0434398 NOZZLE WELL JOHNSON
BJ20SREUM, BJ25BAEUA, BJ30BAEUD, HJ20CREDA, HJ25RLEDA, HJ30REDE, J20CREIE, J20CREND, J20CREOR, J20CRERC, J20CRETS, J20EEIE, J20EEND, J20EEOR, J20EERC, J20EETS, J25EEID, J25EENS, J25EEOA, J25EERR, J25EETC, J25REIE, J25REND, J25REOR, J25RERC, J25RETS,
NOZZLE
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Rating:
Compatible models:
BJ20SREUM
BJ25BAEUA
BJ30BAEUD
HJ20CREDA
HJ25RLEDA
HJ30REDE
J20CREIE
J20CREND
J20CREOR
J20CRERC
J20CRETS
J20EEIE
J20EEND
J20EEOR
J20EERC
J20EETS
J25EEID
J25EENS
J25EEOA
J25EERR
J25EETC
J25REIE
J25REND
J25REOR
J25RERC
J25RETS
J30EEIC
J30EENR
J30EEOB
J30EERM
J30EETA
J30REIC
J30RENR
J30REOB
J30RERM
J30RETA
J35REIC
J35RENR
J35RERM
J35RETA
SJ35REDE
JOHNSON
BRP JOHNSON entire parts catalog list:
- CARBURETOR - 20CR » 0434398
BJ30BAEUD, BJ30BALEUD, J30REUD, J30RLEUD 1997
HJ20CREDA, HJ20CRLEDA, J20CREDA, J20CRLEDA 1996
HJ25RLEDA, J25REDA, J25RLEDA, SJ25REDA, SJ25RLEDA 1996
HJ30REDE, HJ30RLEDE, J30REDE, J30RLEDE, SJ30REDE, SJ30RLEDE 1996
J20CREIE, J20CRLEIE, TJ20CRLEIE 1991
J20CREND, J20CRLEND, TJ20CREND, TJ20CRLEND 1992
J20CREOR, J20CRLEOR 1995
J20CRERC, J20CRLERC 1994
J20CRETS, J20CRLETS, TJ20CRETS, TJ20CRLETS 1993
J20EEIE, J20ELEIE 1991
J20EEND, J20ELEND 1992
J20EEOR, J20ELEOR 1995
J20EERC, J20ELERC 1994
J20EETS, J20ELETS 1993
J25EEID, J25ELEID, TJ25ELEID, VJ25ELEID 1991
J25EENS, J25ELENS, TJ25ELENS, VJ25ELENS 1992
J25EEOA, J25ELEOA 1995
J25EERR, J25ELERR 1994
J25EETC, J25ELETC, TJ25ELETC, VJ25ELETC 1993
J25REIE, J25RLEIE, VJ25REIE 1991
J25REND, J25RLEND 1992
J25REOR, J25RLEOR 1995
J25RERC, J25RLERC 1994
J25RETS, J25RLETS 1993
J30EEIC, J30ELEIC, VJ30EEIC, VJ30ELEIC 1991
J30EENR, J30ELENR, VJ30EENR, VJ30ELENR 1992
J30EEOB, J30ELEOB 1995
J30EERM, J30ELERM 1994
J30EETA, J30ELETA, VJ30EETA, VJ30ELETA 1993
J30REIC, J30RLEIC 1991
J30RENR, J30RLENR 1992
J30REOB, J30RLEOB 1995
J30RERM, J30RLERM 1994
J30RETA, J30RLETA 1993
J35REIC, J35RLEIC 1991
J35RENR, J35RLENR 1992
J35RERM, J35RLERM 1994
J35RETA, J35RLETA 1993
SJ35REDE, SJ35RLEDE 1996
Information:
ORRule of Thumb for tank size with 25% reserve
0.056 × Ave. BHP demand × Hours between refills × 1.25 = _____ gal.0.27 × Ave. BKW demand × Hours between refills × 1.25 = _____ liters Additional tank capacity required for cooling of recirculated fuel in unit injected engines. Tank should be located below level of injectors or nozzles.Piping
Fuel Supply Line Maximum Restriction*: 3600 ... -38.8 kPa (11.6 in Hg)(Vacuum)3400, 3500 ... -30 kPa (9 in. Hg) (Vacuum)3300 ... -20 kPa (6 in. Hg) (Vacuum)3208 ... -27 kPa (8 in. Hg) (Vacuum)Fuel Return Line Maximum Restriction:* 3600 ... 350 kPa (51 psi)3300 ... 20 kPa (3 psi)3208, 3400, 3500 ... 27 kPa (4 psi)*Locate day tank and design piping to meet these requirements.Fuel Properties
Blended (Heavy) fuels are usually described by their viscosity, expressed either in "centistokes" (cSt) or "Seconds Redwood". The Redwood scale at 100°F is being phased out and replaced by the centistokes scale at 50°C. The centistoke viscosity may be preceded by the letters IF for "intermediate fuel" or IBF for "intermediate bunker fuel". For example, IF 180 fuel has a viscosity of 180 cSt at 50°C. The following table gives the approximate relationship between the two scales. Fuel Properties
Density and Specific Gravity
Fuel API Correction Chart - API Gravity Corrected to 60°F
Tooling: Fuel Thermo-hydrometer 1P7408Test Breaker 1P7438Distillate Fuel Temperature
Maximum Fuel Supply Temperature:- Without Power Reduction: 85°F (29°C)Power is reduced 1% for each 10°F (5.6°C) above 100°F (38°C) if engine is running against fuel stop.- Without Injector Damage: 150°F (65°C)Performance Analysis Rules of Thumb
Correction Factors: Power Calculation:
BSFC Tolerances
Performance curves represent typical values obtained under normal operating conditions. Ambient air conditions and fuel used will affect these values. Each of the values may vary in accordance with the following tolerances:Exhaust Stack Temperature 42 DEG C 75 DEG FIntake Manifold Pressure-Gage 10 kPa 3 in HgPower 3 PercentFuel Consumption 6 g/kW-hr .010 lb/hp-hrFuel Rate 5 PercentConditions
