78-1 AB Emissions and Fuel Economy Testing of a Naval Academy Heat Balanced Engine (NAHBE) April 1978 Technology Assessment and Evaluation Branch Emission Control Technology Division Office of Mobile Source Air Pollution Control Environmental Protection Agency ------- Background For several years personnel at the Naval Academy have been involved in research efforts directed toward improving the combustion cycle of spark ignition engines. They have developed a technique which is stated to be based on pressure exchange between two zones in the combustion chamber thereby achieving a heat balanced cycle (NAHBE) which combines the best characteristics of the Diesel and Otto cycles. The developers claim that their technique: increases engine efficiency; provides more complete fuel oxidation and therefore lowers HC and CO emissions; reduces peak cylinder pressures; reduces engine temperature; and reduces engine knock tendencies. The hardware utilized by the Naval Academy personnel in implementing this concept consists of a standard Otto cycle engine in which the head of the piston has been modified to establish two distinct combustion volumes and the intake system has been modified through enleanment of the carburetor and the addition of an air bleed with claimed stratification of the intake charge. In 1977 EPA was requested to test an engine modified to the NAHBE con- figuration. EPA was furnished two new, military, motor/generator sets (one NAHBE and one stock) for evaluation of the NAHBE concept. The required break-in of the new engines delayed the completion of testing until early 1978. The primary responsibility of the EPA Motor Vehicle Emission Lab is to test and evaluate vehicles. Therefore, there are only limited facilities and resources available to test a motor-generator set. A comprehensive evaluation of the NAHBE concept was, therefore, neither planned nor conducted. The testing conducted was, however, complete enough to characterize the fuel economy and emissions of the test engines under the operating conditions permitted by the motor-generator configuration. The conclusions drawn from this EPA evaluation test can be considered to be qualitatively and quantitatively valid only for the specific, motor- generator set used; however it is reasonable to extrapolate the results from the EPA test to other types of engine applications in a qualitative manner, i.e., to suggest that similar results are likely to be achieved on other types of engines using similar emission control technology for similar applications. Summary of Findings* 1. As delivered and operating on gasoline under steady state condi- tions, the NAHBE engine HC and CO emissions were substantially lower than the stock engine; NOx emissions were substantially higher than the stock engine and the thermal efficiency was signi- ficantly higher than the stock engine. *A11 HC, CO, and NOx comparisons are based on grams per kW hr. All thermal efficiency comparisons are based on kW hr per BTU of fuel. ------- 2. Operation of the stock engine with the induction system and car- buretor from the NAHBE engine resulted in changes in emissions and thermal efficiency which, within the constraints of experimental error, were identical to those observed with the NAHBE engine. 3. Operation of the NAHBE engine on alcohol caused an incease in HC emissions and a substantial reduction in NOx emissions relative to operation on gasoline. CO emissions and thermal efficiency were unchanged. 4. When operated on gasoline, the NAHBE engine, the stock engine, and the stock engine with the NAHBE induction system and carburetor performed satisfactorily with changes in load and under steady load conditions. Operation of the NAHBE engine on alcohol resulted in unsastifactory operation both under steady state and changing load conditions. When operated on alcohol, carburetor adjustments were required at each load change. 5. Exhaust gas temperatures of the NAHBE engine were, in general, significantly higher than those of the stock engine. 