<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">JAMP</journal-id><journal-title-group><journal-title>Journal of Applied Mathematics and Physics</journal-title></journal-title-group><issn pub-type="epub">2327-4352</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jamp.2015.35071</article-id><article-id pub-id-type="publisher-id">JAMP-56757</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Fatigue Crack Analysis on the Bracket of Sanding Nozzle of CRH5 EMU Bogie
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>elong</surname><given-names>Fu</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Tao</surname><given-names>Zhang</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Changchun Railway Vehicle Co., Ltd., Changchun, China</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>dragonfdl@163.com(EF)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>11</day><month>05</month><year>2015</year></pub-date><volume>03</volume><issue>05</issue><fpage>577</fpage><lpage>583</lpage><history><date date-type="received"><day>20</day>	<month>April</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>24</month>	<year>May</year>	</date><date date-type="accepted"><day>28</day>	<month>May</month>	<year>2015</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  Aiming at the fracture of the bracket of sanding nozzle of CRH5 EMU bogie, the fatigue strength analysis and modal analysis of the bracket were conducted according to En13749 and BS7608 standards, and the track excitation during the vehicle running was thoroughly analyzed. The cause leading to the fracture of the bracket was found and the bracket was redesigned.
 
</p></abstract><kwd-group><kwd>Bracket of Sanding Nozzle</kwd><kwd> Model Analysis</kwd><kwd> Track Excitation</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>With the development of high-speed train and the increase of the speed, some non-sustaining components of the bogie are affected by the wheel-rail excitation and the fatigue fractures thus often occur. Fatigue failure is not only related to the amplitude of vibration, but also associated with the vibration frequency. Once, cracks appear on the bracket of sanding nozzle of CRH5 EMU bogie after for 1,200,000 kilometers operation. Aiming at this fatigue fracture, the fatigue strength analysis and modal analysis of the bracket structure were conducted in this paper. Based on the modal theory, the natural vibration modes and track excitation were combined to be analyzed. The cause of the fatigue crack was found, which provided a basis for the improvement of subsequent structural design.</p></sec><sec id="s2"><title>2. Introduction to the Structure of the Sander and Finite Element Model</title><p>A sander is mounted on the side sill end of the CRH5 EMU bogie, as shown in Figures 1(a)-(b). The sanding device is fixed on the side sill by bolts, and the nozzle bracket is connected to the sander; the baffle is fixed on the end of the side beam; the baffle, the nozzle bracket, the heating box and the nozzle are connected by bolts.</p><fig-group id="fig1"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> (a) Sander unit. (b) 3D model of sander.</title></caption><fig id ="fig1_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/14-1720293x5.png"/></fig><fig id ="fig1_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/14-1720293x6.png"/></fig></fig-group><p>The cracks occurred at the welding end of the rib plate, as shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>.</p><p>In the finite element analysis, the sander was discretized by shell elements. The bolts connection was modeled using the bond constraints. The model totally consisted of 19,862 elements and 17,313 nodes. The hose and the bolts were ignored in the model. The joint of components and sander structure is considered as fixed constraint and the FEM model is shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>.</p></sec><sec id="s3"><title>3. Model Analysis</title><p>The sander is mounted on the end of bogie side beam, which would undertake complex loading condition in the process of train’s running. In addition, the sander will vibrate under the excitation of trail-wheel interaction due to its complex structure. Therefore, modal analysis on the whole sander system should be carried out, thereby the natural frequency range and the main vibration modes of the sander structure can be understood clearly so as to find the critical weak links sensitive to stress and the cause of cracks, providing the basis for structural improvement.