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contributor authorR. B. Mindek
contributor authorT. D. Howes
date accessioned2017-05-08T23:50:05Z
date available2017-05-08T23:50:05Z
date copyrightJuly, 1996
date issued1996
identifier issn1528-8919
identifier otherJETPEZ-26756#620_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116915
description abstractWorkpiece profile accuracy, wheel wear, and thermal damage were investigated for the grinding of slots and vertical faces on MAR-M-247, Inconel 713C, and M-2 tool steel using both alumina and cubic boron nitride (CBN) grinding wheels. It was found when grinding with alumina wheels that the wheel corner and first 2.5 mm of the grinding wheel sidewall account for all the grinding forces in the vertical, horizontal, and transverse directions, and therefore is responsible for all the significant grinding done on the sideface of the workpiece. Since previous work links wheel wear and workpiece thermal damage during grinding to grinding forces, this finding suggests that the area around the wheel corner is the critical region of importance in grinding these types of profiles in terms of wheel wear and the heat input to the workpiece. These, in turn, are linked to workpiece profile accuracy and metallurgical damage. Results also show that striation marks inherent in sidewall grinding can be minimized by controlling the maximum normal infeed rate of the wheel. A method for minimizing the heat input into the workpiece by minimizing grinding force during vertical face grinding is also reported.
publisherThe American Society of Mechanical Engineers (ASME)
titleSlot and Vertical Face Grinding of Aerospace Components
typeJournal Paper
journal volume118
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2816693
journal fristpage620
journal lastpage625
identifier eissn0742-4795
keywordsGrinding
keywordsAerospace industry
keywordsWheels
keywordsForce
keywordsWear
keywordsHeat
keywordsGrinding wheels
keywordsCorners (Structural elements) AND Tool steel
treeJournal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 003
contenttypeFulltext


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