000			02039nam a2200253 a 4500
001			vtls000069303
003			KUKTEM
005			20251114204535.0
008			130319t2012 my ao f m 000 0 eng d
020			_aTHE0005929(Local)
039		9	_a201905141453 _baida _y201303191451 _zFida
040			_aUMP
090			_aTA492.R6 N87 2012 rs Bc.
100	0		_aMohd Nur Hilmi Mohd Nazih
245	1	0	_aBMM87 bearing load on a brass pin with aluminium plates / _cMohd Nur Hilmi Mohd Nazih
260			_aKuantan, Pahang : _bUMP, _c2012
300			_axvii, 71 p. : _bill. (some col.) ; _c30 cm. + _e1 CD-ROM
502			_aProject paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2012
504			_aBibliography : p. 62
520	3		_aThe investigation is about the bearing load on a brass pin joined with Aluminium thin plates of variables thickness. The experiment had done using various dimensions of the specimens which is pin diameter, plates thickness and plate thickness to diameter ratio, t/D. The specimens were tested using universal tensile testing machine. The movement for upper crosshead of the testing machine is stopped when the specimen is break. For each specimen, the bearing load was taken and determined from the load vs. displacement graph which is obtained from the Trapezium software in computer that connects with the universal tensile testing machine. The differences dimensions of the specimens give different value of bearing load. By t/D ratio increasing, the higher load pin can support. The higher bearing load is obtained from 5mm brass pin diameter which is 3898.84 N. The finite element analysis ALGOR is use to compare the bearing stress value with experimental test, to choose the more accurate method for other investigation. Finally, the graph of bearing load vs. pin diameter can be used to design brass rivet in the future.
650		0	_aRivets
650		0	_aJoints (Engineering)
999			_aVIRTUA40 _c3793 _d3799
999			_aVTLSSORT0080*0200*0400*0900*1000*2450*2600*3000*5020*5040*5200*6500*6501*9992