AGMA 99FTM3-1999 Measurement Uncertainty for Pitch and Runout Artifacts《齿距和圆跳动标准器的测量不确定度》.pdf
《AGMA 99FTM3-1999 Measurement Uncertainty for Pitch and Runout Artifacts《齿距和圆跳动标准器的测量不确定度》.pdf》由会员分享,可在线阅读,更多相关《AGMA 99FTM3-1999 Measurement Uncertainty for Pitch and Runout Artifacts《齿距和圆跳动标准器的测量不确定度》.pdf(16页珍藏版)》请在麦多课文档分享上搜索。
1、I Measurement Uncertainty for Pitch and Runout Artifacts by: B. Cox, Lockheed Martin Energy Systems, Inc. TECHNICAL PAPER COPYRIGHT American Gear Manufacturers Association, Inc.Licensed by Information Handling Servicesa Measurement Uncertainty for Pitch and Runout Artifacts Bruce Cox, Lockheed Marti
2、n Energy Systems, Inc. The statements and opinions contained herein,re those of the author and should not be construed as an official action or opinion of the American Gear Manufacturers Association. Abstract Primary-level calibration of pitch and runout artifacts require quantifying the measurement
3、 uncertainty on the artifact being calibrated by a method that does not rely on a transfer comparison. The measurement decomposition method, developed jointly by National Institute of Standardsand Technology (NIST) and Oak Ridge Metrology Center (ORMC) personnel, is used to determine the uncertainty
4、 of each component of the measurement task. Once quantified, these components are added in quadrature according to NISTTechnicalNote 1297,1994 Edition). Verification of this method was accomplished by inter-comparison between ORMC and NIST using high precision coordinate measurement machines and rot
5、ary tables. The results were also compared with data obtained using the circle closure principie. Copyright O 1999 American Gear Manufacturers Association 1500 King Street, Suite 201 Alexandria. Virginia, 22314 October. 1999 ISBN: I-55589-741-X COPYRIGHT American Gear Manufacturers Association, Inc.
6、Licensed by Information Handling ServicesIndex and Runout Artifact Measurement Decomposition In the case of an index and runout artifact, the uncertainty determination consists of checking pitch error using a rotary table and a 1440 Divider by the closure method; checking radial runout of the rotary
7、 table; and checking repeatability using an index artifact. The pitch test which involved repeated measurements on three balls mounted so that a line through the first and second ball centers and a line through the first and third ball centers formed a 15“ angle. In the pitch test, the balls were mo
8、unted on a1440 divider, which was also mounted on the rotary table, see Figure 1. When the divider was rotated 15“, the rotary table was rotated 15“ in the opposite direction. The angle positions were analyzed by using the circle closure method, where all angles must add to 360“. The angle results a
9、re summarized in Table 1. Figure 1 Checking rotary table error using 3 balls and 1440 divider by circle closure 2 COPYRIGHT American Gear Manufacturers Association, Inc.Licensed by Information Handling Services1 Table 1. Pitch test with 3 balls using closure (arcseconds) I I -0.50400 -0.43200 -0.396
10、00 -0.43200 -0.50400 -0.43200 -0.46800 -0.54000 -0.39601 -0.25200 -0.25200 -0.21 600 -0.18000 -0.28800 -0.2 1600 -0.2 160C -0.32400 -0.2520( -0.10800 -0.07200 -0.07200 -0.03600 -0.10800 -0.10800 -0.07200 -0.10800 -0.18001 I -0.4680a -0.54000( -0.1440a -0.0360 , I l 0.0000ol 0.00000l The results of 1
11、3 runs of the pitch test, in arcseconds, were a maximum deviation of 0.432 a minimum deviation of -0.972. Using a rectangular distribution the standard deviation is calculated below (in arcseconds): 0.432 - (-0.972) = 0.405 - 2J3 “P - Next, a test was conducted, which involved a known ball mounted i