6. Test results from this program were compared to data from an EPA contractor test program on several commercial engines of similar size and type. This comparison showed that: a) HC emissions from the stock engine were, on average, higher than those from gasoline fueled commercial engines and much higher than those from diesel engines. b) HC emissions from the NAHBE engine were lower than those from gasoline fueled commercial gasoline engines and up to 200 times higher than those from the diesel engines. c) CO emissions from the stock engine were on average, twice as high as those from commercial gasoline engines and up to 200 times higher than those from diesel engines. d) CO emissions from the NAHBE engine were significantly lower than from the commercial gasoline engines while being up to five to ten times higher than those from diesel engines. e) NOx emissions from the stock engine were lower than those from the commercial gasoline engines and substantially lower than those from the diesel engines. ' f) NOx emissions from the NAHBE engine were higher than those from the diesel engines and significantly higher than those from the commercial gasoline engines. ------- g) The thermal efficiency of the stock engine was between 3% and 39% lower than the worst commercial gasoline engine, between 32% and 57% lower than the best commercial gasoline engine used in the comparison and between 46% and 71% lower than the diesel engines used in the comparison. h) The thermal efficiency of the NAHBE engine was between 14% higher and 16% lower than the worst commercial gasoline engine used in the comparison, between 20% and 41% lower than the best commercial gasoline engine and between 37% and 60% lower than the diesel engines used in the comparison. Conclusions'"' The stock engine used in the NAHBE engine project is not representative of similar commercial engines and is therefore not a good engine for comparative purposes because it provides misleadingly large improvements for the NAHBE concept. When compared to representative commercial engines, the NAHBE engine is at a significant disadvantage both with respect to thermal efficiency and NOx emissions, while appearing to offer some benefits in HC and CO emissions relative to gasoline engines through enleanment of the air/fuel mixture. The ability to sustain this apparent HC and CO benefit is questionable, however, because many engines of this type depend on charge cooling (operating fuel rich) as a method for attaining acceptable engine life. All of the emission and fuel consumption characteristics of the NAHBE engine can be reproduced on the stock engine through the substitution of the NAHBE induction system (modified intake manifold and a modified carburetor with a modified metering rod) for the stock components. It appears, therefore, that the modified piston which is used in the NAHBE concept and which is claimed to be its major feature, did not contribute significantly to the observed changes in performance of the test engine. Performance of the NAHBE engines on alcohol, as built, was unsatisfactory. It is not clear whether this poor performance is inherent with the NAHBE concept or whether it is the result of inadequate development of the test engine. The results of this test and evaluation project indicate that the NAHBE concept did not offer any benefits in either emissions or fuel economy when compared to similar gasoline and diesel engines. Test Engine Description The engines delivered for testing were 10 hp military motor generator sets designed to produce 5 kW of continuous power. The generator is *A11 HC, CO, and NOx comparisons are based on grams per kW hr. All thermal efficiency comparisons are based on kW hr per BTU of fuel. ------- directly attached to the engine crankshaft and operates at engine rpm. The units are self contained and designed to be operated at all ambient temperatures. They are skid mounted in a tubular frame. The engines and generators are manufactured to military specifications by several manufacturers. Therefore, although the two engines tested were manu- factured by Wisconsin and Hercules, they are identical in all respects and have complete parts interchangeability. A complete description of the motor-generator sets is given in Appendix A at the end of this report. The conversion of a stock engine to NAHBE configuration principally consists of changes to the piston (see Figures 1 & 2) and the fuel/air induction system by using modified metering rods and by introducing small air bleeds (see Figure 3). The piston is modified by the addition of a cap which separates the combustion chamber into two zones (a primary combustion zone and a balancing combustion zone). According to the developers, this design, coupled with the air bleed, stratifies the combustion fuel-air mixture by introducing additional air through the auxilary air inlet at the start of the intake stroke. During compression the leaner mixture is forced into the balancing chamber. This balancing chamber mixture is compressed during ignition and