GMW GMW14164-2012 Torque Tension Angle and Compression Evaluation of Fastened Joints Issue 2 English.pdf
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1、 WORLDWIDE ENGINEERING STANDARDS Test Procedure GMW14164 Torque, Tension, Angle, and Compression Evaluation of Fastened Joints Copyright 2012 General Motors Company All Rights Reserved November 2012 Originating Department: North American Engineering Standards Page 1 of 14 1 Scope Note: Nothing in th
2、is standard supercedes applicable laws and regulations. Note: In the event of conflict between the English and domestic language, the English language shall take precedence. 1.1 Purpose. To determine the dynamic torque, tension, angle, and compression characteristics of the threaded fastener joint w
3、ith bushing inner sleeve as compressed member. 1.2 Foreword. 1.2.1 Limitations. This procedure does not apply to Pulse tools. 1.2.2 Unless otherwise specified, any requirements or direction provided in the Test Request documentation will supercede this test procedure. 1.3 Applicability. Unless other
4、wise specified, this procedure applies to the initial tightening event of joints using new threaded fasteners, bearing surfaces and clamped members for each joint. 2 References Note: Only the latest approved standards are applicable unless otherwise specified. 2.1 External Standards/Specifications.
5、None 2.2 GM Standards/Specifications. GMW25 2.3 Additional References. Data Acquisition System Manufacturers Operating Procedure D.C. Electric Tool Manufacturers Operating Procedure 3 Resources 3.1 Facilities. GM approved laboratory or location for this test procedure. 3.2 Equipment. 3.2.1 Torque an
6、gle transducer. 3.2.2 Data acquisition system capable of collecting data at a sampling rate of at least 1000 Hz, plotting data at user specified scales, and identifying data at all points on the curve. 3.2.3 Strain gaged fastener, force washer, or fastener prepared for ultrasonic measurement. 3.2.4
7、Ultrasonic measurement device (if required). 3.2.5 Strain gaged bushing inner sleeves. 3.2.6 Load frame. 3.2.7 Tightening tool. 3.2.8 Appropriate fixturing, adapters, bedplate, or slotted table. 3.2.9 Strain indicator. 3.3 Test Vehicle/Test Piece. 3.3.1 A complete bill of materials of required test
8、pieces will be specified in the Test Request documentation. Copyright General Motors Company Provided by IHS under license with General Motors CompanyNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-GM WORLDWIDE ENGINEERING STANDARDS GMW14164 Copyright 2012 General
9、Motors Company All Rights Reserved November 2012 Page 2 of 14 3.3.2 Unless otherwise specified, a minimum of eight joints are to be used for this procedure plus a minimum of two additional bushing inner sleeves for bushing load deflection test. 3.4 Test Time. Calendar time: 1 to 2 weeks Test hours:
10、24 hours Coordination hours: 8 hours 3.5 Test Required Information. Test Request documentation should outline specific information and test parameters (reference Appendix A). 3.6 Personnel/Skills. Test Technician shall be qualified on the basis of appropriate education, training, experience and/or d
11、emonstrated skills. 4 Procedure 4.1 Preparation. 4.1.1 Bushing Load Deflection Test. 4.1.1.1 Fasteners, bushings, and associated components should be inspected for conformity to specification (including surface specification for ends of bushing, dimensional measurements on the sleeve and brackets, o
12、r a measurement of the gap between them) per applicable drawing(s) or as directed by the test requestor. 4.1.1.2 Install the adapters in the load frame. Install and hook up the instrumentation. The linear displacement measurement device should be mounted so that it measures between the adapters of t
13、he ram and the plate in as direct a manner as possible with its centerline as close to the ram centerline as the test parts will permit. Fixturing deflection may be erroneously interpreted as test part deflection if care is not exercised in the setup. 4.1.1.3 Calibrate the instrumentation to record
14、expected full scale values for force and deflection. 4.1.1.4 Run a force-deflection test up to maximum requested load with fixturing and adapters alone (no test parts). If desired to minimize load frame height readjustment, a solid steel block with parallel sides and height similar to bushing may be
15、 placed between the load frame adapters. 4.1.1.5 Start the recording device and begin loading the fixturing. 4.1.1.6 Continue increasing the force until the maximum requested load is achieved. 4.1.1.7 Decrease the load to 0 while still recording. 4.1.1.8 If requested, repeat 4.1.1.4 through 4.1.1.7.
16、 4.1.1.9 Remove the inner sleeve from a bushing assembly by cutting away the surrounding metal and rubber. Do not damage bushing inner sleeve. Inner sleeves may be available separately from bushings for prototype level parts. 4.1.1.10 Install the bushing inner sleeve test specimen into the load fram
17、e to load the sleeve axially. 4.1.1.11 Start the recording device and begin loading the bushing. Use displacement control at a rate of 0.1 mm/s. 4.1.1.12 Continue increasing the force until the maximum requested load is achieved. Test shutoff parameters may include, but are not limited to: 4.1.1.12.
18、1 One hundred ten percent (110%) of fastener proof load. 4.1.1.12.2 Onset of permanent bushing deformation. 4.1.1.12.3 Load capability of the load frame and/or load cell. 4.1.1.13 Decrease the load to 0 while still recording. 4.1.1.14 Optional: Repeat 4.1.1.10 through 4.1.1.13 using a complete bushi
19、ng assembly (inner sleeve plus surrounding metal and rubber still intact). 4.1.1.15 Repeat 4.1.1.10 through 4.1.1.14 for the total number of samples requested. 4.1.1.16 Visually inspect the test parts and record if or how they were deformed. 4.1.1.17 Photograph the test setup and the test components
20、 after test. Copyright General Motors Company Provided by IHS under license with General Motors CompanyNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-GM WORLDWIDE ENGINEERING STANDARDS GMW14164 Copyright 2012 General Motors Company All Rights Reserved November 201
21、2 Page 3 of 14 4.1.1.18 Review load vs. displacement plots with test requestor. Curve from sample with fixturing and adapters alone (no test parts) should be linear with minimal offset Curves from bushing inner sleeve and complete bushing assembly samples should be linear up to desired calibration l
22、oad, which is to be 110% of fastener proof load unless otherwise specified by test requestor. 4.1.2 Bushing Strain Gaging and Calibration. 4.1.2.1 Remove the remaining inner sleeves from the bushing assemblies by cutting away the surrounding metal and rubber. Do not damage bushing inner sleeve. Inne
23、r sleeves may be available separately from bushings for prototype level parts. 4.1.2.2 If there are teeth or serrations on the ends of the sleeves, then aluminum plates should be used between the loading device and sleeve ends. 4.1.2.3 Optional: Cycle inner sleeves at least five times up to the desi
24、red calibration load of the sleeve then back down to zero load on a load frame. To remove residual stresses in the sleeves (work hardening processes), operate at a slow ram rate. 4.1.2.4 Attach strain gages on the inner sleeves, full bridge wired for axial loading, and cycle at least five times. 4.1
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