques[10].The destructive and semi-destructive techniques,called mechanical methods,are dependent on inferring the residual stresses from the displacement measured after completely or partially relieving the stresses by removing material[11].Sectioning,contour,hole-drilling,deephole and ring-core are the principal destructive and semi-destructive techniques used to measure the residual stresses in structural members[10-11].Non-destructive techniques include neutron or X-ray diffraction,magnetic methods and ultrasonic methods.These techniques usually measure some parameters related to the stresses[12-15].X-ray diffraction(XRD)method is commonly used to measure the surface residual stresses,as the penetration depth of X-rays in common metals is very shallow(just few microns).A layer removal technique must thus be used in association with XRD method to measure in-depth stresses.It is recognized that the XRD equipment is very expensive,and the XRD method is just applicable to materials that are crystalline and relatively fine grained[16],which are serious drawbacks.Therefore,this paper presents a strain-based method using much cheaper equipment to measure the residual stresses induced by boring in internal surface of the tube.The correctness of the strainbased method will be validated by the results obtained from the XRD method later in this paper.

    2 Calculation Principle

    The theory of calculating residual stresses in the internal surface of tube is based on the variations of the axial length and the external diameter when removing the internal stress layers,which was first presented by Mesnager in 1919[15].Authors improve the calculating method and put it into practice here.

    Assuming that the tube is so long that it can be disposed as a problem in a plane(an appropriate length of the tube will be determined by finite element method(FEM)in what follows).The internal radius of the tube is RIN,and the external radius ROUT.σZ,σT,σRare the stresses along the axial,tangential and radial directions in the tube,respectively.A schematic representation of the residual stresses in the tube is shown in Fig.1.

    Fig.1 Schematic representation of the residual stress in tube

    The average value of the residual stress in the layer from radius RINto radius rMisσ(rM).When removing this layer,it equals to applying the force of the same magnitude in the reverse direction on the newly exposed surface of the rest part after the layer removal.HereσZO,σTOandσROare the stresses along the axial,tangential and radial directions on the outside surface induced by the internal layer removal.There is no force on the internal surface in the radial direction before layer removal,and thusσROis 0.According to the Lame cylinder theory,it can be concluded that

    LetεZO,εTO,εROrepresent the strains along the axial,tangential and radial directions on the outside surface.The relationship between the stresses and the strains on the external surface is as follows

    where E andμare the elasticity modulus and poisson ratio of the material,respectively.AsσROis 0,it can be obtained by

    From Eqs.(1,3,5),another equation can be written as

    Moreover,the axisymmetric plane equilibrium should be satisfied,i.e.

    If there is no external force applied to the part,the equilibrium equations along the axial and tangential directions should be satisfied as follows

    The residual stress along the tangential direction can be obtained from Eqs.(6,7)

    In Eq.(10),SROUT=πR2OUT,S=πR2M.When the internal layer from radius RINto radius rMhas been removed,the residual stresses in the rest part can be assumed to be redistributed uniformly.Based on this assumption and Eq.(8),another equilibrium equation can be obtained

    Taking a derivative with respect to rMof Eq.(11),we have

    The residual stress along the axial direction can be derived from Eqs.(2,5,12)

    In conclusion,the residual stresses in three directions induced by boring in the internal surface of the tube can be obtained from Eqs.(6,10,13).

    3 FEM Validation of Tube Length

    The aforementioned equations are deduced on the very long tube assumption,but in practice it is not the case.For the convenience and accuracy of the measurements,F(xiàn)EM is used to find an appropriate length of the tube in this paper.

    The tube model,created by Abaqus 6.10 software,has a 45mm external diameter and a 41mm internal diameter.As presented in Ref.[2],when the length of the tube is over 6times of the external diameter,the measurement accuracy will be high enough.Here the length of the tube is first set as 450mm to ensure a very high accuracy.Since the residual stresses along the radial direction are so small in a real part that they can be ignored in the model,the model is just loaded with the residual stresses along the axial and tangential directions.Here an input file calculated by MATLAB is used to load the residual stresses,and the stress values in the cylindrical coordinate should be transmitted to the rectangular coordinate with the following equation

    With the command″initial conditions,type=stress,input=S.dat″,the stress file is imported.Here the residual stresses applied to the model can be seen as a typical case of residual stresses induced by boring.