subsequently flows out to the main chamber during the later stages of combustion. The combustion process is thereby prolonged and allowed to achieve a greater degree of completion than the stock engine. However, the calibrated orifices of the auxilary air bleeds are very small (about 1/8" diameter) and therefore appear to introduce little air when compared to the one inch manifold tube. This air is introduced before the intake valve, thus there is no special means for assuring that this air enters the balancing chamber undiluted as claimed. The NAHBE is designed for multi-fuel capability. Because the BTU content per unit volume is higher for gasoline than for alcohol, operation of the ,NAHBE engine with gasoline requires lower volumetric fuel flow than with alcohol. The developers furnished metering rods designed to accomplish this. The developers indicated that the stock metering rod was'to be used with gasoline and that the modified metering rod was to be used with alcohol. Additional enleanment is also provided on the NAHBE by the carburetor to intake manifold air bleed. The fuel system components were not modified for sustained operation on alcohol. To prevent deterioration of fuel system components the engine must be switched over to gasoline prior to shutting down. Test Procedures Testing procedures for the engines in this project were adapted from the procedures used in the testing of heavy-duty engines by EPA for emis- sions certification and in the development of engine performance maps by engine manufacturers. Testing was performed at the governed (rated) speed of the engines and represents, therefore, modes 8 through 12 of the heavy-duty diesel procedure. These modes are 100, 75, 50, 25 and 0 percent of rated load at rated (governed) speed. ------- Standard Geometry Valves Valves (17° inclined) Spark Plug Hemispheric Head •Piston STOCK ENGINE NAHBE Changes in Basic Geometry Head Modification Balancing Chamber Geometry Solid Addition NAHBE ENGINE Figure 1 - NAHBE Changes in Basic Combustion Chamber Geometry ------- Chamber Cap Clearance to cylinder wall .075 in. Standard Piston \ NAHBE MODIFICATION Figure 2 Schematic of NAHBE Piston Modification ------- Calibrated Orifice Bleed Valve fr r i j 1 ! TJ r~~Z NAHBE Addition Stock induction Calibrated Orifice Figure 3 - Fuel Air Induction System speed of the engines and represents, therefore, modes 8 through 12 of the heavy-duty diesel procedure. These modes are 100, 75, 50, 25 and 0 percent of rated load at rated (governed) speed. Gaseous exhaust emission tests were run using the analytical equipment and sampling system specified in the 1977 Federal Test Procedure ('77 FTP) described in part 40 of the Combined Federal Register of July 1, 1976 for light-duty vehicles. All tests were steady state and followed the heavy-duty diesel test schedule. A thermocouple was installed in the muffler outlet to monitor exhaust gas temperature (EGT) as an aid in evaluating test results. ------- The engines/generators were loaded by using a resistive load bank to dissipate the engine/alternator power. Alternator voltage, current, and frequency were controlled and monitored for all testing. The voltage was held at 110V and the frequency at 60 cycles during engine break-in and during all testing. The engine exhaust was collected by the con- stant volume sampling (CVS) procedure which gives exhaust emissions of HC, CO, C0_ and NOx in grams per kW hr. Fuel economy was calculated by the carbon balance method. The fuels used were Indolene 30, a leaded 100 RON gasoline, and denatured ethyl alcohol (190 proof, 95% ethyl alcohol). All fuel consumption results for tests using alcohol are given as gallons of denatured alcohol. All tests were conducted at 3600 rpm (governed speed). Testing When delivered the engines were "green". The stock engine/alternator had 3.2 total hours and the NAHBE had 6.1 total hours. Apparently both had only been operated during manufacturing inspection check out and following modification to the NAHBE concept. Therefore, before testing, the engines were broken in by operating them to 50 hours total operating time. Break-in consisted of a repetitive cycle of running the engines for two hours at each load (50, 75, and 100 percent of full load). All break-in was done with Indolene 30 fuel. Exhaust emissions were periodically measured throughout the break-in to establish whether or not emission levels had stabilized prior to of- ficial testing. Also during break-in a few tests were performed to determine the potential effects of