For all of you motor heads out there, you’re going to love this!
Pictured below is a recent acquisition of mine, and is probably the oddest and most unique piece of aero “junque” I’ve ever seen. What you’re looking at is a factory mockup of a Continental XO-1430-3 engine. It is a liquid cooled “flat 12” opposed piston engine. It is constructed primarily of wood, and the detail is absolutely incredible for this type of construction. It is also quite a massive engine, measuring over 6ft long by 4ft wide, and standing nearly 2ft tall on the mounts. Truly a beast!
I’ve been trying to determine exactly what this engine was conceived for, and I believe it MIGHT have been used in a XB-35 mockup? Any Northrop guys out there? I found a very old tag attached to the engine, part of which is missing, but by “filling in the blanks” it says in part “…..For Wooden Mockup Of Flying Wing”
I’ve been in touch with a Mr. Graham White who just so happens to own a Continental IV-1430 engine (one of only a handful known to survive, and the only one still operational) Graham was very helpful with my query into the XO-1430, but he was just as mystified by it as I am. He himself had never heard of an XO-1430 before either, and believed my example to be the only one to exist. Still more perplexing was the possible Northrop connection indicated by the tag attached to the engine.
Graham's IV-1430 can be seen here:
http://www.enginehistory.org/iv-1430.htm
Graham also indicated that NASM actually has manuals for the IV-1430, and that they could possibly have something on the XO-1430. I do intend to contact them about this, but I’m still waiting to hear back from them with regards to some XB-29 stuff, so in the meantime I’m hoping a WIXer out there might be able to help me out w/ this beast! The only thing I’ve found on the net about the XO is as follows:
"The US Army at McCook Field (later at Wright Field) began cylinder research in 1929 under the direction of S.D. Heron and others. By 1931, a twelve cylinder, V-12 liquid-cooled engine with {4.625 / 5.0 / 1008.0} had been developed. In 1934, the US Army increased the cylinder size to 1425 cu. in. for a V-12; this was redesigned further into the OL-1430 and tested in 1938. The motivation for a high-power HOAE was the promise shown for low-drag, in-wing installation, but this soon was seen as impractical (see, also, the Lycoming OL-1230). Later, the OL-1430 was redesigned into the Continental IV-1430, which was an inverted V-12.
12cyl; O-1430-1; 1150hp@3150rpm; 1938-1941; Wt = 1300#; TC = none.
Supercharged and geared to 0.455 or 0.556.
Aerofiles.com; AMC; BGE; BGP.
Applications: None found.
12cyl; XO-1430-3; 1500hp@3150rpm; 1938-1941; Wt = 1600#; TC = none.
Supercharged and geared to 0.336.
Aerofiles.com; AMC; BGE; BGP.
Applications: None found.
http://home.adelphia.net/~aeroengine/Continental2.html
I also found the following mentioned with regards to the XB-35:
“In November, 1941, two XB-35 prototypes were ordered by the Army Air Force. Preliminary design work began on the XB-35 early in 1942, and on July 5th of that year the mock-up Board from Wright Field inspected a full size wood mock-up of the centre section and a portion of the left wing.”
http://www.century-of-flight.freeola.com/Aviation%20history/evolution%20of%20technology/Northrop.htm
While the XB-35 ultimately used the -4360, there is no mention to the type of engine(s) employed in the partial mockup from 1942. This, coupled with the tag I found attached to the engine raises the question; could my XO-1430 have been used in this mockup? Can anyone confirm what type of engine was used in the mockup from ’42?
If anyone out there has any additional info on this engine, please post it here or e-mail me