    After loading the residual stresses(Fig.2),the gradient of the stresses along the depth direction is extremely high,which is the main characteristic of the residual stresses induced by machining.To simulate the experimental process of removing material layers by corrosion,the technology of″element birth and death″is used to″kill″the elements in the internal surface of the model layer by layer.The strains on the outside surface along the axial and tangential directions are recorded after″killing″each layer.Here the recorded strains are in the mid-h(huán)eight of the model.In the experiments,the strain gauge should also be installed in the mid-h(huán)eight of the tube.

    Fig.2 Results of the model after imposing residual stress

    The accuracy of the results obtained from the above model is high.But the tube is too long,thus causing lots of inconvenience and material wastage.A new model with the same internal and external radii is created to have a different length along the axial direction.The strains obtained from the long model mentioned above is set as references to see how long the new model should be in order to gain accurate results.

    Here,Python language is used to create the model and make the second development to Abaqus.The tube length is first set as 20mm.The tube length is increased by an increment of 5mm each time.The calculated strains and the references are compared to find out whether the accuracy is high enough.Fig.3gives a schematic representation of the second development,where the high accuracy is defined as that the maximum error is no more than 0.1×10-6.

    The analytical result indicates that when the tube length reaches 50mm,the accuracy can meet the requirement.Therefore,it can be concluded that the 50mm tube length is long enough to obtain an accurate result.The result can give some guidance to the related projects in practice,that is,as the tube diameter changes,if the ratio of tube length to external diameter is no less thanλ=50/45=1.11,the accuracy will be high enough.

    Fig.3 Schematic of the second development

    4 Validation of Strain-Based Method with XRD Method

    To validate the correctness of the strainedbased method,a comparison should be made between the results obtained from the strain-based method and those from XRD method.

    The tube used in experiments(Fig.4(a))is made of Ti6Al4V.First,annealing treatment is performed on the tube to remove the initial residual stresses.The external and internal diameters are 50mm and 41mm,respectively.The internal material layers are removed by chemical corrosion which will not introduce any new residual stress to the rest part.According to the relationship between the depth of the removed layer and corrosion time,the time should be precisely controlled to make sure that for each time the depth of the removed layer is 10μm.After finished corrosion,the chemical reagent is washed away immediately.When the tube reached the room temperature,the strains in the tangential and axial directions are recorded.Since temperature has a significant effect on the measuring results,and the room temperature cannot always stay the same,temperature compensation must be accomplished here.After each layer removal and the corresponding strains recording,the residual stresses on the internal surface of the tube are also measured by the XRD method,using aportable Proto-LXRD machine and employing the following parameters:tube voltage of 30kV,tube current of 25mA,irradiated area of 1mm×3mm and the sin2φmethod.

    Fig.4 Tube to be measured and the strain meter equipment

    Removing the stress layers surely causes some relaxation and redistribution of the residual stresses,and thus the results from the XRD method should be compensated in order to obtain correct stress values.

    After Moore and Evans published their paper in 1958,few literatures can be found on the development of correction method for layer removal[17-18].The correction method proposed by Moore and Evans for plates and cylinders is still the most commonly used one,that is

    whereσT,σR,σZare the corrected circumferential,radial,axial stresses,respectively.σZMand σTMare the measured residual stresses in the axial and tangential directions,while ROUT,RINand r are the external,internal and actual measurement radii,respectively.

    Eqs.(15-17)are based on several assumptions:(1)Circumferential layer removal should not introduce any new residual stress to the rest of the part.It is well-known that corrosion will not cause any new residual stress,and the material layers are thus removed by chemical corrosion here.(2)The tubes to be measured must be long enough and the measurement location should be far away from the edges.In this paper,the tube used in the experiments is not very long,just 50 mm.According to the finite element analysis,the accuracy is acceptable when the measurement is performed in the middle height of the tube.(3)The residual stresses to be measured are either plane symmetric or rotationally symmetric[18].Here in this paper,the residual stresses induced by boring is highly rotationally symmetric.(4)During the relaxation and redistribution caused by layer removal,the stresses must always remain elastic.In our experiments,the residual stresses induced by boring are certainly far from elastic limit of the material.Hence,it will not cause any plasticity during relaxation and redistribution.

    In general,these assumptions are all satisfied here.Therefore,the measured residual stress can be corrected by Eqs.(15-17).

    5 Results and Discussion

    The residual stress profiles obtained from two methods are shown in Fig.5.The residual stresses in the axial and tangential directions induced by boring are all compressive in the outmost layers.The magnitude of the stress along the tangential direction is greater than the one along the axial direction.Besides,the depth of the layer with compressive residual stress is about 60μm in both directions.