</p><p>The results of modal analysis of the whole sander are shown in <xref ref-type="fig" rid="fig4">Figure 4</xref>. The first-order natural frequency is only 47.8 Hz, corresponding to the axial vibration of the connection region of nozzle bracket with the lower part of the sander and producing a relatively large stress. Taking into account the additional mass of sand-spurting hose and control cable connected to the sander bracket, and an elastic suspension support, the first-order natural frequency of the structure should be even lower. Based on experience, the first-order natural frequency is comparatively low.</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Crack on the nozzle bracket</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/14-1720293x7.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> FEA model of sander</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/14-1720293x8.png"/></fig></sec><sec id="s4"><title>4. Strength Analysis</title><p>The whole sander is installed on the end of the bracket frame. According to the En13749 [<xref ref-type="bibr" rid="scirp.56757-ref1">1</xref>] standard, the exceptional acceleration loads which caused by the additional mass and attached to the bogie frame end are vertical &#177;6 g and lateral &#177;2 g respectively; the normal acceleration loads are vertical &#177;3 g and lateral &#177;1 g respectively. Under the combined action of vertical 3 g and lateral 1 g acceleration loads, the movement of nozzle bracket is a longitudinal swing, and the principal stress contour is shown in <xref ref-type="fig" rid="fig5">Figure 5</xref>. At the rib plate welding end of nozzle bracket inner side, there is an obvious stress concentration; and through interpolation calculation, the maximum stress at weld toe is about 15.7 Mpa.</p></sec><sec id="s5"><title>5. Analysis of Wheel-Rail Excitation</title><p>When the vehicle is running, the wheel-rail interaction produces an excitation on the vehicle system. According to the test data [<xref ref-type="bibr" rid="scirp.56757-ref2">2</xref>] , the irregularities of high speed railway is very obvious, the high-frequency part of the wavelength is located in 1.4 m, 2.8 m, 6.5 m, etc. Among them, 2.8 m is close to the wheel circumference, so this frequency primarily reflects the wheel’s dynamic unbalance; 1.4 m is half the wheel circumfe-</p><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> First mode of sander</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/14-1720293x9.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> The principal stress contour of nozzle bracket</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/14-1720293x10.png"/></fig><p>rence, it is the reflection of wheel’s ellipticity; 6.5 m is the length of track plate, so the frequency is caused by the forced vibration of track slab. In consideration of the wheel diameter 890 mm, when the train runs at a speed of 200 km/h, the corresponding excitation frequency is 40 Hz, 20 Hz and 8.55 Hz respectively; when the train is running at a speed of 250 km/h, the excitation frequency is 49.6 Hz, 24.8 Hz and 10.68 Hz respectively.</p><p>So, no matter whether the train runs at 200 km/h or 250 km/h, the wheel-rail excitation frequencies are all close to the natural frequencies of the sand. The wheel-rail excitation is a kind of forced vibration input, assuming the displacement of the bracket is <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x11.png" xlink:type="simple"/></inline-formula> under the acceleration load <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x12.png" xlink:type="simple"/></inline-formula> and the displacement of nozzle bracket due to the excitation of wheel-rail is v, according to the dynamic theory of [<xref ref-type="bibr" rid="scirp.56757-ref3">3</xref>] , the dynamic amplifying coefficient caused by the excitation is:</p><disp-formula id="scirp.56757-formula931"><graphic  xlink:href="http://html.scirp.org/file/14-1720293x13.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x14.png" xlink:type="simple"/></inline-formula> is the ratio of excitation frequency to structural natural frequency; <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x15.png" xlink:type="simple"/></inline-formula>is the ratio of</p><p>structural damping to critical damping, namely, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x16.png" xlink:type="simple"/></inline-formula>, usually<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x17.png" xlink:type="simple"/></inline-formula>.</p><p>Suppose train’s running speed is 200 km/h, means<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x18.png" xlink:type="simple"/></inline-formula>, then<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x19.png" xlink:type="simple"/></inline-formula>, and the amplifying</p><p>coefficient<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x20.png" xlink:type="simple"/></inline-formula>. Also<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x21.png" xlink:type="simple"/></inline-formula>, the strain is a derivative of displacement, which means that</p><p>under the excitation of this frequency, the stress will be 2.89 times as much as the normal value in stiffened plate.