DIAGNOSTIC TECHNIQUES FOR A SURGE VALVE OF A TURBOCHARGED ENGINE
20190323445 ยท 2019-10-24
Inventors
- Scott E. Henson (Chelsea, MI, US)
- Amarjeet Singh Sahota (Ann Arbor, MI, US)
- Dhaval D. Shah (Rochester Hills, MI, US)
Cpc classification
F02D41/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2041/1432
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/602
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/703
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02D23/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/101
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/2403
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
G01L23/24
PHYSICS
International classification
F02D41/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G07C5/08
PHYSICS
Abstract
Diagnostic systems and methods for a surge valve that selectively bypasses a compressor of a turbocharger of an engine involve receiving, by a controller, a barometric pressure signal indicative of a barometric pressure external to the engine, receiving, by the controller, a throttle inlet pressure (TIP) signal indicative of an air pressure at an inlet of a throttle valve of the engine and downstream from the surge valve and the compressor, and performing, by the controller, a diagnostic technique on the surge valve, the diagnostic technique comprising generating a pressure ratio signal that is a ratio of the TIP signal to the barometric pressure signal, applying a high-pass filter to the pressure ratio signal to obtain a filtered pressure ratio signal, and based on a quantity of detected pulses in the filtered pressure ratio signal that exceed the diagnostic threshold, detecting a malfunction of the surge valve.
Claims
1. A diagnostic system for a surge valve that selectively bypasses a compressor of a turbocharger of an engine, the system comprising: a barometric pressure sensor configured to generate a barometric pressure signal indicative of a barometric pressure external to the engine; a throttle inlet pressure (TIP) sensor disposed downstream from the surge valve and the compressor and being configured to output a TIP signal indicative of an air pressure at an inlet of a throttle valve of the engine; and a controller configured to perform a diagnostic technique on the surge valve, the diagnostic technique comprising: generating a pressure ratio signal that is a ratio of the TIP signal to the barometric pressure signal; applying a high-pass filter to the pressure ratio signal to obtain a filtered pressure ratio signal; detecting any pulses in the filtered pressure ratio signal that exceed a diagnostic threshold; and based on a quantity of detected pulses exceeding the diagnostic threshold, detecting a malfunction of the surge valve.
2. The system of claim 1, wherein the controller is configured to detect a set of preconditions for performing the diagnostic technique.
3. The system of claim 2, wherein the set of preconditions comprises (i) a current request to open the surge valve, (ii) a recent tip-in to tip-out transition of an accelerator device of the engine, and (iii) the throttle valve being closed.
4. The system of claim 3, wherein the set of preconditions further comprises engine speed and requested turbocharger boost being within predetermined ranges.
5. The system of claim 3, wherein a count corresponding to the quantity of detected pulses resets to zero when the surge valve is no longer requested to open.
6. The system of claim 1, wherein the malfunction indicates that the surge valve is stuck closed.
7. The system of claim 6, wherein the controller is further configured to activate a malfunction indicator lamp (MIL) indicating a need to replace the surge valve.
8. The system of claim 1, wherein the diagnostic technique is non-intrusive in that the controller does not temporarily alter operation of the engine as part of the diagnostic technique.
9. A diagnostic method for a surge valve that selectively bypasses a compressor of a turbocharger of an engine, the method comprising: receiving, by a controller and from a barometric pressure sensor, a barometric pressure signal indicative of a barometric pressure external to the engine; receiving, by the controller and from a throttle inlet pressure (TIP) sensor disposed downstream from the surge valve and the compressor, a TIP signal indicative of an air pressure at an inlet of a throttle valve of the engine; and performing, by the controller, a diagnostic technique on the surge valve, the diagnostic technique comprising: generating a pressure ratio signal that is a ratio of the TIP signal to the barometric pressure signal; applying a high-pass filter to the pressure ratio signal to obtain a filtered pressure ratio signal; detecting any pulses in the filtered pressure ratio signal that exceed a diagnostic threshold; and based on a quantity of detected pulses exceeding the diagnostic threshold, detecting a malfunction of the surge valve.
10. The method of claim 9, further comprising detecting, by the controller, a set of preconditions for performing the diagnostic technique.