    Fig.5 Residual stress measured by two methods

    The stress profiles along both the axial and the tangential directions obtained from the two methods agree well with each other.The maximum error between the two results is less than 10 MPa,which can be ascribed to the limit of the measuring equipment.The margin of error from this method is no more than±10MPa,which can be accepted in most cases.By analyzing the obtained results,it can be concluded that the accuracy of the strain-based method proposed in this paper is high enough and it can be used to measure the residual stresses in the internal surface of the tube in practice.

    6 Conclusions

    A strain-based method is proposed to measure the residual stresses induced by boring in internal surface of the tube,and it is based on the strains on external surface of the tube.The results of the finite element analysis show that if the ratio of tube length to external diameter reaches no less thanλ=50/45=1.11,the accuracy will be high enough for both strain-based measuring method and the correction method proposed by Ref.[18].The measurements obtained from strain-based method are compared with those obtained from XRD method.Both the stress profiles correspond to each other very well and the validity of the strain-based method has thus been confirmed.Therefore,the proposed method can provide stress profiles with high accuracy and can take the place of XRD method in practice in some cases with much cheaper equipments.

    [1] Withers P J,Turski M,Edwards L,et al.Recent advances in residual stress measurement[J].International Journal of Pressure Vessels and Piping,2008,85:118-127.

    [2] Ge W H.The analysis of the residual stress in Spinning tube parts[J].Metal Forming Machinery,1985(3):2-12.(in Chinese)

    [3] Yu X X,Lau W S,Lee T C.A finite element analysis of residual stress in stretch turning[J].Int J Mach Tools Manufact,1997,37(10):1525-1537.

    [4] Liu C,Zhang J X,Wu B,et al.Numerical investigation on the variation of welding stresses after material removal from a thick titanium alloy plate joined by electron beam welding[J].Materials and Design,2012,34:609-617.

    [5] Wang Q C.Evaluation and relief of residual stress in aluminum alloys for aircraft structures[D].Hangzhou:College of Mechanical and Energy Engineering,Zhejiang University,2003:4-7.(in Chinese)

    [6] Larsson C,Holden T M,Bourke M A M,et al.Measurement and modeling of residual stress in a welded Haynes 25cylinder[J].Materials Science and Engineering,2005,A(399):49-57.

    [7] Grzesik W,Zak K.Surface integrity generated by oblique machining of steel and iron parts[J].Journal of Materials Processing Technology,2012,212:2586-2596.

    [8] Wang H F,Zuo D W,Dai S,et al.Milling Deformations of Jointed 7022Aluminum Alloy by FSJ[J].Journal of Nanjing University of Aeronautics &Astronautics,2013,45(2):245-249.(in Chinese)

    [9] Miao H,Zuo D W,Wang H J,et al.Surface Characteristic of 10Ni3MnCuAl Steel by Shot Peening[J].Transactions of Nanjing University of Aeronautics and Astronautics,2009,26(3):178-183.

    [10]Mirzaee-Sisan A,F(xiàn)ookes A J,Truman C E,et al.Truman residual stress measurement in a repair welded header in the as-welded condition and after advanced post weld treatment[J].International Journal of Pressure Vessels and Piping,2007,84:265-273.

    [11]Yan D J,Liu X S,Li J,et al.Effect of strain hardening and strain softening on welding distortion and residual stress of A7N01-T4aluminum alloy by simulation analysis[J].Journal of Central South University of Technology,2010,17:666-673.

    [12]Navas V G,Gonzalo O,Bengoetxea I.Effect of cutting parameters in the surface residual stress generated by turning in AISI 4340steel[J].International Journal of Machine Tools &Manufacture,2012,61:48-57.

    [13]Pratihar S,Stelmukh V,Hutchings M T,et al.Measurement of the residual stress field in MIG-welded Al-2024and Al-7150aluminium alloy compact tension specimens[J].Materials Science and Engineering,2006,A(437):46-53.

    [14]Sebastiani M,Eberl C,Bemporad E,et al.Depth-resolved residual stress analysis of thin coatings by a new FIB-DIC method[J].Materials Science and Engineering,2011,A(528):7901-7908.

    [15]Carrera E,Rodríguez A,Talamantes J,et al.Measurement of residual stress in cast aluminium engine blocks[J].Journal of Materials Processing Technology,2007,189:206-210.

