After only a few weeks and 3,000 miles my Bombed HX40 blew up.
It was a HX40 Center Section and Wheels with machined 12cm housings. The Turbo work was done at a reputable and established Turbo shop.
It performed exactly as I was told. Lower EGT's, Less Smoke, More Boost and still be Fast Spooling up. I was very happy with it and was getting ready to swap it back and forth with my stock HX35 while Towing and running empty for some real numbers on the Benefits/ improvements. My EGT's were Lower at all boost levels and no problem with lag.
The turbo failed during Fairly heavy acceleration and at around 2300-2500 rpm. Right before shift to 5th gear. We are not sure what failed the shaft, Turbine wheel, Bearings or maybe FOD. It has been sent to Holset for their analysis. The Turbine side was trashed and the Compressor side looked good.
To be fair I had run the turbo at estimated 45+psi boost during my R&D testing looking for the lowest EGT with that Turbo setup.
The best boost setting according to my EGT's and at the time of failure the (wastegate) was set for 36 to 38psi. If the wheel threw a blade first it could of been fatigued from overspeed at the higher boost levels.
One other possibility is shaft failure. On a Diesel engine without the stress that a throttle plate can impose what could cause the shaft to fail? Of course the bearings but with little mileage on the turbo this is not likely. .
My fellow Bombers with experience in HX40 Turbo's and / or the recent rash of failures. What is your Thoughts and Opinions. It will benefit us all if we can find out what improvement or weak link change can be made that will keep them alive and happy.
It was a HX40 Center Section and Wheels with machined 12cm housings. The Turbo work was done at a reputable and established Turbo shop.
It performed exactly as I was told. Lower EGT's, Less Smoke, More Boost and still be Fast Spooling up. I was very happy with it and was getting ready to swap it back and forth with my stock HX35 while Towing and running empty for some real numbers on the Benefits/ improvements. My EGT's were Lower at all boost levels and no problem with lag.
The turbo failed during Fairly heavy acceleration and at around 2300-2500 rpm. Right before shift to 5th gear. We are not sure what failed the shaft, Turbine wheel, Bearings or maybe FOD. It has been sent to Holset for their analysis. The Turbine side was trashed and the Compressor side looked good.
To be fair I had run the turbo at estimated 45+psi boost during my R&D testing looking for the lowest EGT with that Turbo setup.
The best boost setting according to my EGT's and at the time of failure the (wastegate) was set for 36 to 38psi. If the wheel threw a blade first it could of been fatigued from overspeed at the higher boost levels.
One other possibility is shaft failure. On a Diesel engine without the stress that a throttle plate can impose what could cause the shaft to fail? Of course the bearings but with little mileage on the turbo this is not likely. .
My fellow Bombers with experience in HX40 Turbo's and / or the recent rash of failures. What is your Thoughts and Opinions. It will benefit us all if we can find out what improvement or weak link change can be made that will keep them alive and happy.
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