Ratings are based on SAE J1349 standard conditions of 100 kPa (29.61 in Hg) and 25°C (77°F). These ratings also apply at ISO 3046/1, DIN 6271 and BS 5514 standard conditions of 100 kPa (29.61 in Hg), 27°C (81°F) and 60% relative humidity.Fuel Rates are based on fuel oil of 35° API [16°C (60°F)] gravity having an LHV of 42 780 kJ/kg (18,390 Btu/lb) when used at 29°C (85°F) and weighing 838.9 g/liter (7.001 lbs/U.S. gal).Additional Formulas Used to Develop Marine Par Curves
For Torque Check GPH proceed as follows:Torque Check GPH = TQ COR. Fuel Rate (G/MIN) ÷ 454 × 60 = LBS/HRLBS/HR ÷ 7.076 = GPHFor BSFC proceed as follows:BSFC = Adjusted CSFC (G/kW HR) ÷ 454 = LBS/kW HRLBS/kW HR ÷ 1.34 = BSFC (LBS/HP HR)Recommended "Guide Line" Gas Supply Pressures for Caterpillar Gas Engines - All Values in PSIG (kPag) Natural Gas
Gas Regulator Capacity Chart
Fuel Gas Methane Numbers
Physical Constants of Gases:
Air-Fuel Ratio Adjustment for Initial Start-up:
Fuel Consumption Calculation
Published fuel consumption values are for 905 BTU/FT3 LHV. To calculate fuel consumption for other fuel gas, the following equation can be used: Special Lube Oil Information for Gas Engines:
Condemning limits
Alternate Oil Analysis (additional test procedures for more data) -1Differential infrared analysis of used oil must not exceed the following absorbance/CM:
Scheduled Oil Sampling If analysis of the used oil at the recommended oil change interval exceeds the condemning limits, the following courses of action can be taken:1. Modify the jacket water temperature and/or adjust the air-to-fuel to minimize the oil degradation rate.2. Shorten the oil change interval.3. Work with your oil supplier to arrive at an oil that will not exceed the limits.Maximum PPM (Parts Per Million) of Wear Metals Detected at 750 Hours to Achieve Projected Overhaul Interval
Oil Failure
Causes and Avoidance
Symptoms of oil failure are stuck piston rings, heavy piston deposits, sludged oil, plugged oil filters, rapid ring and liner wear, and high copper concentrations in oil analysis.It is important that oil analysis measure oxidation and nitration since they result in corrosive wear and accelerate oil degradation. Oxidation and nitration cause oil to thicken and form lacquer and maroon-colored deposits.The nitration rate of an oil is associated with the air-to-fuel ratio for the engine. There is evidence that suggests operating the engine with an air-to-fuel ratio between 10:1 and 11:1 promotes rapid nitration of the oil. This is the normal air-to-fuel ratio range for most Caterpillar Natural Gas Engines and permits the optimum fuel consumption at rated power. In this range, nitrous oxide (NOx) as measured in the exhaust stream is at its highest level. This range may cause the oil to degrade at an unacceptable rate.If nitration is determined to be the principal reason for oil degradation, it may be necessary to adjust the air-to-fuel ratio either higher or lower to minimize the nitration rate.If the air-to-fuel ratio is changed, it must be done with care because it may have a negative effect on the power of the engine or result in excessive exhaust temperature which could affect the service life of the engine.Engine Data
0.056 × Ave. BHP demand × Hours between refills × 1.25 = _____ gal.0.27 × Ave. BKW demand × Hours between refills × 1.25 = _____ liters Additional tank capacity required for cooling of recirculated fuel in unit injected engines. Tank should be located below level of injectors or nozzles.Piping
Fuel Supply Line Maximum Restriction*: 3600 ... -38.8 kPa (11.6 in Hg)(Vacuum)3400, 3500 ... -30 kPa (9 in. Hg) (Vacuum)3300 ... -20 kPa (6 in. Hg) (Vacuum)3208 ... -27 kPa (8 in. Hg) (Vacuum)Fuel Return Line Maximum Restriction:* 3600 ... 350 kPa (51 psi)3300 ... 20 kPa (3 psi)3208, 3400, 3500 ... 27 kPa (4 psi)*Locate day tank and design piping to meet these requirements.Fuel Properties
Blended (Heavy) fuels are usually described by their viscosity, expressed either in "centistokes" (cSt) or "Seconds Redwood". The Redwood scale at 100°F is being phased out and replaced by the centistokes scale at 50°C. The centistoke viscosity may be preceded by the letters IF for "intermediate fuel" or IBF for "intermediate bunker fuel". For example, IF 180 fuel has a viscosity of 180 cSt at 50°C. The following table gives the approximate relationship between the two scales. Fuel Properties