fuel/air mixture changes on the two engines. These break-in results are tabulated in Tables C-l and C-2 at the end of this report. After the engines had accumulated approximately 50 total hours the engines were tested for emissions and fuel consumption. Both engines were extensively baseline tested with their respective standard induction system. The baseline configuration for the NAHBE used the NAHBE induction system consisting of the modified intake manifold and a modified car- buretor with a modified metering rod. The baseline configuration of the stock engine used the stock induction system consisting of a stock intake manifold and a stock carburetor with a stock metering rod. The induction systems of both engines were changed from their baseline configuration to investigate the effects of changes in fuel/air ratio on the engines emissions and fuel consumption performance. The NAHBE was tested with the modified intake manifold, modified carburetor and the stock metering rod. The stock engine was tested with modified intake manifold, modified carburetor, and both the stock and modified metering rods. ------- According to the engine developers, the NAHBE induction system, as delivered, had a modified fuel metering rod installed which was cali- brated for the larger fuel flow required for alcohol. When tested with alcohol, the NAHBE surged badly apparently because of too lean a mixture. The engine developer who was witnessing the tests raised the float level and readjusted the idle mixture to stop the heavy surge. However, after running a few minutes, the engine again surged slightly. Also the engine required additional manual adjustment whenever the load was changed. Therefore, with the necessary warmup, stabilization, the high fuel consumption and the restart, only a few tests were possible with alcohol before the limited supply was used up. These engine test configurations are summarized below: Engine Intake Manifold Carburetor Metering Rod NAHBE Modified Modified Modified (both (Baseline gasoline and configuration) alcohol) NAHBE Modified Modified Stock (Configuration A) Stock Stock Stock Stock (baseline configuration) Stock Modified Modified Stock (Configuration A) Stock Modified Modified Modified (Configuration B) The results of the above tests are tabulated in Tables C-l and C-2 and are summarized in Tables B-l through B-5 as NAHBE and stock engines. Discussion of Results Included in Tables B-l through B-5 are the results of similar tests on other small utility and small heavy-duty engines. A description of these engines is included in Appendix A. These teslp^ were conducted by Southwest Research Institute under an EPA contractViy and are included here to establish a basis for comparison of the relative merits of the NAHBE concept and the stock engine used as a baseline in this project. (1) Exhaust Emissions from Uncontrolled Vehicles and Related Equipment Using Internal Combustion Engines. Part 4, Small air cooled spark ignition utility engines, and Part 5, Heavy-Duty Farm, Construction and Industrial Engines. APTD report numbers 1494 and 1495. ------- 10 Also Included in Tables Bl through B5 are the results for the NAHBE and stock engines restated to account for the generator losses. Based on discussions with the army engineering contracts office responsible for the procurement and production testing of these untis, a generator efficiency of 90% was selected as being most representative of the effi- ciency encountered during EPA testing. A comparison of the test results (using gasoline) shows little difference in thermal efficiency or HC, CO, or NOx emissions between the NAHBE with the stock metering rod (NAHBE configuration A) and the baseline stock engine. However, a comparison of the tests of the NAHBE with the stock metering rod and the modified metering rod (NAHBE baseline) show a marked difference. With the modified metering rod installed, the NAHBE's HC emissions were reduced by factors of 3 to 15; CO emissions were reduced by factors of 20 to 50; NOx emissions increased by factors of 1 to 5; and thermal efficiency increased by 10 to 20 percent. These results show that the modified metering rod reduces the quantity of fuel supplied to the engine rather than increasing it as planned by the designers. A review of the thermal efficiency and the HC, CO, and NOx emissions of the stock engine shows that it was designed to operate very fuel rich. The HC and CO emissions are the highest of the group of engines listed and, conversely, the thermal efficiency and NOx emissions