A key step in the development of the famous Chrysler Hemi V8 was this monster: a 2500-horsepower aircraft engine designed for the U.S. armed forces in World War II.
In histories of the Chrysler Corporation (now Stellantis) and its Hemi engine program, the beast shown here is invariably included in the narrative. First proposed to the U.S. Army Air Corps in the summer of 1940, the XI-2220 is quite a remarkable engine, and its hemispherical combustion chambers aren’t the half of it.
Carefully engineered for minimal frontal area and low aerodynamic drag, the 60-degree V16 was barely 33 inches wide—but more than 10 feet long. The layout was an inverted vee, like Germany’s Mercedes-Benz V12s of WWI. That is, as installed in the aircraft, the crankshaft was on top with the cylinders underneath. Another distinctive feature: the big Chrysler’s propeller drive and gear reduction unit were mounted not at the end but at the middle of the crankshaft, in order to control the tremendous torsional vibrations—the forces from the two halves of the engine could now stabilize rather than battle each other. Also due to the engine’s great length and weight (2430 lbs) it was supported at the middle when mounted in the aircraft. Note the massive I-beams and tubular braces that form the cantilevered engine mount.
Each of the 16 liquid-cooled cylinders featured a bore of 5.80 inches and a stroke of 5.25 inches, or nearly 139 cubic inches per cylinder. But instead of a four-valve layout as in the vaunted Rolls-Royce Merlin or the German V12s, the Chrysler engineers opted for two valves per cylinder and hemispherical combustion chambers, already proven effective for decades in auto racing. In its final stage of development with a General Electric turbocharger and charge coolers, the XI-2220 was rated at 2500 takeoff horsepower—more than respectable.
Unlike many of the radical engines under experimental development during World War II, the Chrysler V16 flew successfully, in a pair of highly modified Republic P-47 Thunderbolts (below) in July of 1945. But by then, the war in Europe was over, the war in the Pacific was nearing a resolution, and it was already becoming clear that the jet engine was the future of combat aircraft. But whenever writers sit down to tell the story of the Chrysler Hemi, the fantastic XI-2220 lives again.
Thanks. I saw the engine at the WPC museum a few times and didn’t know what those big brackets were. I thought they were part of the engine stand.
The Allison V-1710 had 4 valve pent roof combustion chambers. I believe the Merlin did not.
The Merlin did have 4 valves per cylinder SOHC…. but had flat roof heads…
Good catch. Bad edit. Now changed. Thanks.
Wow !!! Just when I thought there wasn’t anything more to learn or read about !
how fast was it?
The P-47H is often claimed to have hit very high speeds, but there seems to be no documentation of it exceeding 400 mph in flight tests. As sleek as that ship looks, its engine installation was kind of a lash-up, and the test program was cut short.
….it definitely needed turbocharging with only 2 valves….and it would have made it fantastic as a high altitude interceptor engine. I think with some development on the heads..(i.e. another 2 valves)..it would have made American fighters all American, instead of relying on the Merlins in the P-51’s…I can’t believe how much horsepower could have been achieved with that kind of arrangement….but the Germans wouldn’t have liked it at all!…
The Merlins were USA made under license to RR…
No, Packard made merlins under licence FROM Rolls-Royce, but many US fighters still ended up with the RR…
I seem to recall reading somewhere that it didn’t have conventional valves either, that they were rotary valves thus not disturbing the combustion chamber?
Quite often, the very best examples of a given technology are created just as it becomes obsolete.