11. The method of claim 10, wherein the set of preconditions comprises (i) a current request to open the surge valve, (ii) a recent tip-in to tip-out transition of an accelerator device of the engine, and (iii) the throttle valve being closed.
12. The method of claim 11, wherein the set of preconditions further comprises engine speed and requested turbocharger boost being within predetermined ranges.
13. The method of claim 11, wherein a count corresponding to the quantity of detected pulses resets to zero when the surge valve is no longer requested to open.
14. The method of claim 9, wherein the malfunction indicates that the surge valve is stuck closed.
15. The method of claim 14, further comprising activating, by the controller, a malfunction indicator lamp (MIL) indicating a need to replace the surge valve.
16. The method of claim 9, wherein the diagnostic technique is non-intrusive in that the controller does not temporarily alter operation of the engine as part of the diagnostic technique.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0010]
[0011]
[0012]
DETAILED DESCRIPTION
[0013] As discussed above, conventional surge valve diagnostics are intrusive. For example, a conventional surge valve diagnostic technique could temporarily adjust operation of the engine, such as commanding the surge valve to open when unnecessary. These techniques decrease engine performance (fuel economy, responsiveness, etc.). Accordingly, improved diagnostic techniques for a surge valve of a turbocharged engine are presented. These techniques are non-intrusive in that a controller does not temporarily alter operation of the engine as part of the diagnostic routine. These techniques monitor a pressure ratio signal that is a ratio of a throttle inlet pressure (TIP) signal to a barometric pressure signal and, after high-pass filtering the pressure ratio signal, detect pulsations in the filtered pressure ratio signal that exceed a threshold. When a count or quantity of the detected pulsations during a period while the surge valve is requested to open exceeds a threshold, a malfunction of the surge valve is detected (e.g., a stuck closed surge valve).
[0014] Referring now to
[0015] The air in the intake manifold 108 is distributed to a plurality of cylinders (not shown) and combined with fuel (e.g., gasoline) to create an air/fuel mixture that is combusted to generate drive torque. Exhaust gas resulting from combustion is expelled into an exhaust manifold 144 and through an exhaust system 148. The exhaust system 148 includes an exhaust passage 152 through which the exhaust gas flows. The energy of the exhaust gas powers a turbine 156 of the turbocharger 128, which in turn drives the compressor 124 via a shaft 160 of the turbocharger 128. A wastegate valve 164 is configured to selectively bypass the turbine 156 to control exhaust gas pressure or boost. It will be appreciated that, while not shown, the exhaust system 148 could include other components such as a catalytic converter and/or an exhaust gas recirculation (EGR) system.
[0016] A controller 172 controls operation of the vehicle 100, such as controlling air and fuel supplied to the engine 104 such that the engine 104 generates enough drive torque to meet a driver torque request. The driver provides the torque request via an accelerator device (ACCEL) 176, such as an accelerator pedal. The control by the controller 172 includes, for example, controlling the throttle valve 120, the surge valve 132, and the wastegate valve 164. A barometric pressure sensor 180 is configured to generate a barometric pressure signal indicative of a barometric pressure external to the engine 104 or the vehicle 100. In one exemplary implementation, the barometric pressure sensor 180 is integrated within the controller 172, but it will be appreciated that the barometric pressure sensor 180 could be a standalone sensor.
[0017] Referring now to
[0018] At 224, the controller 172 detects any pulses/pulsations in the filtered pressure ratio signal that exceed a diagnostic threshold (TH.sub.D). This diagnostic threshold is a calibratable threshold and could vary across different vehicle applications.
[0019] It will be appreciated that the term controller as used herein refers to any suitable control device or set of multiple control devices that is/are configured to perform at least a portion of the techniques of the present disclosure. Non-limiting examples include an application-specific integrated circuit (ASIC), one or more processors and a non-transitory memory having instructions stored thereon that, when executed by the one or more processors, cause the controller to perform a set of operations corresponding to at least a portion of the techniques of the present disclosure. The one or more processors could be either a single processor or two or more processors operating in a parallel or distributed architecture.
[0020] It should be understood that the mixing and matching of features, elements, methodologies and/or functions between various examples may be expressly contemplated herein so that one skilled in the art would appreciate from the present teachings that features, elements and/or functions of one example may be incorporated into another example as appropriate, unless described otherwise above.