are the lowest. Therefore, by enleanment alone, the stock engine should show improvements in HC, CO, and efficiency with a possible increase in NOx emissions. These improvements were observed in the test data. Since the preceding results indicated that a large part of any benefits of the NAHBE concept were due to enleanment, a series of tests was run on the stock engine using the NAHBE induction system (modified carburetor and modified intake tubes) and the two metering rods. When the stock engine (with the NAHBE induction system) was tested with the stock metering rod installed (stock configuration A), the HC, CO, NOx emissions and thermal efficiency were very similar to the baseline tests of the stock engine and the tests of the NAHBE with the stock metering rod . (NAHBE configuration A). The only major change was at 100% load where the CO emissions were halved and the NOx emissions doubled. Also, when the stock engine with the NAHBE induction system was tested with the modified metering rod (stock configuration B) the results were very similar to the NAHBE under the same conditions. Therefore from the viewpoint of emissions or thermal efficiency: 1) the benefits of the NAHBE concept, as tested, can be ascribed to fuel enleanment alone, 2) this enleanment can be readily accomplished by modifying the induction system on the stock engine through the use of a leaner metering rod and 3) the NAHBE pressure balance concept requiring piston modification showed no benefit in this series of tests. ------- 11 Due to the previously reported limited volume of alcohol, only a few tests of the NAHBE were run on alcohol. Compared to the NAHBE with the modified metering rod and running on gasoline, HC emissions were up by a factor of 2 to A, CO emissions were unchanged, NOx emissions were reduced by a factor of 7 to 10, and thermal efficiency ranged from unchanged to 10% worse. A comparison of the NAHBE (baseline configuration, using gasoline) test results with those of the other engines in Tables B-l through B-5 shows few if any benefits. In thermal efficiency the NAHBE at best only equals the poorest of the group. The developers hoped for efficiency of the heat balanced cycle is not evident. Its thermal efficiency is only half that of the diesel under all conditions and several of the gasoline engines better it by more than 30 percent most of the time. The diesels are consistently better than the NAHBE in HC and CO emissions. Although the NAHBE HC and CO emissions are better than some of the gasoline engines, these gasoline engine emisssions could also be reduced by enleanment. In NOx emissions the NAHBE is similar to a few and greater than many by a factor of two. Thus if the other gasoline engine HC and CO emissions were reduced by enleanment, many have a considerable NOx cushion before their NOx emissions would exceed the NAHBE emission levels. One question left unanswered by the test program is the potential effects on engine durability due to the reduction in charge cooling and increase in exhaust gas temperature (EGT) resulting from the NAHBE conversion. The stock engine was designed for use in a military motor/generator set. The induction system was designed specifically for this military application and was designed to run fuel rich. As shown by the test data in Tables C-l and C-2, enleanment raised the muffler EGT by 50° to 200°F. The effects of this on piston, valve component, cylinder head, and exhaust system life is unknown. Although both engines experienced similar exhaust gas temperature rises when leaned out, the effect on engine durability may not be identical for both engines. The developers presented only limited durability data on the NAHBE. Several problems were encountered during testing. On alcohol the NAHBE could not be properly adjusted to a low speed idle since it would surge or stall. At higher power settings the NAHBE surged moderately after a few minutes of steady state testing even after the developer had adjusted the carburetor. In addition it required additional adjustment whenever the load was changed. The NAHBE air injection tube broke during testing and had to be repaired. The modified metering rod was improperly fabricated so that it did not seat exactly in the center of the metering jet. ------- 12 Appendix A Heat Balanced Engine Test System Description 5 kW generator set, military standard DOD model MEP-017A with heat balanced engine Engine Nomenclature Manufacturer, Type Cooling Bore and Stroke Displacement Compression Ratio Rated HP Maximum HP Speed