Principles of naval engineering - Historic Naval Ships Association

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PRINCIPLES OF NAVAL ENGINEERINGFIRST STAGEREDUCTION DRIVECLUTCH'SHAFTH, SELECTOR VALVE.DRIVEN PLATES (FIXED TO GEAR).DRIVING PLATESOUTPUT GEAR.sulEM^SECOND STAGEREDUCTION DRIVEJ^FORWARD DRIVEFROM —^SCAVENGE PUMPPISTON COMPRESSESCLUTCH PLATES ANDOUTPUT GEAR E DRIVEN\ TO COOLER INACTIVE ÂME DIRECTION ASPETON CLUTCH SHAFTDIVERSIONVALVECOUNTERSHAFTREVERSELEGENDDRIVEOIL AT PRESSURENON-ACTIVE OILCOOLING OILRgure 23-20.— Clutch,PETON COMPRESSES CLUTCH PLATESAND OUTPUT GEAR E DRIVEN BYCOUNTERSHAFT IN OPPOSITE DIRECTIONTO CLUTCH SHAFTreduction gear, and reverse gear arrangement.147,153612
Chapter 23. -GAS TURBINEmover in the power plants of many militaryaircraft. When so adapted, the gas turbineengine develops power by converting thermalenergy into mechanical kinetic energy in a highvelocity gas stream. The highly accelerated gasstream creates thrust which propels the aircraft.This methodof creating thrust is called thedirect reaction or jet propulsion method.The concept of thrust is basic to an understandingof jet propulsion. The concept of thrustis based on Newton's third law of motion, whichmay be stated as follows: For every acting forcethere is an equal and opposite reacting force .In the case of aircraft in flight, the acting forceis the force the engine exerts on the air massas itflows through the engine. The reacting force(thrust) is the force which the air mass exertson the components of the engine as the heatedair mass is discharged from the jet nozzle atthe rear of the airplane. In other words, thrustis not produced by the ejected air mass reactingagainst the atmosphere; rather, thrust is createdwithin the engine as the air mass flowingthrough the engine is accelerated and discharged.Engines which include the gas turbine andwhich create thrust by the direct reactionmethod are commonly identified as turbojetengines. Except for a diffuser and a differenttype exhaust system in engines of the turbojettype, the basic components of the turbojet engineare similar in design and function to the componentsof any open-cycle gas turbine engine.The function of the diffuser is to decrease thevelocity of the inlet air and to increase itspressure before the air enters the compressor.The exhaust system of aturbojet engine consistsbasically of a cone and a convergent nozzle.The exhaust cone is designed to exhaust to thenozzle the accelerated air mass which the othercomponents of the engine deliver to the cone.As the accelerated air mass flows through theconvergent nozzle, its velocity is greatly increasedand thrust is created within the engine.MAINTENANCEThe maintenance of gas turbines is thenormal function of operating activities. Cleanlinessis one of the most important basic essentialsin operation and maintenance of gas turbines.Particular care should be exercised inkeeping fuel, air, coolants, lubricants, rotatingelements, and combustion chambers clean. Periodicinspection procedures should be followedin order to detect maladjustments, possiblefailures, and excessive clearances of movingparts. All inspection and maintenance requirementsshould be accomplished in accordancewith the 3-M System (PMS Subsystem).CAUTION : Never use lead pencils for markinggas turbine hot parts, because the carboncontent of the pencil lead will cause stainlesssteel to become brittle, causing a possible failureof the parts that were marked. A greasepencil should be used in marking gas turbineparts. Do not use steel wool to clean gas turbineparts, unless the wool is stainless steel.Overhaul periods and procedures are setup by the Naval Ship Systems Command. Theseperiods and procedures are reported to theFleet through NavShips Technical Manuals and/or direct correspondence. Accurate operatinglogs should be kept on each engine so the numberof hours and operational history on each engineis readily known. These records aid in developingmeasures which improve engine reliability.613
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PRINCIPLES OFNAVAL ENGINEERINGPrepa
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PART l-THE NAVAL SHIPChapter 1Chapt
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CHAPTER 8INTRODUCTION TO THERMODYNA
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CHAPTER 10PROPULSION BOILERSIn the
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CHAPTER13CONDENSERS AND OTHER HEAT
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Page 667 and 668: INDEXComponents and accessories-Con
Page 669 and 670: INDEXMain line shaft bearing, 96Mai
Page 671: INDEXShipboard electrical systems-C
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