    [16]Rossini N S,Dassisti M,Benyounis K Y,et al.Methods of measuring residual stress in components[J].Materials and Design,2012,35:572-588.

    [17]George D,Smith D J.Through thickness measurement of residual stress in a stainless steel cylinder containing shallow and deep weld repairs[J].International Journal of Pressure Vessels and Piping,2005,82:279-287.

    [18]Rossini N S,Dassisti M,Benyounis K Y,et al.Methods of measuring residual stress in components[J].Materials and Design,2012(35):572-588.

    [19]Azanza Ricardo C L,D′Incau M,Scardi P.Revision and extension of the standard laboratory technique for X-ray diffraction measurement of residual stress gradients[J].Appl Crystallogr,2007,40:675-83.

    [20]Moore M G,Evans W P.Mathematical correction for stress in removed layers in X-ray diffraction residual stress analysis[J].SAE Trans 1958,66:340-345.

    香蕉国产在线看| 99国产精品一区二区三区| 悠悠久久av| 日韩 欧美 亚洲 中文字幕| 亚洲精品美女久久av网站| a级毛片在线看网站| 性少妇av在线| 香蕉久久夜色| 久久久久久人人人人人| 精品一品国产午夜福利视频| 国产视频一区二区在线看| 免费观看人在逋| 国产精品av久久久久免费| 19禁男女啪啪无遮挡网站| 午夜福利免费观看在线| 黄色片一级片一级黄色片| 亚洲在线自拍视频| 不卡一级毛片| 黄色视频不卡| 无人区码免费观看不卡| 91在线观看av| 好男人电影高清在线观看| 一二三四社区在线视频社区8| 丝袜人妻中文字幕| 法律面前人人平等表现在哪些方面| 国产成+人综合+亚洲专区| 日韩欧美国产一区二区入口| 国内毛片毛片毛片毛片毛片| 中文字幕色久视频| 99国产精品一区二区三区| 亚洲成人免费av在线播放| 一个人免费在线观看的高清视频| 精品一区二区三区四区五区乱码| 成人永久免费在线观看视频| 国产一区在线观看成人免费| 1024视频免费在线观看| 国产精品一区二区免费欧美| 女人被躁到高潮嗷嗷叫费观| 美女高潮到喷水免费观看| 一级作爱视频免费观看| 精品卡一卡二卡四卡免费| 日韩免费av在线播放| 捣出白浆h1v1| 黄色片一级片一级黄色片| 一级毛片精品| 久久人人97超碰香蕉20202| 成年人免费黄色播放视频| 久久午夜亚洲精品久久| 在线观看免费高清a一片| 欧美日韩亚洲高清精品| 国产一区二区三区在线臀色熟女 | 亚洲av日韩在线播放| 亚洲精品乱久久久久久| 成人永久免费在线观看视频| 国产xxxxx性猛交| 亚洲av第一区精品v没综合| 成人国语在线视频| 岛国在线观看网站| 精品人妻在线不人妻| 亚洲七黄色美女视频| 久久久久视频综合| 成年人午夜在线观看视频| 天天影视国产精品| 日韩欧美免费精品| 成人18禁在线播放| 亚洲欧美激情在线| 啦啦啦 在线观看视频| 