DesignofaTestBenchforMicroCombustionEngines - ULisboa

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Design of a Test Bench for Micro Combustion EnginesHugo Cristiano Pereira da Silva o Superior Técnico, Lisboa, PortugalJune 2016AbstractThis study is about the design, construction and instrumentation of a test bench for testing microcombustion engines used in model vehicles. Several sensors and actuators were used to obtain itsperformance specifications. There is no standard test bench for micro engines, so this equipment intendsto present drivers with viable information, something that is missing. Several technical requirementswere considered for the test bench to be safe, effective and practical to use. Some of the componentswere manufactured while others were off-the-shelf and, at a final stage of the construction, the testbench was assembled with all the required model parts. One of the objectives is to characterise a 3.5cc micro engine. For that, the test bench was designed to obtain the power and torque diagrams andthe fuel consumption rate. These results are displayed on a PC through a data acquisition board ableto conduct all the necessary readings and processing for characterisation.First a conceptual design was made to assess the idea behind the project. After a thorough researchon test benches and micro engines, the concept gave way to the actual design of an inertia dynamometer.A program in LabView was developed for the data acquisition system including the actual control ofthe actuators. Components were produced in Instituto Superior Tecnico and, finally, the test bench wasassembled with the required flywheel and all the necessary electronic components. Tests were made foran electric motor driving a gyroscope to validate the instrumentation and then the 3.5 cc glow plugengine was tested, whose results of the power curves validated the whole design of the test bench.The inertia dynamometer is viable and flexible, able to test any kind of micro engine from 2.0 to20.0 cc. The program running the acceleration tests is fully automatic, allowing the test bench to havegood repeatability which is essential to get realistic data.Keywords: Power curves, inertia dynamometer, micro engines, performance, data acquisition.1. IntroductionThere is a growing need to characterise micro engines. At this point, there is no standard test benchfor testing them. The manufacturers fail to providerealistic performance specifications and the objective of this thesis is to develop an equipment capableof doing it for any kind of micro engine.1.1. Micro EnginesMicro engines are internal combustion engines [1]that go up to 20.0 cc of displacement and are largelyused in radio-controlled model vehicles (Figure 1),mostly for racing purposes. There are three typesof micro engines: spark ignition, diesel and the glowplug, which offers the highest power to weight ratioand is the primary choice for most of the modelracing car drivers.These engines can go up to 45 000 rpm [2], sothey have a very well-defined flow pattern withinthe combustion chamber characterised by a loopscavenging in the two-stroke engines. The admission of fuel and air is accomplished by a variable-(a) Model racing car with (b) Starting the Glow Plug enassembled micro engine.gine of a model airplane.Figure 1: Applications of micro engines.venturi carburetor with a slide that is actuated byan electric servo responsible for throttle control.1.2. Test BenchesThere are two main types of engine test benchesfor power assessment, commonly known as ”dynos”(from dynamometer): the inertia dynamometer andthe steady-state dynamometer. The inertia dynamometer works by having the engine accelerate1

