The Role of Piston Distortion on Lubrication in a Reciprocating EngineSource: Journal of Engineering for Gas Turbines and Power:;1990:;volume( 112 ):;issue: 003::page 287DOI: 10.1115/1.2906494Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The microgeometry of the piston, rings, and skirt relative to the liner strongly influences lubrication in a reciprocating engine. This study develops an approximation technique that decouples the thermomechanical piston-skirt distortions from the complex lubricant support in a large diesel engine. The model considers the limiting case of starved skirt lubrication with large clearance. It permits efficient design of machined three-dimensional piston-skirt contours for piston support. In the calculations, a three-dimensional finite-element model is coupled with a postprocessing algorithm to predict skirt distortions, piston tilt, operating clearance, and oil-film contact area as a function of machined profile, thermal expansion, cylinder pressure, piston inertia, and transient side loads. A piston dynamics model is developed that defines the transient piston side force based on engine geometry, cylinder pressure, inertial loads, and wrist-pin offset. The results of this study indicate that (1) the transient skirt distortions due to cylinder pressure on the compression and power strokes result in a significant increase in oil-film contact area; (2) the piston skirt operating shape depends on the location and area of oil-film contact; (3) the contact area and location during intake and exhaust strokes vary substantially from that during the compression and power strokes; (4) the wrist-pin offset reduces the maximum side load and piston slap intensity occurring in the region of maximum cylinder pressure; (5) effective three-dimensional skirt profile design may result in significant changes in oil-film contact area and location on the skirt throughout the cycle.
keyword(s): Lubrication , Pistons , Piston engines , Pressure , Cylinders , Stress , Clearances (Engineering) , Design , Compression , Cycles , Shapes , Approximation , Algorithms , Diesel engines , Exhaust systems , Finite element model , Geometry , Piston rings , Engines , Lubricants , Thermal expansion , Inertia (Mechanics) , Dynamics (Mechanics) AND Force ,
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| contributor author | W. L. Blair | |
| contributor author | D. P. Hoult | |
| contributor author | V. W. Wong | |
| date accessioned | 2017-05-08T23:32:35Z | |
| date available | 2017-05-08T23:32:35Z | |
| date copyright | July, 1990 | |
| date issued | 1990 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26677#287_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/106894 | |
| description abstract | The microgeometry of the piston, rings, and skirt relative to the liner strongly influences lubrication in a reciprocating engine. This study develops an approximation technique that decouples the thermomechanical piston-skirt distortions from the complex lubricant support in a large diesel engine. The model considers the limiting case of starved skirt lubrication with large clearance. It permits efficient design of machined three-dimensional piston-skirt contours for piston support. In the calculations, a three-dimensional finite-element model is coupled with a postprocessing algorithm to predict skirt distortions, piston tilt, operating clearance, and oil-film contact area as a function of machined profile, thermal expansion, cylinder pressure, piston inertia, and transient side loads. A piston dynamics model is developed that defines the transient piston side force based on engine geometry, cylinder pressure, inertial loads, and wrist-pin offset. The results of this study indicate that (1) the transient skirt distortions due to cylinder pressure on the compression and power strokes result in a significant increase in oil-film contact area; (2) the piston skirt operating shape depends on the location and area of oil-film contact; (3) the contact area and location during intake and exhaust strokes vary substantially from that during the compression and power strokes; (4) the wrist-pin offset reduces the maximum side load and piston slap intensity occurring in the region of maximum cylinder pressure; (5) effective three-dimensional skirt profile design may result in significant changes in oil-film contact area and location on the skirt throughout the cycle. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Role of Piston Distortion on Lubrication in a Reciprocating Engine | |
| type | Journal Paper | |
| journal volume | 112 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2906494 | |
| journal fristpage | 287 | |
| journal lastpage | 300 | |
| identifier eissn | 0742-4795 | |
| keywords | Lubrication | |
| keywords | Pistons | |
| keywords | Piston engines | |
| keywords | Pressure | |
| keywords | Cylinders | |
| keywords | Stress | |
| keywords | Clearances (Engineering) | |
| keywords | Design | |
| keywords | Compression | |
| keywords | Cycles | |
| keywords | Shapes | |
| keywords | Approximation | |
| keywords | Algorithms | |
| keywords | Diesel engines | |
| keywords | Exhaust systems | |
| keywords | Finite element model | |
| keywords | Geometry | |
| keywords | Piston rings | |
| keywords | Engines | |
| keywords | Lubricants | |
| keywords | Thermal expansion | |
| keywords | Inertia (Mechanics) | |
| keywords | Dynamics (Mechanics) AND Force | |
| tree | Journal of Engineering for Gas Turbines and Power:;1990:;volume( 112 ):;issue: 003 | |
| contenttype | Fulltext |