制服诱惑二区| 男男h啪啪无遮挡| 亚洲成人免费电影在线观看| 欧美av亚洲av综合av国产av| 夜夜爽天天搞| 色婷婷av一区二区三区视频| 午夜日韩欧美国产| 久久久久久久久久久久大奶| 精品久久久久久久久久免费视频 | 国产日韩欧美亚洲二区| 啪啪无遮挡十八禁网站| 淫妇啪啪啪对白视频| 婷婷成人精品国产| 亚洲性夜色夜夜综合| 两人在一起打扑克的视频| 午夜91福利影院| 亚洲美女黄片视频| 在线看a的网站| 午夜久久久在线观看| 亚洲精品成人av观看孕妇| a级片在线免费高清观看视频| 在线观看免费日韩欧美大片| 99久久99久久久精品蜜桃| 精品人妻1区二区| 香蕉丝袜av| 777米奇影视久久| 手机成人av网站| 日韩欧美一区二区三区在线观看 | 欧美激情久久久久久爽电影 | 国产一区在线观看成人免费| 91国产中文字幕| 国产日韩一区二区三区精品不卡| 成人av一区二区三区在线看| 欧美日韩乱码在线| av天堂久久9| 亚洲精品在线美女| 亚洲九九香蕉| 欧美一级毛片孕妇| 亚洲成人免费电影在线观看| 黑丝袜美女国产一区| 久久久久久亚洲精品国产蜜桃av| 一本大道久久a久久精品| 国产淫语在线视频| 欧美人与性动交α欧美精品济南到| 日日爽夜夜爽网站| 国产又爽黄色视频| 母亲3免费完整高清在线观看| 正在播放国产对白刺激| 91字幕亚洲| 国产精品av久久久久免费| 99久久综合精品五月天人人| 亚洲精品一卡2卡三卡4卡5卡| 国产精品免费一区二区三区在线 | aaaaa片日本免费| 国产精品秋霞免费鲁丝片| 精品久久久久久久久久免费视频 | 黄色怎么调成土黄色| 亚洲精品成人av观看孕妇| 精品一品国产午夜福利视频| 免费观看人在逋| 成人国语在线视频| 热re99久久国产66热| 每晚都被弄得嗷嗷叫到高潮| 一a级毛片在线观看| 亚洲,欧美精品.| 久久中文字幕人妻熟女| 午夜精品久久久久久毛片777| 伦理电影免费视频| 成人精品一区二区免费| 久久精品亚洲精品国产色婷小说| 亚洲va日本ⅴa欧美va伊人久久| 亚洲精品在线美女| 午夜影院日韩av| 国产精品免费一区二区三区在线 | 男人操女人黄网站| 夫妻午夜视频| 欧美性长视频在线观看| 精品亚洲成a人片在线观看| 大香蕉久久网| 午夜免费成人在线视频| 久热爱精品视频在线9| 丝袜在线中文字幕| 久热这里只有精品99| 90打野战视频偷拍视频| 日韩有码中文字幕| 久久久久久久久免费视频了| 亚洲欧美日韩另类电影网站| 日韩成人在线观看一区二区三区| 天堂动漫精品| 一区二区三区精品91| 正在播放国产对白刺激| 在线观看66精品国产| 久久精品熟女亚洲av麻豆精品| 一个人免费在线观看的高清视频| 久久天躁狠狠躁夜夜2o2o| 国产成人免费观看mmmm| 久久人人爽av亚洲精品天堂| 欧美日韩av久久| 美女午夜性视频免费| 国产男女超爽视频在线观看| 欧美日韩成人在线一区二区| 午夜老司机福利片| 无人区码免费观看不卡| 久久久久国产一级毛片高清牌| 欧美大码av| 看免费av毛片| 老司机在亚洲福利影院| 97人妻天天添夜夜摸| 亚洲欧美日韩另类电影网站| 久久精品熟女亚洲av麻豆精品| 黄色视频,在线免费观看| 国产熟女午夜一区二区三区| 国产精品永久免费网站| 两性午夜刺激爽爽歪歪视频在线观看 | 自线自在国产av| 午夜福利一区二区在线看| 天天躁狠狠躁夜夜躁狠狠躁| www.999成人在线观看| 亚洲av第一区精品v没综合| 久久香蕉激情| av一本久久久久| 欧美日韩精品网址| 国产在线一区二区三区精| 美女高潮喷水抽搐中文字幕| 久久久久久久久久久久大奶| 久久久久视频综合| av国产精品久久久久影院| 精品国产国语对白av| 超碰97精品在线观看| 欧美亚洲日本最大视频资源| svipshipincom国产片| 91大片在线观看| 麻豆乱淫一区二区| 十八禁网站免费在线| 国产精品二区激情视频| 亚洲精品在线观看二区| 人妻 亚洲 视频| 天堂动漫精品| 免费女性裸体啪啪无遮挡网站| 丝袜人妻中文字幕| 国产成人免费观看mmmm| 伦理电影免费视频| 成人精品一区二区免费| 亚洲色图av天堂| www.