an inertial mass (often called flywheel) during a certain amount of time until the torque evolution isfully collected [3]. Steady-state dynamometers usea brake (also named absorber or retarder) to applya load to the engine and hold it at a constant speedagainst the open throttle, where an electronic ”loadcell” reads the torque transmitted to the brakes [4].To characterise micro engines, it will be used anengine inertia dynamometer. It conducts an acceleration test more similar to the real world, whilecheaper and simpler (no need for large braking systems). The flywheel simulates the inertia experienced by the engine [5]. The torque is given byT [N.m] I[Kg.m2 ] α[rad/s2 ] ,The technical requirements covered in this sectionare summarized in Table 1.DescriptionEngine displacement vol.Maximum powerMaximum torqueSafety factorEngine max rot. speedEngine idle rot. speedEngine max temperatureRun acceleration timeFlywheel diameterFlywheel massDrive shaft rot. speed(1)where I is the moment of inertia of the flywheel andshaft all together and α is its angular acceleration.The main goal is to obtain the power (P) diagram, which is proportional to torque (T) and rotation speed (ω) of the drive shaft. By measuringboth, power is calculated asP [W ] T [N.m] ω[rad/s] .ParameterDPmaxTmaxnNmaxNidleTmax tdf lywheelmf lywheelNdriveshaf tValue2.0 - 20.0 cc2.5 kW0.750 Nm1.540 000 rpm10 000 rpm130 C10 s 300 mm 10 Kg 10 000 rpmTable 1: Technical requirements for the engine dynamometer.2.3. Auxiliary Systems RequiredA braking system has to be implemented in the testbench to stop the flywheel after a run. It shouldalso stop it fast enough to save time between runs,allowing the dynamometer to be more efficient.The temperature at the engine cylinder headshould not exceed 130C, according to some driversreports. As such, the engine needs to have a coolingsystem. The micro engines are cooled by air, so afan cooler needs to be considered.A device to actuate the throttle must also be implemented, to control the engine load.Micro engines are started by a 12V electric motorconnected to its crankshaft allowing it to rotate andstart burning fuel [2]. A device must be set to makethe coupling on the crankshaft wheel and allow theelectric motor to kick back at the moment the engine starts. At the same time, the glow plug mustbe heated by a 1.5V glow starter. This requireselectric power for both the electric motor and theglow starter.(2)2. BackgroundBefore beginning the design of the inertia dynamometer, technical requirements must be definedaccordingly to the objectives for this test bench.2.1. Engine SpecificationsThe type of micro engine to be tested for this dissertation is the glow plug of a car. According to theO.S. Engines manufacturer [6], the 4.5cc for truggies is one of the most powerful engines and yetlargely used, having a maximum crankshaft poweroutput of 3.26 HP (2.43 kW) at 32 000 RPM, resulting the estimation of maximum torqueP 60 0.725N.m(3)2 π NA safety factor of 1.5 will be used to ensure thatthe test bench withstands the test of any kind ofmicro engine from 2.0 to 20.0 cc.Tengine 2.4. Drive Shaft and Components ConfigurationThe drive shaft for the test bench, comprising thereduction gear and the flywheel, will be a solid steelshaft to prevent deflection, keeping the diameter assmall as possible [7]. Three ball-bearings supportswill secure it, two of them set close to the flywheelto minimize deflection. To attach the flywheel, anhub will be used with a cubic shape. A screw is usedto lock it on the shaft in a section where a grooveis set to receive the screw, preventing it to slide.The flywheel will be a balanced disc with aninner-disc and a thicker outer-ring. This way it willbe lighter for a given radius (R) than it would be ifdesigned as a regular disc. The moment of inertiafor a flywheel this shape is given by2.2. Technical RequirementsThe drive shaft must have a given amount of inertia for the engine to complete a run in, approximately, 10 seconds (recommended value for Inertiadynamometers) [3].For practical reasons, the flywheel should not exceed 300mm of diameter and 10Kg of mass. It mustbe perfectly balanced to ensure maximum stabilityat the highest RPMs.For safety and balancing reasons, the rotationalspeed of the drive shaft must not exceed 10 000rpm. A reduction gear needs to be implemented,given the engine maximum RPM greatly exceedsthis value.2

I 11mdisc R1 2 mring (R1 2 R2 2 )22(4)being R1 the radius of the inner-disc, and R2 theouter radius of the flywheel.The reduction is accomplished by a spur gear thatreduces the speed of the drive shaft according to agear ratio given byφ2ω1 ,(5)ω2φ1where ω1 and φ1 are the engine crankshaft rotationspeed and diameter, and ω2 and φ2 are the driveshaft rotation speed and diameter.To prevent engine overheating, a one-way bearing is used. This way, the flywheel overruns theengine crankshaft after a run, when the throttle isclosed for deceleration, preventing engine brakingthat could damage it [8].i Figure 3: Layout of the test bench.and relatively low cost. It has a yield strength of390 MPa and a tensile strength of 470 MPa [7].The flywheel will be made of steel. Other materials with lower densities would cause it to be muchbigger to reach the required inertia. The frameto help support the ground components of the testbench will be a stainless steel sheet mounted on awooden table. The supports for the drive shaft andthe gear itself are made of a hard and light composite, implemented from XRay model vehicles [9].2.5. Auxiliary Systems ConfigurationThe braking system is similar to the one used inmodel cars. A small disc is attached to the driveshaft with two pads right next to it. One pad isstatic, the other one is actuated by a rotating pin,located by the shaft support, which will cause thepad to press the disc and, eventually, stop it withinthe two parallel pads. In Figure 2 is possible to seesuch system.3.1. Drive ShaftTo size the drive shaft, it is important to know themaximum torque applied to it. Remembering themaximum of N 10 000 rpm for the drive shaft, andthat the maximum rotation speed of micro enginesis N 45 000 rpm, the minimum gear ratio (i ) givenby Equation (5) is45000 4.50 .10000To prevent the drive shaft to reach its maximumspeed, it is being used a more conservative gear ratioof i 5. Therefore, the applied torque on the driveshaft is given byimin Ttransmitted Tengine i 3.75N m .Figure 2: Braking system.(6)The AISI 1020 CD steel has a yield strength ofσy 390M P a. Considering the safety factor n 1.5, the maximum stress σmax is given byTo give the required degree of freedom for positioning the engine in the test bench, it has to comprise adjustable supports.For throttle and brake control, the electric servoused in model cars will be applied, which directlycontrols the position of both the throttle and thebrake pads by actuating the mechanical arm connected to the carburetor and the rotating pin onthe other end, respectively.In Figure 3 is possible to see a previous layout ofthe test bench.σy 260M P a(7)nThe torque transmitted from the engine causes atorsional moment on the drive shaft and, due to theflywheel weight, it will also experience a bendingmoment. The shaft will have an effective length ofL 220mm. It needs to be this long to ensure theflywheel does not interfere with other components,namely a 180 muffler or the starter below the mainframe.Conducting an equilibrium analysis, it is possibleto draw the load diagrams and assess the maximumσmax 3. Design, Assembly and Wiring LayoutThe material chosen for the drive shaft was the colddrawn AISI 1020 for its good mechanical properties3