Density and Specific Gravity
Fuel API Correction Chart - API Gravity Corrected to 60°F
Tooling: Fuel Thermo-hydrometer 1P7408Test Breaker 1P7438Distillate Fuel Temperature
Maximum Fuel Supply Temperature:- Without Power Reduction: 85°F (29°C)Power is reduced 1% for each 10°F (5.6°C) above 100°F (38°C) if engine is running against fuel stop.- Without Injector Damage: 150°F (65°C)Performance Analysis Rules of Thumb
Correction Factors: Power Calculation:
BSFC Tolerances
Performance curves represent typical values obtained under normal operating conditions. Ambient air conditions and fuel used will affect these values. Each of the values may vary in accordance with the following tolerances:Exhaust Stack Temperature 42 DEG C 75 DEG FIntake Manifold Pressure-Gage 10 kPa 3 in HgPower 3 PercentFuel Consumption 6 g/kW-hr .010 lb/hp-hrFuel Rate 5 PercentConditions
Ratings are based on SAE J1349 standard conditions of 100 kPa (29.61 in Hg) and 25°C (77°F). These ratings also apply at ISO 3046/1, DIN 6271 and BS 5514 standard conditions of 100 kPa (29.61 in Hg), 27°C (81°F) and 60% relative humidity.Fuel Rates are based on fuel oil of 35° API [16°C (60°F)] gravity having an LHV of 42 780 kJ/kg (18,390 Btu/lb) when used at 29°C (85°F) and weighing 838.9 g/liter (7.001 lbs/U.S. gal).Additional Formulas Used to Develop Marine Par Curves
For Torque Check GPH proceed as follows:Torque Check GPH = TQ COR. Fuel Rate (G/MIN) ÷ 454 × 60 = LBS/HRLBS/HR ÷ 7.076 = GPHFor BSFC proceed as follows:BSFC = Adjusted CSFC (G/kW HR) ÷ 454 = LBS/kW HRLBS/kW HR ÷ 1.34 = BSFC (LBS/HP HR)Recommended "Guide Line" Gas Supply Pressures for Caterpillar Gas Engines - All Values in PSIG (kPag) Natural Gas
Gas Regulator Capacity Chart
Fuel Gas Methane Numbers
Physical Constants of Gases:
Air-Fuel Ratio Adjustment for Initial Start-up:
Fuel Consumption Calculation
Published fuel consumption values are for 905 BTU/FT3 LHV. To calculate fuel consumption for other fuel gas, the following equation can be used: Special Lube Oil Information for Gas Engines:
Condemning limits
Alternate Oil Analysis (additional test procedures for more data) -1Differential infrared analysis of used oil must not exceed the following absorbance/CM:
Scheduled Oil Sampling If analysis of the used oil at the recommended oil change interval exceeds the condemning limits, the following courses of action can be taken:1. Modify the jacket water temperature and/or adjust the air-to-fuel to minimize the oil degradation rate.2. Shorten the oil change interval.3. Work with your oil supplier to arrive at an oil that will not exceed the limits.Maximum PPM (Parts Per Million) of Wear Metals Detected at 750 Hours to Achieve Projected Overhaul Interval
Oil Failure
Causes and Avoidance
Symptoms of oil failure are stuck piston rings, heavy piston deposits, sludged oil, plugged oil filters, rapid ring and liner wear, and high copper concentrations in oil analysis.It is important that oil analysis measure oxidation and nitration since they result in corrosive wear and accelerate oil degradation. Oxidation and nitration cause oil to thicken and form lacquer and maroon-colored deposits.The nitration rate of an oil is associated with the air-to-fuel ratio for the engine. There is evidence that suggests operating the engine with an air-to-fuel ratio between 10:1 and 11:1 promotes rapid nitration of the oil. This is the normal air-to-fuel ratio range for most Caterpillar Natural Gas Engines and permits the optimum fuel consumption at rated power. In this range, nitrous oxide (NOx) as measured in the exhaust stream is at its highest level. This range may cause the oil to degrade at an unacceptable rate.If nitration is determined to be the principal reason for oil degradation, it may be necessary to adjust the air-to-fuel ratio either higher or lower to minimize the nitration rate.If the air-to-fuel ratio is changed, it must be done with care because it may have a negative effect on the power of the engine or result in excessive exhaust temperature which could affect the service life of the engine.Engine Data