1 / 38

Lightweight Fuel Efficient Engine Package

Lightweight Fuel Efficient Engine Package . Brittany Borella , Chris Jones, John Scanlon, Stanley Fofano , Taylor Hattori, and Evan See. Project Overview. Customer Needs. Engineering Specifications. Engine Model. Air/Fuel Ratio: 0.86 Lambda

aurora
Download Presentation

Lightweight Fuel Efficient Engine Package

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Lightweight Fuel Efficient Engine Package Brittany Borella, Chris Jones, John Scanlon, Stanley Fofano, Taylor Hattori, and Evan See

  2. Project Overview

  3. Customer Needs

  4. Engineering Specifications

  5. Engine Model

  6. Air/Fuel Ratio: 0.86 Lambda • Simplified tubular geometry used for initial induction and exhaust models • CRF250R valve flow scaled until WR450F data is measured • Wiebe combustion model parameters currently estimated until cylinder pressure data is obtained • Ignore effects of muffler • Surface roughness values estimated • Wall heat transfer properties estimated for steel exhaust sections • Intake and exhaust valve lift estimated from YZ400F until actual measurements can be made • Assume constant operating temperature and component temperatures—to be correlated with dyno data • Assume ambient conditions of 14.7 psia and 80°F Overall Assumptions

  7. Finalized intake/throttle/restrictor geometry • Finalized injector placement(s) • Injector flow data • Intake/exhaust valve inflow and outflow loss coefficients • Intake/exhaust cam profiles • Base cam timing • General cranktrain dimensions • Surface area ratios for head and pistons • P-V Diagrams to validate Wiebe model assumptions • Various temperature measurements Required Parameters

  8. Theoretical Engine Model

  9. Live Simulation of Engine Parameters

  10. Dynamometer Test Stand

  11. Cylinder Head Removed for Measurement

  12. Flow Testing of Cylinder Head Bore Tube Production Photo Courtesy of DUT Racing

  13. System Test Plan

  14. Engine Characterization • Torque • P-V Diagrams • Brake Specific Fuel Consumption • Cooling System • Sensors • Cylinder Pressure • Crank angle • Thermocouples • Fuel Flow • Coolant Flow • Basic Engine Diagnostics • Wideband Lambda Engine Testing

  15. FT-210 Series • Gems Sensors & Control • 0.026 - 0.65 gal/min • ± 3% Accuracy Fuel Flow Sensor

  16. PCB Piezotronics • Transducer 112B10 • 422E In-Line Charge Converter Cylinder Pressure Sensor

  17. AM4096 - 12 bit rotary • Measure Angular Position • Outputs • Incremental • Series SSI • Linear Voltage • Analogue Sinusoidal Magnetic Encoder

  18. Load Simulation • Power Characterization • Fuel/Spark Mapping Dynamometer

  19. Dynamometer Controller • Data Input Improvement • NI PCI-6024E • 200 kS/s • 12-Bit • 16-Analog-Input DAQ Data Acquisition

  20. CFD Analysis

  21. 20 mm inlet diameter (19 mm for E85) creates choked flow conditions, limiting total mass airflow to engine • Required by competition rules • Keeps engine power at a safe level for competition • Design goal is to minimize loss coefficient through restrictor geometry to allow maximum airflow into engine • Supersonic Converging – Diverging Nozzle Geometry • Expand out diverging section to allow for proper shock development to minimize loss coefficient • Keep diffuser angle low enough to avoid potential flow separation • Keep overall length low to reduce viscous losses due to surface friction and boundary layer growth Intake Restrictor

  22. 2-Dimensional Axis-Symmetric analysis allows for fast solving time with refined mesh in areas of shock development Intake Restrictor

  23. Air flows from throttle to engine intake port through intake manifold • Intake Plenum • Acts as air reservoir for engine to draw air from during intake stroke • Primary purpose is to damp out pressure pulses from intake stroke to create steady flow conditions at the restrictor • Intake Runner • Path through which engine pulls air from the plenum into the combustion chamber during intake stroke • Length decided by harmonic frequency at various engine operating speeds, can be used to create a resonant “tuning point” Intake Manifold

  24. Transient Pressure Boundary Condition used to simulate pressure pulses within manifold from intake stroke • Piecewise-Linear Approximation used for initial analysis trouble-shooting • End analysis will use pressure trace measured during Dynamometer Testing Intake Manifold

  25. Component Simulation • Shroud structure analyzed to ensure uniform airflow distribution across radiator face and verify proper mass airflow through radiator • Radiator modeled as a material resistance with heat addition and flow re-direction to properly simulate airflow through core Cooling System Airflow

  26. Full Car Simulation to verify shroud is receiving adequate airflow • Simulation model still in progress, needs additional geometry and refinement Cooling System Airflow

  27. Cooling System

  28. Overflow Tank Surge Tank Cooling System Schematic Steam from Cylinder Head Thermostat Radiator Fan Engine Block Water Pump

  29. Modify for bleed line to Surge Tank • Rule of thumb: 1.1 in2 radiator surface area needed per hp produced • Therefore need approx. 66 in2 • Radiator from YFZ450R Yamaha ATV • 7.5” H x 11.5” W x 7/8” D • Surface Area 86.25 in2 • Inlet and Outlet ¾” ID tubing to connect to water pump Radiator Inlet from Engine Outlet to Water Pump

  30. Coolant naturally builds to approximately 16-18 psi • Normal production cars run 16-18 psi, high performance cars run 22-24 psi , and racing systems run 29-31 psi • Pressurizing the water allows for the water to reach a higher temperature before boiling (therefore vaporizing) • Part# T30R Radiator Cap 29-31 PSI Radiator Cap

  31. Typically a 1 quart container • Need to modify the part of the Radiator that currently has the cap and overflow line to run a ¼”- 3/8” bleed line from radiator to top of surge tank • ½” – ¾” Refill line from bottom of surge tank to inlet of water pump • Benefits – de-aeration • 2% air in the system leads to an 8% decrease in cooling efficiency • 4% air in the system leads to a 38% decrease in cooling efficiency! 30 PSI Pressurized Radiator Cap Bleed line inlet from radiator and cylinder head Surge Tank Outlet to overflow tank Refill line back to water pump

  32. Comes stock on engine • No internal bypass system. Thermostat will have to regulate continual water flow through engine • ¾” ID inlet and outlet tubing to connect to radiator Need to test flow rate once we have the cylinder head again Water Pump Flow Rate vs. RPM from R6 water pump

  33. Placed at the outlet of the engine, a thermostat allows water to circulate through the block, but doesn’t allow this water to circulate through the radiator until it has reached proper operating temperature • This temperature (195°F) melts the “wax motor”, which forces the thermostat piston to open and allows the water to flow through. • If the engine’s temperature is lowered too much, the piston closes until it has reached proper operating temperature once again Thermostat • Stewart/Robert Shaw Thermostats – 302 • Augments bypass system • $14.95

  34. Reviewed three sets of autocross runs with different drivers Cooling System Data

  35. Verify radiator is receiving adequate airflow at low speeds • SPAL Axial Fan • 11” Dia. • 755.0 CFM • Based on predicted power require minimum 450 CFM • Based on airflow at speed available require minimum 500 CFM • Maximum 7” Dia. to fit radiator • Yamaha R6 Fan • 5.5” Dia. • Est. >500 CFM Fan • Q = required heat rejected into air

  36. Risk Assessment

  37. Risk Assessment - Technical

  38. Risk Assessment - Management

More Related