The amount of intake air flow must be inputted to ECM in order to determine the fuel injection quantity. To measure the pressure inside of intake manifold, MAFS is used at idle and MAPS is required at accelerating. MAPS(Manifold Absolute Pressure) calculates the amount of air indirectly as measuring the pressure inside of intake manifold. This system is called a Speed-Density type.
MAPS transfers analog output signal which is proportional to the change of intake manifold pressure, then, with this signal and RPM, ECM calculates the amount of intake air flow.
The MAPS is mounted on surge tank to measure the pressure inside of intake manifold, and it consists of a piezo electric element and hybrid IC which amplifies output signal from the element. A piezo electric element is a sort of a diaphragm using piezo electric effect. One side of the diaphragm is surrounded with vacuum chamber while intake pressure is applied to the other side. Thus, signals are output by the transformation of diagphragm according to the change of pressure inside of intake manifold.
ECM compares the difference between MAPS output and calculated MAPS value while enable condition is met.
If the acutal MAP value or lower than calculated(threshold) value for 2 min failure during tip in-out driving, ECM determines that a fault exists and a DTC is stored.
MIL(Malfunction Indicatin Lamp) turns on when the malfunction lasts till cosecutive 2 driving cycle.
Item | Detecting Condition | Possible Cause | |
DTC Strategy |
•
The MAP reading is compared to expected MAP high and low limits based on engine speed & Throttle Position | 1. Faulty TPS 2. Faulty MAPS | |
Enable Conditions |
•
Engine Coolant Temperature ≥ 60℃ (Fully Warmed up state)
•
600rpm < Engine Speed < 3000rpm | ||
Threshold value | Case 1 |
–
Power Test
•
Altitude compensated MAP < Calculated min. MAP data
•
Altitude compensated MAP > Calculated max. MAP data | |
Case 2 |
–
Decelleration Test
•
Altitude compensated MAP < Calculated MAP data | ||
Diagnosis Time |
•
Continuous (within 5min.) | ||
MIL On Condition |
•
NO MIL ON(DTC only) | ||
Pressure(kPa) | Voltage(V) |
20 | 0.79 |
46.66 | 1.84 |
101.32 | 4.0 |
Fig.1) Normal waveform of MAPS & TPS with acceleration.
Fig.2) Normal data of MAPS at idle.
It is necessary that MAPS should be checked along with TPS. Because the MAP/TPS rationality diagnostic is comprised of two tests. A deceleration test is performed to provide a robust method for detection of an altitude compensated MAP value that is too high for the deceleration condition. The second test compares the altitude compensated MAP value to both high and low limits, dependent upon throttle position and engine speed. When the MAP value is out of the threshold range, the MAP/TPS system is determined to be failed.