自偷自拍.com| 日韩 欧美 亚洲 中文字幕| 成年人免费黄色播放视频| 久久人妻熟女aⅴ| 久久久久久久精品吃奶| 大片电影免费在线观看免费| av免费在线观看网站| 国产高清激情床上av| videosex国产| 又大又爽又粗| 国产麻豆69| 成熟少妇高潮喷水视频| 午夜福利影视在线免费观看| 久久婷婷成人综合色麻豆| 国产av一区二区精品久久| 免费人成视频x8x8入口观看| 国产精品永久免费网站| 亚洲三区欧美一区| 午夜福利,免费看| 久久精品91无色码中文字幕| 欧美国产精品一级二级三级| 欧美日韩精品网址| 国产免费av片在线观看野外av| 日韩大码丰满熟妇| 男女高潮啪啪啪动态图| 建设人人有责人人尽责人人享有的| 亚洲精品一二三| 国产精品久久视频播放| 久久人妻av系列| 又紧又爽又黄一区二区| 国产淫语在线视频| 一本一本久久a久久精品综合妖精| 人妻一区二区av| 99热只有精品国产| 国产午夜精品久久久久久| 在线观看免费日韩欧美大片| av一本久久久久| 精品国产超薄肉色丝袜足j| 久久中文看片网| 国产极品粉嫩免费观看在线| 免费在线观看视频国产中文字幕亚洲| 亚洲国产毛片av蜜桃av| 夜夜爽天天搞| 免费在线观看日本一区| 黄网站色视频无遮挡免费观看| 欧美黑人欧美精品刺激| 一进一出抽搐动态| 曰老女人黄片| 两个人免费观看高清视频| 制服诱惑二区| 日日夜夜操网爽| 色在线成人网| 欧美在线一区亚洲| 91大片在线观看| 亚洲av成人不卡在线观看播放网| 丝袜美腿诱惑在线| 狂野欧美激情性xxxx| 少妇 在线观看| 欧美日韩中文字幕国产精品一区二区三区 | 成年女人毛片免费观看观看9 | 午夜免费观看网址| 国产国语露脸激情在线看| 欧美人与性动交α欧美软件| 男女床上黄色一级片免费看| 99热网站在线观看| 精品福利观看| 欧美日本中文国产一区发布| 精品国产一区二区久久| 一二三四在线观看免费中文在| 老司机影院毛片| 国产成人啪精品午夜网站| 身体一侧抽搐| 人妻 亚洲 视频| 亚洲人成电影免费在线| 又黄又粗又硬又大视频| 亚洲视频免费观看视频| 午夜精品久久久久久毛片777| 久久久久久久久免费视频了| 国产高清视频在线播放一区| 成在线人永久免费视频| 自拍欧美九色日韩亚洲蝌蚪91| av免费在线观看网站| 欧美黑人欧美精品刺激| 亚洲成a人片在线一区二区| 下体分泌物呈黄色| 国产精品二区激情视频| 免费不卡黄色视频| 亚洲欧美精品综合一区二区三区| 黄色视频不卡| 老司机福利观看| 久久久久久免费高清国产稀缺| 亚洲av电影在线进入| 色综合欧美亚洲国产小说| 精品一区二区三区视频在线观看免费 | www日本在线高清视频| 另类亚洲欧美激情| 国产精品美女特级片免费视频播放器 | 亚洲精品一卡2卡三卡4卡5卡| 在线天堂中文资源库| 首页视频小说图片口味搜索| 成人精品一区二区免费| 97人妻精品一区二区三区麻豆| 在线观看午夜福利视频| 免费av观看视频| 宅男免费午夜| 国产成人系列免费观看| 国产亚洲av嫩草精品影院| 亚洲欧美日韩东京热| 国产一区二区三区在线臀色熟女| 亚洲午夜理论影院| 综合色av麻豆| 亚洲国产日韩欧美精品在线观看 | 国产探花极品一区二区| а√天堂www在线а√下载| 9191精品国产免费久久| 国产精品爽爽va在线观看网站| 国产探花在线观看一区二区| 床上黄色一级片| 亚洲在线观看片| 日韩欧美三级三区| 真实男女啪啪啪动态图| 国产真实伦视频高清在线观看 | 亚洲人成网站在线播放欧美日韩| 88av欧美| 亚洲av第一区精品v没综合| 国产黄色小视频在线观看| 男女那种视频在线观看| 2021天堂中文幕一二区在线观| 久久久久国内视频| 91在线观看av| 