Range Governed Speed Ignition Fuel Metering Fuel Requirement Military standard model 2A042 III. Piston, combustion chamber, and induction system were modified by the Naval Academy Wisconsin (mfr. of stock engine) 4 stroke, Otto cycle, OHV, 2 cyl. opposed air cooled. Modified by Naval Academy to heat balanced engine concept. Air cooled 76.2 x 76.2 mm/3.00 x 3.00 in. 695 cc/42.4 cu. in. 8.5 to 1 (modified piston and cylinder head) 7.5 kW/10 hp at 3600 rpm (stock engine rating) 13.0 kW/17.5 hp at 3600 RPM (stock engine rating) None. Controlled at 3600 RPM 3600 RPM Magneto Stock single, side draft, 1 venturi carburetor with air bleed Regular leaded 91 octane automotive or ethyl alcohol. Tested with Indolene 30, RON 100; and also with ethyl alcohol ------- 13 Generator Manufacturer Output Power Output Voltage Frequency Power Factor General Frame Size Weight Mounting Total System Operating Time Appendix A Heat Balanced Engine (Continued) Fermont 5 kW AC 120/240 V single phase, 120/208 V three phase 60 hertz 0.8 Tubular frame, skid mounted 101.0 cm long x 76.2 cm wide x 63.5 cm high; 39 3/4 in long x 30 in wide x 25 in high 217.3 kg/479 pounds Engine directly coupled to generator. 5 hours when received ------- 14 5 kW Generator Set, Engine Nomenclature Manufacturer Type Cooling Bore and Stroke . Displacement . •• Compression Ratio Rated hp Maximum hp Speed Range Governed Speed Ignition Fuel Metering Fuel Requirement Appendix A Stock Test System Description Military Standard, DOD Model MEP-017A Military standard model 2A042-II1 Hercules (Identical to engine manu- factured by Wisconsin) 4 stroke, Otto cycle, OHV, 2 cyl. opposed Air cooled 76.2 x 76.2 mm/3.00 x 3.00 in. 695 cc/42.4 cu. in. 6.9:1 7.5 kW/10 hp at 3600 RPM 13.0 kW/17.5 hp at 3600 RPM 3000 to 4000 RPM 3600 RPM Magneto Single, side draft, 1 venturi carburetor Regular leaded, 91 octane automotive gasoline (tested with Indolene 30, RON 100) ------- 15 Generator Manufacturer Output Power Output Voltage Frequency Power Factor Appendix A Stock Engine (continued) Fermont 5 kW AC 120/240 V single phase; 120/208 V three phase 60 hertz 0.8 General Frame Size Weight Total System Operating Time Tubular frame, skid mounted 101.0 cm long x 76.2 cm wide x 63.5 cm high; 39 3/4in. long x 30 in. wide x 25 in. high 217.3 kg/479 pounds 3 hours when received ------- Appendix A (continued) Specification of Comparison Engines Manufacturer Model Cylinders Bore & Stroke in. 3 Displacement, in Compression Ratio Rated HP @ RPM Rated Torque (fr Ibf) @ RPM Cooling Ignition Fuel Metering Fuel Type Aspiration Comb. Chamber Briggs & Stratton 92908 1 2.56 x 1.75 9.02 6.20:1 3.5 @ 3600 5.2 @ 3100 Air mag. 1 V gasoline Briggs & Stratton 100202 1 2.50 x 2.13 10.43 6.20:1 4 @ 3600 5.9 @ 3100 Air mag. 1 V gasoline Wisconsin SD 12 1 3.50 x 3.00 28.86 6.35:1 12.5 @ 3600 21.5 @ 2200 Air Batt & mag. 1 V gasoline Kohler K482 opposed-2 3.25 x 2.88 48.0 6.00:1 18 @ 3600 31.7 @ 2400 Air Batt & mag. 1 V gasoline Mercedes Benz OM636 1-4 2.94 x 3.94 108 19.0:1 29 @ 2400 60 @ 2000 Water CI FI diesel natural Onan DJBA 1-2 3.25 x 3.63 60 19.0:1 14.6 @ 2400 36 @ 1800 Air CI FI diesel natural Wisconsin VH4D V-4 3.25 x 3.25 108 5.50:1 30 @ 2800 M 66 @ 1700 Air Batt 1 V gasoline pre-cup pre-cup ------- 17 Table B-l HC Emissions gm/kW hr % full load @ rated RPM 0* 25 50 75 100 ENGINE W/GENERATOR NAHBE w/modified MR 13.5 7.2 4.3 2.6 3.9 NAHBE (alcohol) - - - 11.9 5.7 NAHBE w/standard MR 189.4 67.3 30.3 16.3 9.8 Stock 55.8 57.0 31.3 20.4 13.3 Stock w/NAHBE induction & modified MR - - 4.4 2.0 1.8 Stock w/NAHBE induction & Standard MR 260.2 90.8 29.3 15.5 9.2 ENGINE NAHBE w/modified MR 13.5 6.5 3.9 2.3 3.5 NAHBE (alcohol) - - - 10.9 5.1 NAHBE w/standard MR 189.4 60.6 27.3 14.7 8.8 Stock 55.8 51.3 28.2 18.4 12.0 Stock w/NAHBE induc- tion & modified MR - - 4.0 1.8 1.6 Stock w/NAHBE induc- tion & Standard MR 260.2 81.7 26.4 14.0 8.3 B&S 92908 17.7 49.1 31.4 29.8 14.5 B&S 100202 4.18 ' 8.43 6.85 6.05 5.03 Wisconsin SD12 73.3 33.6 23.6 20.5 17.0 Kohler K 482** 120 40.0 22.4 22.2 21.1 Mercedes-Benz OM 636 20.7 5,29 1.93 -78 .36 Onan DJBA 20.2 5.29 2.08 .99 1.18 Wisconsin VH4D 120 24.56 13.07 8.34 8.11 MR - Metering rod * - grams/hr ** - Emissions from the test engine may be higher than typical due to the carburetor setting ------- 18 Table B-2 CO Emissions gm/kW. hr % full load @ rated RPM 0* 25 50 75 100 ENGINE W/GENERATOR NAHBE w/modif ied MR NAHBE (Alcohol) NAHBE w/ standard MR Stock Stock w/NAHBE induc- tion & modified MR Stock w/NAHBE induc- tion & standard MR ENGINE NAHBE w/modified MR NAHBE (Alcohol) NAHBE w/standard MR Stock Stock w/NAHBE induc- tion & modified MR Stock w/NAHBE induc- tion & standard MR B&S 92908 B&S 100202 : Wisconsin SD12 Kohler K482** Mercedes-Benz OM 636 Onan DJBA Wisconsin VH4D 50 - 2813 2175 - 2582 50 - 2813 2175 - 2582 134 20.6 ' 1540 1970 69.9 70.3 2636 33 - 2151 2172 - 2269 30 - 1936 1955 - 2042 619 38.0 838 424 7.30 13.69 680.5 19 - 996 1041 33 1008 17 — 896 937 30 907 440 53.4 729 419 4.81 4.77 429.5 20 19 489 687 18 406 18 17 440 618 16 365 510 80.3 670 356 3.06 2.43 318.1 18 12 394 428 14 201 16 11 355 385 13 181 199 48. 