where dmin is the minimum diameter, σy is the yieldstrength, M is the maximum Moment, T is the maximum Torque. As such, a shaft with 6mm of diameter satisfies the criterion.After a thorough research regarding these modelvehicles, a solution for the drive shaft and the attachment of its components is found. The driveshaft must have 8mm of diameter to comply withthe components found for the braking system. It isa AISI 1020 steel provided by Poly Lanema.As such, the shaft diameter exceeds the previously suggested 6mm. The safety factor should bemuch higher than the original value of 1.5,torque and moment suffered by the shaft. FromSection 3.2 in this chapter, it is known that theflywheel will have a mass of 9.81 Kg, which corresponds to a Weight of W 96.1 N, consideringg 9.8 m/s2 . The shaft is supported by simple ballbearings (points A, C and D) restraining it only inthe y direction. The flywheel is set at just 40mmfrom supports C and D. This way it causes a lowbending moment.The weight of the gear is being neglected becausethis is made of a light composite. Besides that, thebending moment is minimal because it is set rightnext to support D. The free-body diagram can beseen in Figure 4 a).π σyn d3 32qM2 5.234(9)T2In Figure 5 it is possible to see the solution forthe drive shaft of the test bench.(a) Free-body diagram.(b) Shear, bending and torsional moments.Figure 4: Load diagrams.Using the equilibrium equations for the appliedloads to acknowledge RA and RC , it is possible tocalculate the shear forces (V), torque (T) and bending moment (M) to draw its load diagrams,XMC 0 RA Figure 5: Drive shaft and its components.3.2. Flywheel SpecificationsTo calculate the required inertia of the flywheel, theangular acceleration (α) must be estimated from ω0to ωf .0.04 96.1 RA 48.05N0.08ωf ω0 α tXFy 0 RC 96.1N RA RC 48.05N(10)From the technical requirements, it is knownthat the common micro engine goes up to 40The load diagrams for the drive shaft can be 000 rpm and that the idle speed is, usually, 10seen in Figure 4 b). Torque is constant between 000 RPM. Considering the gear ratio, i 5, ω0 2000 RP M 209.44 rad/s, ωf 40000 the gear and the flywheel and equal to 3.75 Nm 1000055and the maximum bending moment is given by 8000 RP M 837.76 rad/s.Considering t 10 s from the technical reM RA 0.04 Mmax 1.9N m.quirements, results an average angular acceleration2There is no thrust load and since the shaft com- of α 62.83 rad/s .Lplies to the long shaft criteria ( d 10), shear forcesConsequently, the desired moment of inertia of(V) are negligible.theflywheel is given by Equation 1,Considering both T and M in the most solicitedsection of the shaft (B), the minimum diameter forTstatic analysis, according to Von Mises theory [7], 0.0597 Kg.m2I αis given byThe flywheel can have up to 300 mm of diameterand the mass must not exceed 10 Kg. It will be sizedrdown until a fair equilibrium of mass and radius1332 nσy M 2 T 2 ) 3 5.3mm (8) is found. From Equation (4), an iterative processdmin (π44

