Effect of Intercooler on Turbocharged Diesel Engine Performance
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The Effect of Turbocharging on Volumetric Efficiency in Low Heat Rejection C.I. Engine Fueled with Jatrophafor Improved Performance
International Journal of Engineering Research & Technology (IJERT) ISSN: 2278-0181 Vol. 4 Issue 03, March-2015 The Effect of Turbocharging on Volumetric Efficiency in Low Heat Rejection C.I. Engine fueled with Jatrophafor Improved Performance R. Ganapathi *, Dr. B. Durga Prasad** Lecturer, Professor, Mechanical Engineering department, Mechanical Engineering department, JNTUA College of Engineering, JNTUA College of Engineering, Ananthapuramu, A.P, India. Ananthapuramu, A.P, India. burned. This can be achieved with an LHR engine dueto Abstract:- The world’s rapidly dwindling petroleum the availability of higher temperature at the time of fuel supplies, their raising cost and the growing danger of injection. The heat available due to insulation can be environmental pollution from these fuel, have some effectively used for vaporizing alternative fuel. Some substitute of conventional fuels, vegetable oils has been important advantages of the LHR engines are improved fuel considered as one of the feasible substitute to economy, reduced HC and CO emission, reduced noise due conventional fuel. Among all the fuels, tested Jatropha to lower rate of pressure rise and higher energy in the oil properties are almost closer to diesel, particularly exhaust gases [2 & 3]. However, one of the main problems cetane rating and heat value. In present work in the LHR engines is the drop in volumetric experiments are conducted with Brass Crown efficiency. This further decrease the density of air Aluminium piston with air gap, an air gap liner and entering the cylinder because of high wall temperatures of PSZ coated head and valve have been used in the the LHR engine. The degree of degradation of volumetric present study, which generates higher temperature in efficiency depends on the degree of insulation. -
Supercharger
Supercharger 1 4/13/2019 Supercharger Air Flow Requirements • Naturally aspirated engines with throttle bodies rely on atmospheric pressure to push an air–fuel mixture into the combustion chamber vacuum created by the down stroke of a piston. • The mixture is then compressed before ignition to increase the force of the burning, expanding gases. • The greater the mixture compression, the greater the power resulting from combustion. Engineers calculate engine airflow requirements using these three factors: – Engine displacement – Engine revolutions per minute (RPM) – Volumetric efficiency Volumetric efficiency – is a comparison of the actual volume of air–fuel mixture drawn into an engine to the theoretical maximum volume that could be drawn in. – Volumetric efficiency decreases as engine speed increases. 2 4/13/2019 Supercharger Principles of Power Increase: The power output of the engine depend up on the amount of air induced per unit time and thermal efficiency. The amount of air induced per unit time can be increased by: Increasing the engine speed. the increase in engine speed calls for rigid and robust engine as the inertia load increase also the engine fraction and bearing load increase and also the volumetric efficiency decrease. Increasing the density of air at inlet. The increase of inlet air density calls supercharging which usually used to increase the power output from engine due to increase the air pressure at the inlet of engine. 3 4/13/2019 Supercharger The Objects of Supercharging: To increase the power output for a given weight and bulk of the engine. This is important for aircraft, marine and automotive engines where weight and space are important. -
DEUTZ Pose Also Implies Compliance with the Con- Original Parts Is Prescribed
Operation Manual 914 Safety guidelines / Accident prevention ● Please read and observe the information given in this Operation Manual. This will ● Unauthorized engine modifications will in- enable you to avoid accidents, preserve the validate any liability claims against the manu- manufacturer’s warranty and maintain the facturer for resultant damage. engine in peak operating condition. Manipulations of the injection and regulating system may also influence the performance ● This engine has been built exclusively for of the engine, and its emissions. Adherence the application specified in the scope of to legislation on pollution cannot be guaran- supply, as described by the equipment manu- teed under such conditions. facturer and is to be used only for the intended purpose. Any use exceeding that ● Do not change, convert or adjust the cooling scope is considered to be contrary to the air intake area to the blower. intended purpose. The manufacturer will The manufacturer shall not be held respon- not assume responsibility for any damage sible for any damage which results from resulting therefrom. The risks involved are such work. to be borne solely by the user. ● When carrying out maintenance/repair op- ● Use in accordance with the intended pur- erations on the engine, the use of DEUTZ pose also implies compliance with the con- original parts is prescribed. These are spe- ditions laid down by the manufacturer for cially designed for your engine and guaran- operation, maintenance and servicing. The tee perfect operation. engine should only be operated by person- Non-compliance results in the expiry of the nel trained in its use and the hazards in- warranty! volved. -