636 723 11. 3. 233. 9 83 37 6 MR * ** Metering rod grams/hr Emissions from the test engine may be lower than typical due to the carburetor setting ------- 19 Table B-3 NOx Emissions gm/kW hr 0* % full load @ rated RPM 25 50 75 100 ENGINE W/ GENERATOR NAHBE w/modified MR NAHBE (Alcohol) NAHBE w/ stock MR Stock Stock w/NAHBE induc- tion & modified MR Stock w/NAHBE induc- tion & standard MR ENGINE NAHBE w/modified MR NAHBE (Alcohol) NAHBE w/ stock MR Stock Stock w/NAHBE induc- tion & modified MR Stock w/NAHBE induc- tion & standard MR B&S 92908 B&S 100202 Wisconsin SD12 Kohler K482** Mercedes-Benz OM 636 ONAN DJBA Wisconsin VH4D 7.11 2.03 3.0 5.28 7.11 2.03 3.0 5.28 4.30 3.14 3.21 5.44 19.0 15.1 6.83 14.45 2.91 3.24 4.26 13.01 2.62 2.92 3.83 6.40 14.63 2.91 3.68 5.91 13.83 3.69 14.46 2.81 2.50 18.92 3.97 13.01 2.53 2.25 17.03 3.57 4.71 18.0 2.38 5.23 5.10 9.44 6.05 7.33 1.04 6.00 3.20 9.75 5.92 6.60 .94 5.40 2.88 8.78 5.33 2.66 19.2 1.66 3.87 4.39 6.66 10.26 16.76 1.63 7.84 6.35 15.29 16.00 15.08 1.47 7.06 5.72 13.76 14.4 5.42 24.3 2.21 3.74 2.97 4.70 11.60 MR - Metering rod * - grams/hr ** - Emissions from the test engine may be lower than typical due to carburetor setting ------- 20 Table B-4 Fuel Economy kW hr/gal % full load @ rated RPM 0* 25 50 75 100 ENGINE W/GENERATOR NAHBE w/modified MR NAHBE.(alcohol)** NAHBE w/stock MR Stock Stock w/NAHBE induc- tion & modified MR Stock w/NAHBE induc- tion & standard MR ENGINE NAHBE w/modified MR NAHBE (Alcohol)** NAHBE w/stock MR Stock Stock w/NAHBE induc- tion & modified MR Stock w/NAHBE induc- tion & standard MR B&S 92908 B&S 100202 Wisconsin SD 12 Kohler K482*** Mercedes-Benz OM 636 Onan DJBA Wisconsin VH4D 1.6 1.2 1.4 - 1.1 1.6 1.2 1.4 - 1.1 6.3 7.0 1.6 1.1 1.7 3.2 .8 1.9 1.5 1.4 - 1.4 1.7 1.4 1.3 - 1.3 2.6 3.6 2.5 2.7 5.9 5.2 3.5 3.4 2.7 2.7 3.4 2.7 3.1 2.4 2.4 3.1 2.4 4.3 5.1 3.4 4.3 8.5 7.9 5.1 4.4 2.4 3.9 3.5 4.4 3.8 4.0 2.2 3.5 3.2 4.0 3.4 5.2 6.2 4.3 4.8 9.8 9.6 6.2 5.1 3.1 4.5 4.3 5.2 4.9 4.6 2.8 4.1 3.9 4.7 4.4 7.8 7.0 4.9 5.2 10.0 8.8 7.1 MR - * ** *** _ Metering rod , hr/gal. alcohol, gal are gal alcohol (190 proof, 95% ethyl alcohol) Fuel economy from the test engine may be lower than typical due to the carburetor setting ------- 21 Table B-5 Thermal Efficiency % ENGINE W/ GENERATOR NAHBE w/modified MR NAHBE (alcohol) NAHBE w/ stock MR Stock Stock w/NAHBE induction & modified MR Stock w/NAHBE induction & modified MR ENGINE NAHBE w/modified MR NAHBE (Alcohol) NAHBE w/stock MR Stock Stock w/NAHBE induction & modified MR Stock w/NAHBE induction & modified MR B&S 92908 B&S 100202 Wisconsin SD12 Kohler K 482* Mercedes-Benz OM 636 Onan DJBA Wisconsin VH4D % of 25 5.2 4.0 3.8 3.7 5.8 4.4 4.2 4.1 7.1 9.8 6.9 7.2 14.4 12.8 9.4 full load 50 9.3 7.2 7.4 9.3 7.3 10.3 8.0 8.2 10.3 8.1 11.6 14.0 9.4 11.7 20.9 19.4 14.0 @ actual 75 12.0 10.9 10.5 9.6 11.9 10.4 13.3 12.1 11.7 10.7 13.2 11.6 14.2 16.9 11.9 13.2 24.2 23.5 16.9 RPM 100 13.9 14.1 12.3 11.8 14.1 13.4 15.4 15.7 13.7 13.1 15.7 14.9 21.4 19.0 13.5 14.1 24.4 21.6 19.3 MR - Metering rod * - Thermal efficiency from the test engine may be lower than typical due to the carburetor setting ------- 0% Load 78-6459 78-6632 78-6808 79-0048 25% Load 50% Load Table C-l Heat Balanced Engine/Generator Test No. Comment (1) (1) Eng ine Hours 21.0 51.8 58.4 60.7 Power kW EGT* °F gm/kW hr HC CO CO 78-6456 78-6461 78-6468 78-6475 78-6815 78-6810 (3) (3) 13.3 20.1 41.0 51.2 57.9 59.8 2.3 2.2 2.2 2.5 2.5 2.4 805 795 640 635 (1) (2) '(3) (4) (5) * Gm/hr, hr/gal Manifold air bleed closed Standard (stock) metering rod Carburetor air bleed blocked off Alcohol, gal are gal alcohol Exhaust gas temperature NOx Fuel Economy kW hr/gal 78-6460 78-6467 78-6631 78-6809 78-6811 (3) (3) 20.2 41.2 51.8 58.2 59.9 1.1 1.2 1.3 1.3 1.3 800 790 590 590 6.6 5.9 7.2 74.9 59.7 28 28 33 2344 1958 5128 4932 4717 2542 2652 12.02 14.26 14.45 2.61 3.20 1.7 1.8 1.9 1.4 1.5 17 23 19 19 1079 913 3043 2817 2915 2554 1611 1777 10.72 11.70 15.34 14.46 2.39 3.23 2.9 