</p><p>At the same time, the vibration acceleration is the two-order derivative of displacement, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/14-1720293x22.png" xlink:type="simple"/></inline-formula>, and the vibration acceleration of local position of nozzle bracket will become larger, leading to abnormal vibration.</p></sec><sec id="s6"><title>6. Fatigue Analysis</title><p>According to the BS7608 standard in [<xref ref-type="bibr" rid="scirp.56757-ref4">4</xref>] , in the welding structure similar to the stiffener, it is easy to produce cracks at the weld toe, and the weld type and failure are shown in <xref ref-type="fig" rid="fig6">Figure 6</xref>. This type of weld joint corresponding to F grade; when the corresponding number of cycles is 10<sup>7</sup>, the stress range is 40 Mpa, as shown in <xref ref-type="fig" rid="fig7">Figure 7</xref>. Under the load of vertical 1 g and transverse 3 g, the stress at the weld toe position of rib plate welding end is about 15.7 Mpa. Due to an amplification effect of wheel-rail excitation, the stress range could reach up to 90.7 Mpa, far beyond the fatigue limit of F grade for welded joints. It is clear that, no matter whether the train runs at the speed of 250 km/h or 200 km/h, the fatigue strength of the sanding nozzle bracket cannot meet the requirements.</p></sec><sec id="s7"><title>7. Improved Structure</title><p>It can be seen from the above analysis that the wheel-rail excitation frequency is close to the first-order natural frequency of sander. When the train is running, the first-order mode can be easily excited, resulting in abnormal vibration on the nozzle bracket and making the stress at the end of the internal welding rib plate exceed the fatigue limit. Based on this, we optimized the design of the sanding nozzle structure, aiming to increase the first-order natural frequency of the nozzle seat, or trying to avoid the stress concentration at the rib plate welding end of nozzle bracket inner side. The improved structure is shown in <xref ref-type="fig" rid="fig8">Figure 8</xref>. Its main structure remained unchanged but the installation base of the sander was widened in order to adapt to the new structure of stiffened welding plate. And the stiffened plate was extended to the baffle and the sander installation base; a piece of small rib plate was added to the middle part of the baffle to increase the baffle plate bending strength; the diameter of the holes in the sanding nozzle bracket and sander installation base were reduced from 70 mm to 50 mm. This improved structure has operated for 2,000,000 km running totally without any problems.</p></sec><sec id="s8"><title>8. Conclusion</title><p>This paper used a method combining dynamic analysis with fatigue strength to conduct an in-depth study on the bogie sanding nozzle bracket structure, which took into account the intrinsic vibration mode of structure and rail</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Welding class</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/14-1720293x23.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Designed S-N curve in BS7608</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/14-1720293x24.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Improved structure of the support bracket</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/14-1720293x25.png"/></fig><p>track excitation, then the reason that caused fatigue damage on the sanding nozzle bracket was found. On the basis of above analyses, the nozzle bracket structure was redesigned. The fatigue strength design method based on structural modal analysis has important theoretical significance and engineering value for the structural design of non-sustaining bogie components.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.56757-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">En13749 (2005) Railway Applications-Wheelsets and Bogies-Method of Specifying Structural Requirements of Bogie Frames.</mixed-citation></ref><ref id="scirp.56757-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Zhang S.G. (2009) Study on the Design Method of High Speed Train. China Railway Publishing House, Beijing.</mixed-citation></ref><ref id="scirp.56757-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Clough, R. and Penzien, J. (2006) Dynamics of Structures. Chinese Edition, Higher Education Press, Beijing.</mixed-citation></ref><ref id="scirp.56757-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">BSI (1993) BS7608: Code of Practice for Fatigue Design and Assessment of Steel Structures. British Standards Institution, London.</mixed-citation></ref></ref-list></back></article>