High Pressure Ratio Intercooled Turboprop Study
E AMEICA SOCIEY O MECAICA EGIEES 92-GT-405 4 E. 4 S., ew Yok, .Y. 00 h St hll nt b rpnbl fr ttnt r pnn dvnd In ppr r n d n t tn f th St r f t vn r Stn, r prntd In t pbltn. n rnt nl f th ppr pblhd n n ASME rnl. pr r vlbl fr ASME fr fftn nth ftr th tn. rntd n USA Copyright © 1992 by ASME ig essue aio Iecooe uoo Suy C. OGES Downloaded from http://asmedigitalcollection.asme.org/GT/proceedings-pdf/GT1992/78941/V002T02A028/2401669/v002t02a028-92-gt-405.pdf by guest on 23 September 2021 Sundstrand Power Systems San Diego, CA ASAC NOMENCLATURE High altitude long endurance unmanned aircraft impose KFT Altitude Thousands Feet unique contraints on candidate engine propulsion systems and HP Horsepower types. Piston, rotary and gas turbine engines have been proposed for such special applications. Of prime importance is the HIPIT High Pressure Intercooled Turbine requirement for maximum thermal efficiency (minimum specific Mn Flight Mach Number fuel consumption) with minimum waste heat rejection. Engine weight, although secondary to fuel economy, must be evaluated Mls Inducer Mach Number when comparing various engine candidates. Weight can be Specific Speed (Dimensionless) minimized by either high degrees of turbocharging with the Ns piston and rotary engines, or by the high power density Exponent capabilities of the gas turbine. pps Airflow The design characteristics and features of a conceptual high SFC Specific Fuel Consumption pressure ratio intercooled turboprop are discussed. The intended application would be for long endurance aircraft flying TIT Turbine Inlet Temperature °F at an altitude of 60,000 ft.(18,300 m). -
Air Filter Sizing
SSeeccoonndd SSttrriikkee The Newsletter for the Superformance Owners Group January 17, 2008 / September 5, 2011 Volume 8, Number 1 SECOND STRIKE CARBURETOR CALCULATOR The Carburetor Controlling the airflow introduces the throttle plate assembly. Metering the fuel requires measuring the airflow and measuring the airflow introduces the venturi. Metering the fuel flow introduces boosters. The high flow velocity requirement constrains the size of the air passages. These obstructions cause a pressure drop, a necessary consequence of proper carburetor function. Carburetors are sized by airflow, airflow at 5% pressure drop for four-barrels, 10% for two-barrels. This means that the price for a properly sized four-barrel is a 5% pressure loss and a corresponding 5% horsepower loss. The important thing to remember is that carburetors are sized to provide balanced performance across the entire driving range, not just peak horsepower. When designing low and mid range metering, the carburetor engineers assume airflow conditions for a properly As with everything in the engine, airflow is power. sized carburetor - one sized for 5% loss at the power peak. Carburetors are a key to airflow. As with any component, the key to best all around performance is to pick parts that match Selecting a larger carburetor than recommended will reduce your performance goal and each other – carburetor, intake, pressure losses at high rpm and may help top end horsepower, heads, exhaust, cam, displacement, rpm range, and bottom but will have lower flow velocity at low rpm and poor end. metering and mixing with a loss in low and mid range power and drivability. -
RECIPROCATING COMPRESSOR PERFORMANCE IMPROVEMENT with RADIAL POPPET VALVES 2009 GMRC Gas Machinery Conference – Atlanta, GA – October 5‐7, 2009
RECIPROCATING COMPRESSOR PERFORMANCE IMPROVEMENT WITH RADIAL POPPET VALVES 2009 GMRC Gas Machinery Conference – Atlanta, GA – October 5‐7, 2009 Lauren D. Sperry, PE & W. Norman Shade, PE ACI Services Inc. ABSTRACT Over the past decade, radial compressor valves and unloaders have been successfully introduced into reciprocating compressors for the gas transmission industry. The unique radial valve system seats multiple rows of poppets over ports in a cylindrical sleeve that replaces the traditional cage and single‐deck valve used in a reciprocating compressor. The radial valve concept has been applied for both suction and discharge valves in a broad range of compressor models and pipeline cylinder classes. Use of these valves has resulted in significant increases in efficiency and reductions in HP/MMSCFD. For cylinder end deactivation, the cylindrical valve guard is moved to slide the poppets off their seats and away from the ports, providing a relatively unobstructed flow path for the gas. The resulting parasitic losses of the deactivated cylinder end approach the losses achieved by complete removal of a traditional valve. Use of radial valves has also been found to significantly increase unit capacity. Some of this increase stems from being able to operate the more efficient radial valved compressor with less unloading, so that there is more effective displacement utilized for the same power input. Moreover, in practice the significant added fixed volumetric clearance inherent in the radial poppet valves has not reduced the measured volumetric efficiency or the capacity as much as traditional theory would predict. This paper will present four case studies that show the actual field operating performance improvements obtained with radial poppet valves on both low speed and high speed compressors, along with laboratory test comparisons, and an explanation of why the capacity can increase even though the fixed clearance increases. -
