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Principles of naval engineering - Historic Naval Ships Association

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PRINCIPLES OF NAVAL ENGINEERINGequals the pressure on the opposite side <strong>of</strong> theair inlet valve, the inlet valve closes. Air is increasinglycompressed as the piston movestoward TDC; the pressure in the cylinder finallybecomes great enough to force the dischargevalve open against the discharge line pressureand the pressure <strong>of</strong> the valve springs. During thebalance <strong>of</strong> the compression stroke, the air whichhas been compressed in the cylinder is discharged,at almost constant pressure, throughthe open discharge valve.The basic operating cycle just described isrepeated a number <strong>of</strong> times in double actingcompressors and in other stages <strong>of</strong> multistagecompressors. In a double-acting compressor,each stroke <strong>of</strong> the piston is a suction stroke inrelation to one end <strong>of</strong> the cylinder and a compressionstroke in relation to the other end <strong>of</strong>the cylinder. In a double acting compressor,therefore, two basic compression cycles arealways in process when the compressor is operating;but each cycle, considered separately, issimply one suction stroke and one compressionstroke.In multistage compressors, the basic compressioncycle must occur at least once for eachstage <strong>of</strong> compression. If the compressor is designedwith two compressing elements for thefirst (low pressure) stage, two compressioncycles will be in process in the first stage at thesame time. If the compressor is designed so thattwo stages <strong>of</strong> compression occur at the same timein one compressing element, the two basic cycles(one for each stage) will occur at the same time.Compressor ComponentsA reciprocating air compressor consists <strong>of</strong>a compressor element, a lubrication system, acooling system, a control system, and an unloadingsystem. In addition to these basic components,the compressor has a system <strong>of</strong> connectingrods, crankshaft, and flywheel fortransmitting the power developed by the drivingunit to the air cylinder pistons.COMPRESSING ELEMENT. -The compressingelement <strong>of</strong> a reciprocating air compressorconsists <strong>of</strong> the air valves, the cylinder, and thepiston.The valves <strong>of</strong> modern compressorsare<strong>of</strong> theautomatic type. The opening and closing <strong>of</strong> thesevalves is caused solely by the difference betweenthe pressure <strong>of</strong> the air in the cylinder and thepressure <strong>of</strong> the external air on the intake valveor the pressure <strong>of</strong> the discharged air on the dischargevalve. On most compressors, a thin plate,low lift type <strong>of</strong> valve is used. A valve <strong>of</strong> this typeis shown in figure 17-5.The design <strong>of</strong> pistons and cylinders dependsprimarily upon thenumber<strong>of</strong> stages <strong>of</strong> compressionwhich take place within a cylinder. Commonarrangements <strong>of</strong> pistons and cylinders are shownin a previous illustration (fig. 17-2).Two types <strong>of</strong> pistons are in common use.Trunk pistons (fig. 17-6) are driven directly bythe connecting rods. Since the upper end <strong>of</strong> a connectingrod is fitted directly to the piston wristpin, there is a tendency for a piston to develop aside pressure against the cylinder walls. To distributethe side pressure over a wide area <strong>of</strong> thecylinder walls or liners, trunk pistons with longskirts are used. This type <strong>of</strong> piston tends to eliminatecylinder wall wear. Differential pistons(fig. 17-7) are modified trunk pistons having twoor more different diameters. These pistons arefitted into special cylinders which are arrangedso that more than one stage <strong>of</strong> compression isserved by one piston. The compression for onestage takes place over the piston crown; compressionfor theother stage or stages takes placein the annular space between the large and smalldiameters <strong>of</strong> the piston.LUBRICATION SYSTEM.- Lubrication <strong>of</strong> aircompressor cylinders is generally accomplishedby means <strong>of</strong> a mechanical force-feed lubricatorwhich is driven from a reciprocating or a rotarypart <strong>of</strong> the compressor. Oil is fed from the lubricatorthrough a separate feed line to each cylinder.A check valve is installed at the end<strong>of</strong> each feed line to keep the compressed air fromforcing the lube oil back to the lubricator. Eachfeed line is equipped with a sight glass. Lubricationbegins automatically as the compressorstarts up. The amount <strong>of</strong> oil that must be fed tothe cylinders depends upon the cylinder diameter,the cylinder wall temperature, and the viscosity<strong>of</strong> the oil.On small low pressure and medium pressurecompressors, the cylinders may be lubricated bythe splash method, from dippers on the ends <strong>of</strong>the connecting rods, instead <strong>of</strong> by a mechanicalforce-feed lubricator.Lubrication <strong>of</strong> the running gear <strong>of</strong> most compressorsis accomplished by a lube oil pump(usually <strong>of</strong> the gear type) which is attached to thecompressor and driven from the compressorshaft. This pump draws oil from the reservoir,as shown in figure 17-8, and delivers it, through442

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