is made to assess the required dimensions of theR3 r 34outer ring to ensure the maximum of 10 Kg for the,(14)T Fµ 23R r2flywheel. The results are shown in Table 2. Thedensity of the steel is 7850Kg/m3 , accordingly to Resulting for the ideal forcethe supplier Ramada Acos.3TR2 r 2F 3 408N .(15)4µR r3Thickness eo45 mmR180 mmThis force of 408 N would be capable to stop theflywheel immediately, which will not be the case. AR2105 mmsmaller force does the work by stopping it in a fewseconds, while the generated friction in the brakeTable 2: Dimensions for the outer ring of the fly- pads is absorbing the kinetic energy dissipated bywheel.heat through the disc.The electric servo for throttle and break controlThe mass of the outer ring is given bygenerates up to 13.6 Kg.cm of torque (T). Thisquantity is transmitted to the brake pads by a small22(11) arm connected to the rotating pin that actuates themring ρ eo π (R2 R1 ) 5.12 Kgbrake (Figure 6 b)).and mdisc 4.71 Kg. So the total mass of theflywheel with a radius of 105 mm is equal to 9.83Kg.3.3. Braking SystemIt will be used a disc brake similar to the systemused in model vehicles. Knowing the brake padsactuate at uniform pressure p pa , and simplifying the contact area to Ac π4 (R2 r2 ) for anequivalent annular pad of 90, the braking force [7]is given by(a) Dimension of the braking pads.Figure 6: Braking system.π (R2 r2 )(12)4where pa is the applied pressure by the pads, Rthe outer radius 15mm, and r the inner radius 7mm.F p Ac pa Knowing 1 Kg.cm 0.098 N.m, the torque generated by the servo is equal to 1.33 Nm (T1 ). Theservo arm has a radius (R) of 20mm, so the respective force is given byIn Figure 6 a) is possible to see the dimensions ofthe pads used for the braking system and its equivalent annular pad actuating the disc.The contact area for each pad is Ac π4 (R2 r2 ) 138.23 mm2 . The larger it is, the lower isthe pressure for the required force. Integrating theproduct of the friction force and the radius, theTorque is found byπT µpa 2ZRr2 dr r(b) Braking force.1.33T1 66.64N .(16)R0.02The force F1 actuates the pin arm (R 10mm)transmitting a torque (T2 ) to the rotating pin givenbyF1 T2 F1 0.01 0.6664N m .(17)The rotating pin actuates the braking pads at a45 angle with F2 0.66640.006 111.1N . The torqueT2 causes a moment in the 6mm ledge of the pinthat actuates the brake pad. Projecting F2 to anormal force experienced by the ledge, it is possibleto obtain the braking force,πµpa (R3 r3 ) (13)6πµpa (R3 r3 )6where µ is the friction coefficient. Considering bothmaterials (ferodo and steel), µ 0.4 at 150 C.Since there will be used two pads on either sideof the disc, equation (13) is multiplied by two (thenumber of pairs of mating surfaces).For T 3.75 Nm, pa 2.95M P a 29.5bar.The equation can be written to relate torque withthe braking force,T F2 157.1N(18)cos(45)This is 38.5% of the ideal 408 N. It is sufficientto stop it in a few seconds, so it is viable to usethe braking system of model vehicles on the testbench. Note that the braking must be continuousto prevent an abrupt stopping of the flywheel, whichcould cause the test stand to flip over.Fbrake 5

3.4. Engine SupportIn Figure 9 it is possible to see the deflection exThe engine support blocks will be set on the table perienced by the drive shaft. Note that graphicalthrough two parallel slots. The design takes into representation has a magnifying factor of 200 foraccount the technical requirements for the engine visualization purposes.dimensions. In Figure 7 it is possible to see the solution for locating the support blocks to lock theengine with a 10mm freedom on both x and y directions, in case different gear meshes are used orlarger engines are tested.Figure 9: Displacement on the drive shaft.The maximum displacement occurs, naturally, inthe flywheel section. This value is equal to 0.008mm, as it can be seen in Figure 9.3.7. Structural AssemblyThe flywheel was manufactured in Instituto Superior Tecnico using both turning and milling.The first components to assemble on the driveshaft are the supports, locked on the test stand, thebraking system and the one-way bearing securingthe gear. In Figure 10 a) it is possible to see theassembled braking system.Figure 7: Engine support.3.5. Starting SystemFor setting the starter, a pedal is designed to accomplish the contact between the electric motor (Figure 8 a)) and the engine crankshaft. It is set belowthe test stand, secured by an hinge locked on thewooden table. The operator actuates it by pullingan handle set on the opposite side of the micro engine.To heat the glow plug, it will be used a portable”glow starter” set at 1.5V, as shown in Figure 8 b).(a) Braking system.(b) Flywheel assembled.Figure 10: Drive shaft completed.Next, the flywheel is assembled (Figure 10 b)).After it is in position, the hub must be locked en(a)Electricmotor(b) Glow starter.suring the flywheel does not slip.(starter).The engine support is assembled on the respectiveslots cut on the main frame. Its two supportFigure 8: Starting system.blocks are locked by four M4 bolts (Figure 11 a))and the engine is now locked in position as well. Themuffler is secured by a wire, previously set on the3.6. Deflection AnalysisThe shaft is designed to withstand the weight of main frame very close to the flywheel but withoutthe flywheel with a conservative safety factor, so interference.The electric servo for throttle and brake controlthe displac

for testing them. The manufacturers fail to provide realistic performance specifications and the objec-tive of this thesis is to develop an equipment capable of doing it for any kind of micro engine. 1.1. Micro Engines Micro engines are internal combustion engines [1] that go up to 20.0 cc of displacement and are largely

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