12、n the center of the rotary table at two heights to determine the radial runout of the table. A ball was mounted on the centerline of the rotary table and the radial runout was measured at two heights above the table, 9 7/8“ and 2 1/2“, see Figure 2. The results are shown below in Table 2: 3 COPYRIGH
13、T American Gear Manufacturers Association, Inc.Licensed by Information Handling ServicesFigure 2 Radial runout test Table 2. Radial Runout Test (mm) Number Radial Runout High Radial Runout Low 9 718“ 2 Y2“ 1 0.00028 0.000 18 2 3 4 1 0.0003 1 0.00014 O. 0003 2 0.000 16 0. 00028 0.000 18 I - 51 0.0003
14、1 0.000171 7 8 I 61 0.0003 11 o. 00022 I 0.0003 1 0.00015 0.0003 1 0.00019 Il 12 I 101 O. 00034 0.0001 0.00032 0.0002 1 0.0003 1 0.000 15 The maximum deviation of the radial runout test at two heights was 0.000340 mm. Taking the arctan of the maximum deviation times sin 20“ divided by the base radiu
15、s of 57.15 mm (simulating a 4.5“ base circle diameter) and multiplying by 3600 to convert to arcseconds gives a total range of 10.420 arcseconds (see Figure 3). 4 COPYRIGHT American Gear Manufacturers Association, Inc.Licensed by Information Handling ServicesA=arctan( Y/57.15)*3600 Figure 3 Calculat
16、ion of angle error due to radial runout The corresponding uncertainty is (in arcseconds): = 0.242 0.420 + 0.420 u, = The index artifact from R. E. Smith, Inc. was used to measure repeatability, see Figure 4. The NIST part program was used with two modifications. Instead of one point being taken at t
17、he pitch diameter, five points were taken at the same location and the average of all points was used. The coordinate system was re-established on the first tooth at every 45“ around the rotary table. One run constitutes eight measurements of each tooth (at every 45“ position). The average of all ei
18、ght measurements on each tooth is the value for each run. The results below in Tables 3 and 4 show the runs, the average of all runs, and the standard deviation of all runs: Figure 4 R. E. Smith index artifact 5 COPYRIGHT American Gear Manufacturers Association, Inc.Licensed by Information Handling
19、ServicesO Table 3. Index Repeatability Runs (Right Flank) Smith gear new 1 pt method i DATE: 12/15/98 12/18/98 12/22/98 12/22/98 12/23/98 12/28/98 12/29/98AVG STD DEV TOOTH # Microns Microns Microns Microns Microns Microns Microns Microns Micron F 1 2 3 4 0.000 0.000 0.000 0.000 0.000 0.000 0.006 0.
20、000 0.000 1.573 1.579 1.863 1.762 1.569 1.595 1.498 1.634. 0.129 -0.059 -0.093 0.048 0.068 -0.083 -0.167 -0.1 14 -0.057 0.086 0.985 1.042 1.255 1.24C 1,010 1.051 1.022 1.086 0.112 10 11 12 13 6 -0.456 -0.311 0.024 -0.111 -0.135 -0.242 -0.321 -0.222 0.160 -0.124 0.065 0.400 0.188 0.189 0.13C 0.059 0.
21、130 0.160 0.805 0.994 1.340 1.113 1.133 1.039 1.028 1.063 0.162 0.333 0.520 0.745 0.508 0.666 0.596 0.593 0.566 0.131 COPYRIGHT American Gear Manufacturers Association, Inc.Licensed by Information Handling Services Table 4. Index Repeatability Runs (Left Hank) The maximum standard deviation for all
22、runs was O. 180 microns. The maximum standard deviation in microns was converted to arcseconds by dividing by the deviation by the 1000* cosine (20“). then taking the arctanent of this product divided by the pitch radius of 78 mm and multiplying by 3600. see Figure 5. . 7 COPYRIGHT American Gear Man
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
5000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- AGMA99FTM31999MEASUREMENTUNCERTAINTYFORPITCHANDRUNOUTARTIFACTS 跳动 标准 测量 不确定 PDF

链接地址:http://www.mydoc123.com/p-422452.html