THERMAL EFFICIENCY", of the Engine
PowerPower FlowFlow andand EfficiencyEfficiency Engine Testing and Instrumentation 1 Efficiencies When the engine converts fuel into power, the process is rather inefficient and only about a quarter of the potential energy in the fuel is released as power at the flywheel. The rest is wasted as heat going down the exhaust and into the air or water. This ratio of actual to potential power is called the "THERMAL EFFICIENCY", of the engine. How much energy reaches the flywheel ( or dynamometer) compared to how much could theoretically be released is a function of three efficiencies, namely: 1. Thermal 2 Mechanical 3. Volumetric Engine Testing and Instrumentation 2 Thermal Efficiency Thermal efficiency can be quoted as either brake or indicated. Indicated efficiency is derived from measurements taken at the flywheel. The thermal efficiency is sometimes called the fuel conversion efficiency, defined as the ratio of the work produced per cycle to the amount of fuel energy supplied per cycle that can be released in the combustion process. Engine Testing and Instrumentation 3 B.S. = Brake Specific Brake Specific Fuel Consumption = mass flow rate of fuel ÷ power output bsHC = Brake Specific Hydrocarbons = mass of hydrocarbons/power output. e.g. 0.21 kg /kW hour Engine Testing and Instrumentation 4 Thermal Efficiency Wc Ps ηt = = m f QHV µ f QHV Wc − work _ per _ cycle Ps − power _ output m f − mass _ of _ fuel _ per _ cycle QHV − heating _ value _ of _ fuel µ f − fuel _ mass _ flow _ rate Specific fuel consumption µ Sfc = f Ps Therefore 1 3600 82.76 ηt = = = Sfc ⋅QHV Sfc(g / kW ⋅hr)QHV (MJ / kg) Sfc Since, QHV for petrol = 43.5 MJ/kg Therefore, the brake thermal efficiency = 82.76/ sfc The indicated thermal efficiency = 82.76 / isfc Engine Testing and Instrumentation 5 Mechanical Efficiency The mechanical efficiency compares the amount of energy imparted to the pistons as mechanical work in the expansion stroke to that which actually reaches the flywheel or dynamometer. -
Technical Info
ENGINE (4G6) – GENERAL 1-1 SECTION 1 ENGINE CONTENTS Engine (4G6)............................................1-1 Fuel System.............................................1-7 General information................................1-1 1. Fuel tank ........................................................1-8 1. Major specifications .......................................1-1 Control System.......................................1-9 2. Engine Performance Curve ...........................1-2 1. Fuel injection control ....................................1-11 Base Engine ............................................1-2 2. Idle speed control.........................................1-11 1. Timing belt cover............................................1-2 3. Ignition timing and distribution 2. Piston.............................................................1-3 control..........................................................1-12 3. Valve spring ...................................................1-3 4. Other controls ..............................................1-12 4. Delivery pipe ..................................................1-4 5. Diagnosis system.........................................1-12 Cooling Equipment.................................1-5 Emission Control System ....................1-13 Intake and Exhaust Equipment .............1-5 Mount .....................................................1-14 1. Air intake system............................................1-5 Engine (4G6) General information The 4G63-T/C engine of the Lancer Evolution-VIII -
AC 23.909-1- Installation of Turbochargers in Small Airplanes
0 Advisory U.S. Department ( of Transportation Federal Aviation Circular Administration Subject: INSTALLATION OF TURBOCHARGERS Date: 2/3/86 AC No: 23. 909- 1 IN SMALL AIRPLANES WITH Initiated by: ACE- 100 Change: RECIPROCATING ENG INES 1. PURPOSE. This advisory circular (AC) provides information and gu idance concerning an acceptable means, but not the only means , of showing comp I iance with Part 23 of the Federal Aviation Regulations (FAR) , applicable to approval procedures and installation of turbochargers in smal I a irplanes. Accordingly, this material is neither mandatory nor regulatory in nature and does not constitute a regulation . 2. RELATED FAR SECTIONS . Section 23 .909 and applicable sections of Part 33 of the FAR (Part 3 of the Civ i I Air Regulations (CAR) does not have a corresponding requirement). 3. BACKGROUND . ( a. Exhaust gas- driven turbochargers are avai I able for use with reciprocat ing engines to: (1) Increase takeoff and maximum continuous power avai I able at sea leve l and a ltitude (turbosupercharged - boosted) . (2) Maintain maximum continuous or cruise powers above sea level altitude (turbonormal ized) . (3) Provtde a source of a ir to pressurize the cabin . NOTE : The word turbocharger wi I I be used throughout this AC to include both turbosupercharged boosted and tur bonormal ized engines . b. Section 23 .909 contains requirements for approval of turbochargers on smal I airp lanes. Th is regulation refers to des ign standards required in Part 33 of the FAR. Part 3 of the CAR does not speciflcal ly cover the approva l requirements for the insta l lation of a turbocharged engine in an airplane . -
