Having read through most of these posts I can see where some folks may not buy into the benefits of this unit without seeing dyno results. I'm certain that the theory behind this is sound and in fact, "theory" isn't the right word to use here... this is real science. That thing works and I make that statement merely by looking at the picture.
I should probably state my background up front before the BS flag goes up... I'm a 21 year veteran of Naval Aviation and an FAA certified Airframe and Powerplant technician. I've worked on everything from Vietnam era fighters to Tomcats, Hornets, and most modern commercial platforms. I also served 12 years as a Flight Engineer on multi engine reconnaisance aircraft.
That said, I have
NEVER seen a jet engine that didn't have some type of flow straightener at the compressor inlet. If you look at the photo below, you can see what amounts to a lame attempt by Dodge to accomplish the same effect...
#ad
... if you look below the intake silencer you can see some white-ish looking plastic vanes (this is my 05 Cummins BTW). These vanes are an attempt at directing the airflow more evenly at the compressor vanes. While they likely do an adequate job, they don't nearly equal a honeycomb setup and the thickness of the vanes obstruct airflow to an extent. Just by looking at the TAG I can tell it does a superior job. If you're looking for "dyno" numbers, I think you'll be disappointed. Any gains from this unit are likely experienced under the curve and are small BUT... what it will do, as the inventors claim, is make the turbo compressor much more efficient which equates to several advantages...
1. Turbo efficiency. While power increases on the dyno may be small or nonexistant, turbo response is greatly improved. This likely accounts for the SOTP increases reported by users. What they're feeling is a snappier response to throttle.
2. Boost for a given pedal position will likely go down. Why? Because the engine doesn't need as much boost to make the same amount of power. What you have to keep in mind here is that exhaust energy has to spin the spool. If the spool is easier to spin (because of laminar flow), less heat/exhaust energy is wasted on spinning it and less heat is absorbed by the exhaust impeller. The result... lower boost (not peak boost), lower exhaust backpressure, cooler compressor/exhaust impeller temps and a longer lasting turbo.
Take a look inside the MAF housing of any modern gas engine that incorporates an elbow prior to the MAF inlet... you'll find a honeycomb screen.
Heck ... I just sold myself... where can I get one of these things