3.1 3.0 3.4 2.6 2.7 Thermal Efficiency % 4.4 4.4 3.0 3.3 4.6 4.9 5.2 3.8 4.1 7.9 8.5 8.2 9.3 7.1 7.4 NJ ------- Test No. 75% Load Table C-l (can't) Heat Balanced Engine/Generator Power EGT* gm/kW hr kW °F HC CO CO- Fuel Economy NOx kW hr/gal 78-6457 78-6462 78-6464 78-6471 78-6469 78-6474 78-6630 78-6816 78-6813 78-6807 (2) (2) (2) (5) (3) (3) 13.6 19.5 19.8 39.7 40.9 50.9 51.6 56.0 57.7 59.8 3.5 3.5 3.5 3.6 3.8 3.7 3.8 3.8 3.8 3.8 685 825 815 730 958 705 710 3.4 1.8 9.1 15.9 4.6 2.6 15.2 11.9 18.1 14.4 11 14 467 486 17 20 392 19 564 413 2240 1885 1481 1480 1980 1956 1613 2132 1428 1539 9.64 12.65 4.22 4.47 17.86 7.33 7.80 1.04 5.08 6.92 3.9 4.6 4.0 3.9 4.4 4.4 3.9 2.4 3.7 4.0 100% Load 78-6458 13.8 4.5 78-6463 19.1 4.6 78-6465 (2) 19.3 4.6 78-6472 (2) 39.4 4.8 78-6470 39.9 4.9 78-6473 50.7 5.0 78-6629 (2) 51.4 5.0 78-6791 (2), (4) 52.7 5.0 78-6633 (4) 52.8 5.0 78-6812 (5) 55.2 5.0 78-6817 (5) 55.7 5.0 78-6814 (3) 57.5 5.0 78-6806 (3) 58.9 5.0 78-0049 61.2 5.0 (1) Gra/hr, hr/gal (2) Manifold air bleed closed (3) Standard (stock) metering rod (4) Carburetor air bleed blocked off (5) Alcohol, gal are gal alcohol (190 * Exhaust gas temperature 765 920 895 830 760 840 930 940 780 775 845 proof, 1.9 2.2 5.9 9.5 2.7 3.9 8.7 13.4 6.7 5.6 5.8 12.7 13.6 5.9 95% 7 9 233 203 13 18 134 384 89 12 12 381 406 36 ethyl 1867 1766 1371 1393 1730 1696 1577 1281 1588 1670 1689 1318 1310 1602 alcohol) 12.60 9.06 8.48 9.95 12.93 16.76 17.55 7.10 17.55 1.66 1.60 7.84 7.83 19.52 4.7 5.0 5.0 5.1 5.0 5.1 4.9 4.6 3.1 3.1 5.1 4.5 4.5 5.3 Thermal Efficiency % 10.6 12.6 10.9 10.6 12.0 12.0 10.6 10.9 10.1 10.9 12.8 13.7 13.7 13.9 13.7 13.9 13.4 12.6 13.9 14.2 13.9 12.3 12.3 14.5 to U) ------- Table C-2 Stock Engine/Generator Test No. 0% Load 78-6483 78-6488 78-6624 78-6819 78-6819 25% Load 78-6484 78-6489 78-6625 78-6820 78-6926 50% Load 78-6482 78-6482 78-6485 78-6490 78-6502 78-6542 78-6821 78-6822 78-6922 78-6923 78-6927 Comment (1) (1) (1) (D,(3)* (D,(3)* (3)* (3)* (2)* A * (3)* (3)* Engine Hours 18.9 40.9 53.4 57.7 59.7 19.1 40.7 53.1 57.9 59.9 9.9 10.5 19.3 40.2 48.4 52.5 55.1 56.0 56.8 58.0 56.9 Power kW 1.22 1.21 1.28 1.2 1.3 2.4 2.4 2.2 2.5 2.5 2.5 2.5 2.5 2.5 2.5 2.5 EGT ** °F 555 540 620 635 630 610 645 640 690 680 680 730 845 840 695 700 HC 24.3 35.0 55.8 249.8 270.6 34.4 51.3 57.0 90.9 90.7 21.0 21.0 22.7 29.4 30.1 32.5 13.3 4.0 4.8 28.2 30.4 gm/kW CO 1109 1090 2175 2480 2684 1811 1771 2172 2208 2330 1405 1407 1180 987 1009 1073 326 28 38 980 1035 hr CO 2 3581 3375 2781 3211 3033 3149 2961 2630 2703 2681 1753 1727 1865 1644 1541 1618 2034 2560 2556 1686 1693 NOx 4.83 4.95 3.00 6.34 4.22 3.81 4.13 3.24 4.57 3.95 2.32 2.18 2.66 2.58 2.45 2.54 11.76 19.23 18.60 3.98 3.96 Fuel Econom; kW hr/gal 1.6 1.7 1.4 1.1 1.1 1.5 1.5 1.4 1.4 1.3 2.2 2.2 2.3 2.7 2.8 2.6 3.4 3.4 3.4 2.7 2.6 Thermal Efficiency % (1) (2) (3) A A* Gm/hr, hr/gal Manifold air bleed closed Standard (stock) metering rod Modified Carburetor and modified intake tubes Exhaust gas temperature 4.1 4.1 3.8 3.8 3.5 6.0 6.0 6.3 7.4 7.6 7.1 9.3 9.3 9.3 7.4 7.1 N3 ------- Test No. 75% Load 78-6481 78-6481 78-6486 78-6491 78-6501 78-6503 78-6917 78-6918 78-6921 78-6924 78-6929 100% Load 78-6480 78-6480 78-6487 78-6499 78-6500 78-6626 78-6627 78-6629 78-6919 78-6820 78-6818 78-6925 78-6929 Comment (2)* * * (3)* (3)* (2)* * * (3)* (3)* Engine Hours .1 ,2 9.5 10.3 21.6 39.9 48. 52. 54.9 55.8 56.6 58.8 60.3 9.3 10. 21, 39. 47.9 52.0 53.9 54. 54. 55.6 56.4 59.1 60.5 ,1 .4 ,7 .1 ,7 Table C-2 (con't) Stock Engine/Generator Power EGT ** kW °F 3.5 3.5 3.4 3.8 3.7 3.7 3.8 3.8 3.8 3.8 3.8 4.5 4.5 4.8 5.0 4.6 5.0 755 750 750 805 935 930 965 780 805 810 830 940 920 900 945 945 855 875 (1) Qtt'/hr, hr/gal (2) Manifold air bleed closed (3) Standard (stock) metering rod * Modified Carburetor and modified intake tubes ** Exhaust gas temperature gm/kW hr Fuel Economy HC 13.8 15.4 19.0 23.1 20.1 20.7 8.4 2.0 2.0 15.2 15.8 10.5 12.1 12.8 16.5 14.0 12.5 1.6 2.2 3.6 1.5 1.6 9.0 9.3 cp_ 1022 1109 865 784 687 687 158 18 18 498 314 798 818 615 560 461 395 14 16 31 13 13 202 199 CO 2 1435 1388 1636 1315 1362 1362 1691 2052 1971 1484 937 1296 1319 1169 1180 1377 1304 1722 1692 1533 1670 1640 1444 1502 NOx 2.30 2.00 3.65 2.40 3.22 3.17 13.96 9.86 9.64 7.15 4.69 2.69 2.63 2.62 3.07 6.15 6.54 15.19 21.68 17.44 12.19 12.08 15.09 16.90 kW hr/gal 2.9 2.8 2.9 3.4 3.5 3.5 4.5 4.3 4.4 3.8 3.8 3.5 3.4 4.1 4.2 4.1 4.5 5.1 5.1 5.6 5.2 5.3 5.0 4.8 Thermal Efficiency % 7.9 7.6 7.9 9.3 9.6 9.6 12.3 11.7 12.0 10.4 10.4 9.6 9.3 11.2 11.5 11.2 12.3 13.9 13.9 15.3 14.2 14. 13. 13.1 ------- |