Thrust load measuring device for sealed mixing device and calibration method for same
AssigneeKobe Steel, Ltd.
InventorsToru Okada, Yusuke Tanaka
Life of this patent
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AssigneeKobe Steel, Ltd.
InventorsToru Okada, Yusuke Tanaka
Estimating the term…
The relative displacement in the axial direction between an outer ring fixing member or casing and an inner ring fixing member or rotor is determined, said outer ring fixing member being a member for affixing an outer ring of a bearing on one side, and said inner ring fixing member being a member for affixing an inner ring of the bearing on the one end side. When calculating a thrust load acting on the rotor by multiplying the determined relative displacement by a conversion coefficient, an axial force measuring bolt is used as a tightening bolt for affixing the bearing on the one end side, said axial force measuring bolt enabling measurement of a load acting in the axial direction. The axial force measured by the axial force measuring bolt and the relative displacement during measurement of the axial force are used to calibrate the conversion coefficient.
A calibration method for a thrust load measuring device of a hermetically sealed kneader, the hermetically sealed kneader including a pair of rotors that are disposed to be adjacent to each other with a predetermined space therebetween in such a manner that axes are parallel to each other and rotate in directions different from each other, in which a bearing that supports a load applied to each rotor in a radial direction is provided at both end sides of the pair of rotors, and a load applied to each rotor in a thrust direction is supported by the bearing on one end side among from the bearings at both the end sides, the method comprising:
A thrust load measuring device of a hermetically sealed kneader, the hermetically sealed kneader including a pair of rotors that are disposed to be adjacent to each other with a predetermined space therebetween in such a manner that axes are parallel to each other and rotate in directions different from each other, in which a bearing that supports a load applied to each rotor in a radial direction is provided at both end sides of the pair of rotors, and a load applied to each rotor in a thrust direction is supported by the bearing on one end side among from the bearings at both the end sides, the thrust load measuring device comprising:
Dependencies are inferred from the claim text.