Intercooler Pipe Upgrage Kit (Oem Replacement) 2011 - 2016 6.7L Ford | 122011
INTERCOOLER PIPE UPGRAGE KIT (OEM REPLACEMENT) 2011 - 2016 6.7L FORD | 122011 INSTALLATION GUIDE HS-MOTORSPORTS.COMHS-MOTORSPORTS.COM 1 INTERCOOLER PIPE UPGRADE KIT 6.7L FORD TROUBLESHOOTING Please read and understand all installation instructions before proceeding with the installation. If you have questions during the installation of this product, please contact H&S Motorsports support at [email protected] or (855)623-4450. INCLUDED PARTS 1 - HSM Billet Aluminum Throttle Coupler 1 - 5-Ply Stainless-Reinforced Hose Replacement 2 - Stainless T-bolt Clamps STEP 1 Disconnect the vehicle batteries. Disconnect the intake air temperature sensor connector and clip from the back side of the factory intercooler pipe. Disconnect the clip holding intake air temperature sensor wiring to the fan shroud. 2 2011-2016 6.7L FORD INTERCOOLER PIPE UPGRADE (OEM REPL.) INTERCOOLER PIPE UPGRADE KIT STEP 2 6.7L FORD Remove the bolt holding the power steering reservoir to the fan shroud. Pull the power steering reservoir up to disconnect it from the fan shroud and just let the reservoir swing free to temporarily provide easier access to the lower intercooler pipe connection point (on intercooler). Loosen the lower factory t-bolt clamp (at intercooler). STEP 3 With a pick tool or something similar, carefully remove the metal locking clip from the factory plastic throttle body coupler. Be careful not to damage the ring as it will be re-used later. With everything disconnected, carefully remove the entire cold-side factory intercooler pipe assembly from the vehicle. HS-MOTORSPORTS.COM 3 STEP 4 Twist carefully (1/4 turn counter-clockwise) to unlock and remove the intake air temperature sensor from the factory plastic throttle body coupler. -
Engine Cooling Systems
Emergency Diesel Generator Engine Cooling Systems 6.0 ENGINE COOLING SYSTEMS If this heat is not removed, engine internal temperatures would soon reach a point of This chapter identifies the major component damage and engine failure. All components of the diesel engine cooling commercial diesel engines use some form systems and explains how each system is of cooling system to absorb this heat and necessary for reliable operation of the transfer it to a heat absorbing medium engine. outside of the engine. Learning Objectives Many modern engines are equipped with turbocharging systems to provide enough As a result of this lesson, you will be able to: air to allow the burning of the fuel required to produce the required power. The 1. State the purpose of a diesel engine turbocharging system adds heat to the jacket water cooling system. combustion air. In order to ensure that sufficient pounds of air are provided for the 2. Identify the major components of a combustion of the fuel, it is necessary to typical diesel engine jacket water cool the combustion air before it goes into cooling system and describe the the engine cylinders (to maintain the air operation of each. density). This is done by means of a radiator-like heat exchanger called the air 3. State the purpose and describe the intercooler, or aftercooler, and mounted in operation of the jacket water keepwarm the piping between the turbocharger and circulation system as is commonly compressor outlet and the engine air used on nuclear application diesel manifold. This radiator removes excess engines. heat from the combustion air. -
Aircraft Piston Engine Operation Principles and Theory
Lect-25 Aircraft Piston Engine Operation Principles and Theory 1 Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay Lect-25 How an IC engine operates-1 • Each piston is inside a cylinder, into which a gas is created -- heated inside the cylinder by ignition of a fuel air mixture at high pressure (internal combustion engine). • The hot, high pressure gases expand, pushing the piston to the bottom of the cylinder (BDC) creating Power stroke. 2 Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay Lect-25 How an IC engine operates-2 •The piston is returned to the cylinder top (Top Dead Centre) either by a flywheel or the power from other pistons connected to the same shaft. • In most types the "exhausted" gases are removed from the cylinder by this stroke. • This completes the four strokes of a 4-stroke engine also representing 4 legs of a cycle 3 Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay Lect-25 How an IC engine operates-3 • The linear motion of the piston is converted to a rotational motion via a connecting rod and a crankshaft. • A flywheel is used to ensure continued smooth rotation (i.e. when there is no power stroke). Multiple cylinder power strokes act as a flywheel. 4 Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay Lect-25 How an IC engine operates-4 •The more cylinders a reciprocating engine has, generally, the more vibration-free (smoothly) it can operate. •The aggregate power of a reciprocating engine is proportional to the volume of the combined pistons' displacement.