国产精品免费一区二区三区在线| av片东京热男人的天堂| 亚洲人成网站在线播放欧美日韩| 嫩草影院精品99| 久久国产精品人妻蜜桃| 亚洲av成人不卡在线观看播放网| 天天躁日日操中文字幕| 天堂av国产一区二区熟女人妻| 亚洲美女视频黄频| 一级作爱视频免费观看| 成年版毛片免费区| 九九热线精品视视频播放| 黄色丝袜av网址大全| 亚洲精品一区av在线观看| 欧美成人一区二区免费高清观看| 国产激情欧美一区二区| 欧美bdsm另类| 久久午夜亚洲精品久久| 757午夜福利合集在线观看| 床上黄色一级片| 久久伊人香网站| 亚洲真实伦在线观看| 欧美乱妇无乱码| 欧美激情久久久久久爽电影| 久久精品综合一区二区三区| 色尼玛亚洲综合影院| 人人妻,人人澡人人爽秒播| 亚洲精品久久国产高清桃花| 国产亚洲精品一区二区www| www.色视频.com| 国产视频内射| 不卡一级毛片| 91久久精品国产一区二区成人 | 亚洲美女黄片视频| 久久久国产成人免费| 岛国在线观看网站| 一个人免费在线观看的高清视频| 两个人看的免费小视频| 欧美在线黄色| 亚洲人与动物交配视频| 成人特级黄色片久久久久久久| 91在线精品国自产拍蜜月 | 免费电影在线观看免费观看| 操出白浆在线播放| 岛国在线观看网站| 久久久国产精品麻豆| 国产精品久久电影中文字幕| 欧美+亚洲+日韩+国产| 亚洲精品影视一区二区三区av| 久久久久免费精品人妻一区二区| 亚洲国产欧洲综合997久久,| 亚洲avbb在线观看| 国产三级中文精品| 夜夜爽天天搞| 啦啦啦韩国在线观看视频| 国产高清激情床上av| 亚洲人成电影免费在线| 久久国产精品影院| 少妇裸体淫交视频免费看高清| 亚洲人成网站高清观看| 五月伊人婷婷丁香| 亚洲国产色片| 欧美大码av| 国产高潮美女av| 亚洲熟妇中文字幕五十中出| 午夜福利在线观看吧| 中文字幕av在线有码专区| 高清日韩中文字幕在线| 免费在线观看成人毛片| 精品电影一区二区在线| 最新在线观看一区二区三区| 少妇丰满av| 亚洲精品乱码久久久v下载方式 | 人人妻人人看人人澡| 天天添夜夜摸| 国产精品一区二区三区四区免费观看 | 亚洲国产日韩欧美精品在线观看 | 亚洲 欧美 日韩 在线 免费| 国产亚洲av嫩草精品影院| 国产高潮美女av| 亚洲人成伊人成综合网2020| 3wmmmm亚洲av在线观看| 色综合欧美亚洲国产小说| 村上凉子中文字幕在线| 国产日本99.免费观看| 日本一本二区三区精品| 91九色精品人成在线观看| 国产成人福利小说| 日韩欧美在线二视频| 国产三级中文精品| 51国产日韩欧美| 色老头精品视频在线观看| 亚洲欧美日韩卡通动漫| 国产av麻豆久久久久久久| 成人三级黄色视频| 免费在线观看亚洲国产| 日韩人妻高清精品专区| 嫩草影院入口| 国产乱人伦免费视频| 久久久久久久精品吃奶| 无限看片的www在线观看| 19禁男女啪啪无遮挡网站| 一本精品99久久精品77| 午夜影院日韩av| 亚洲精品影视一区二区三区av| 免费av观看视频| 十八禁网站免费在线| 亚洲av电影不卡..在线观看| 91字幕亚洲| 久久久久九九精品影院| 白带黄色成豆腐渣| 亚洲五月婷婷丁香| 神马国产精品三级电影在线观看| 校园春色视频在线观看| 久久中文看片网| 免费一级毛片在线播放高清视频| 18禁美女被吸乳视频| 一级黄色大片毛片| 在线观看免费午夜福利视频| 美女大奶头视频| av黄色大香蕉| 国产黄a三级三级三级人| 亚洲一区二区三区不卡视频| 一区二区三区免费毛片| 久久久久久九九精品二区国产| av片东京热男人的天堂| 国产伦精品一区二区三区视频9 | 大型黄色视频在线免费观看| 老司机午夜福利在线观看视频| 高清毛片免费观看视频网站| 久久国产精品影院| 国产淫片久久久久久久久 | 日韩欧美一区二区三区在线观看| 成人一区二区视频在线观看| 精品免费久久久久久久清纯| 成人特级黄色片久久久久久久| 