The ongoing saga of my little BC-65 cylinder head temperature chase continues.
Last week I invoked the emergency provisions of Dr. Seuss' theory of Calculatus Eliminatus. I have tried everything else, which left only one thing untried.
I made a template of the lower cowling and firewall, specifically tracing the actual size and shape of the air exit under the firewall onto paper. This drawing was then held up to the front of the cowling, and I was immediately hit with 'the mighty sledgehammer of the obvious'.
The combined size of the air intakes at the front of the cowl were approximately one and one half or more as large as the area of the exit under the firewall. It's commonly known that this is just about exactly backwards. The one thing that I had ASSUMED was correct was the original factory design of the air inlet and outlet. So I spent darn near a year now, chasing everything else.
Two or three things have been considered to solve this airflow bottleneck at the exit. Louvering or shark gills in the cowling, an enormous cowl flap, or reshaping the cowl to hang lower under the firewall making a bigger exit.
The last option was chosen as the best method because it would change the look of the airplane the least. The plan was decided to stretch the cowling down an inch or two, and make a spacer or standoff part for the gap between the lower cowl (and Dzus fastener) and the welded center firewall mount.
Despite my desire to use a jackhammer after all these trials and tribulations, it was admitted that the best tool for the job was an English Wheel.
Today was my second trip to go see an old guy at another local EAA Chapter who owns and operates one of these mystic magic marvels. The first trip didn't stretch the metal much because the metal was hard. So I took it to a heat treat place and had it annealed back to half-soft. I don't want to talk about the burned paint and carbonized felt strips... it looks like the back side of the moon!
Today we rolled it again between the big steel wheels and stretched on it again, and it moved a bunch. Put it back on the airplane and noted where it still needed some more squishing.
But the center of the cowl now sits another inch and a half below the center firewall mount. Should let out a lot more air!
Tomorrow I'll try to go back and have the guy whack at it some more.
I could have built an entire Zenair 701 or a Hummel Bird or a nice cabin in the woods in the same time I've spent on this one little problem !
Last week I invoked the emergency provisions of Dr. Seuss' theory of Calculatus Eliminatus. I have tried everything else, which left only one thing untried.
I made a template of the lower cowling and firewall, specifically tracing the actual size and shape of the air exit under the firewall onto paper. This drawing was then held up to the front of the cowling, and I was immediately hit with 'the mighty sledgehammer of the obvious'.
The combined size of the air intakes at the front of the cowl were approximately one and one half or more as large as the area of the exit under the firewall. It's commonly known that this is just about exactly backwards. The one thing that I had ASSUMED was correct was the original factory design of the air inlet and outlet. So I spent darn near a year now, chasing everything else.
Two or three things have been considered to solve this airflow bottleneck at the exit. Louvering or shark gills in the cowling, an enormous cowl flap, or reshaping the cowl to hang lower under the firewall making a bigger exit.
The last option was chosen as the best method because it would change the look of the airplane the least. The plan was decided to stretch the cowling down an inch or two, and make a spacer or standoff part for the gap between the lower cowl (and Dzus fastener) and the welded center firewall mount.
Despite my desire to use a jackhammer after all these trials and tribulations, it was admitted that the best tool for the job was an English Wheel.
Today was my second trip to go see an old guy at another local EAA Chapter who owns and operates one of these mystic magic marvels. The first trip didn't stretch the metal much because the metal was hard. So I took it to a heat treat place and had it annealed back to half-soft. I don't want to talk about the burned paint and carbonized felt strips... it looks like the back side of the moon!
Today we rolled it again between the big steel wheels and stretched on it again, and it moved a bunch. Put it back on the airplane and noted where it still needed some more squishing.
But the center of the cowl now sits another inch and a half below the center firewall mount. Should let out a lot more air!
Tomorrow I'll try to go back and have the guy whack at it some more.
I could have built an entire Zenair 701 or a Hummel Bird or a nice cabin in the woods in the same time I've spent on this one little problem !
Comment