欧美极品一区二区三区四区| 久久精品国产综合久久久| 国语自产精品视频在线第100页| 中文字幕熟女人妻在线| 麻豆一二三区av精品| 国产国拍精品亚洲av在线观看 | 特大巨黑吊av在线直播| 免费看a级黄色片| 女警被强在线播放| 人妻夜夜爽99麻豆av| 国产亚洲av嫩草精品影院| 久久香蕉精品热| 久久久久国内视频| 三级男女做爰猛烈吃奶摸视频| 欧美zozozo另类| 在线十欧美十亚洲十日本专区| 最近视频中文字幕2019在线8| 成人精品一区二区免费| 亚洲国产欧美人成| 欧美最黄视频在线播放免费| 老汉色av国产亚洲站长工具| xxx96com| 97超视频在线观看视频| 丰满人妻熟妇乱又伦精品不卡| 国产真人三级小视频在线观看| 女人被狂操c到高潮| 亚洲美女黄片视频| 欧美3d第一页| 午夜福利18| 女人被狂操c到高潮| 亚洲自拍偷在线| 国产69精品久久久久777片| 亚洲乱码一区二区免费版| 成年免费大片在线观看| 男人舔奶头视频| 国产成人av教育| 亚洲av成人不卡在线观看播放网| 亚洲人与动物交配视频| 伊人久久大香线蕉亚洲五| 国产成人av教育| 神马国产精品三级电影在线观看| 非洲黑人性xxxx精品又粗又长| 成人国产一区最新在线观看| 亚洲人与动物交配视频| 日韩精品青青久久久久久| 亚洲人成伊人成综合网2020| 精品人妻1区二区| 日本黄色片子视频| 午夜福利18| 国产精品久久久久久久久免 | 1000部很黄的大片| 99精品久久久久人妻精品| 欧美一区二区精品小视频在线| 亚洲成人久久爱视频| 男人舔奶头视频| 国产69精品久久久久777片| 搡老岳熟女国产| 性欧美人与动物交配| 精品久久久久久,| 久久精品国产99精品国产亚洲性色| 精品久久久久久,| www国产在线视频色| av国产免费在线观看| 欧美另类亚洲清纯唯美| 日本 av在线| 国产在视频线在精品| 88av欧美| 99热精品在线国产| 欧美一区二区国产精品久久精品| 日韩欧美在线乱码| 欧美性猛交╳xxx乱大交人| 香蕉久久夜色| 免费大片18禁| 搞女人的毛片| 少妇人妻精品综合一区二区 | 午夜精品一区二区三区免费看| 国产一区二区亚洲精品在线观看| 在线国产一区二区在线| 听说在线观看完整版免费高清| 欧美乱色亚洲激情| 亚洲av熟女| 麻豆成人av在线观看| tocl精华| 久久欧美精品欧美久久欧美| 狂野欧美激情性xxxx| 国产主播在线观看一区二区| 一本精品99久久精品77| 国产成人福利小说| 亚洲成av人片在线播放无| 国产黄色小视频在线观看| 老熟妇乱子伦视频在线观看| 最后的刺客免费高清国语| 日本黄大片高清| 中文字幕精品亚洲无线码一区| 亚洲成人精品中文字幕电影| 法律面前人人平等表现在哪些方面| 国产精品一及| 脱女人内裤的视频| 国产精品爽爽va在线观看网站| 天天一区二区日本电影三级| 免费人成视频x8x8入口观看| 亚洲中文字幕日韩| 操出白浆在线播放| 免费看a级黄色片| 人妻久久中文字幕网| 日韩欧美一区二区三区在线观看| 亚洲在线自拍视频| 露出奶头的视频| 99国产精品一区二区三区| 午夜老司机福利剧场| 悠悠久久av| 日本撒尿小便嘘嘘汇集6| 国产一区在线观看成人免费| 亚洲天堂国产精品一区在线| 19禁男女啪啪无遮挡网站| 国产熟女xx| 老鸭窝网址在线观看| 午夜福利在线观看免费完整高清在 | 手机成人av网站| 欧美在线一区亚洲| 亚洲成人免费电影在线观看| 热99re8久久精品国产| 国产精品香港三级国产av潘金莲| 黑人欧美特级aaaaaa片| 一个人免费在线观看的高清视频| 91九色精品人成在线观看| 少妇裸体淫交视频免费看高清| 91在线观看av| 男女之事视频高清在线观看| 国产亚洲精品综合一区在线观看| 天天添夜夜摸| 成年版毛片免费区| 午夜精品在线福利| 人人妻,人人澡人人爽秒播| 欧美黄色淫秽网站| 男人舔女人下体高潮全视频| 亚洲在线自拍视频| 乱人视频在线观看|