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Mr DonL
With the knowledge that we have today , i believe we can agree that BMW 801 was a failure
Never bacame truly reliable
Never had a good power to weight ratio despite it used C3 fuel
Never had even decent altitude performance
Needed that cooling fan behind the propelller that was consuming valuable power
Very inefficient supercharger
The resources and the c3 fuel could had been used for much better projects like Jumo 211R , additionals and faster developed DB605s
I agree. However DB603 engine offered more bang for the buck.
DB603 prototype was running two years before BMW801 prototype and if properly funded I think Daimler-Benz would have maintained at least a two year development lead over BMW801. DB603 was also less expensive to produce, allowed a hub cannon, more reliable and smaller engine diameter made for better aerodynamics, especially in fighter aircraft. It's the engine Fw-190 should have been designed for from 1937 onward rather then betting on a radial engine which didn't even have a prototype running until Fw-190 design was well advanced.
Make BMW801 engine program a low development priority (i.e. similar to historical DB603 funding after 1940). If/when BMW801 engine starts looking promising then development funding gets increased. Otherwise the BMW801 program gets axed after a few years without entering mass production.
I'd call that an excellent tradeoff. No DB604 engine. Full speed ahead with DB603 engine development and mass production.
DonL,
A little off subject but didn't III./JG 27 use the 1.98ata (2000ps) DB 605's in trials around December 1944?
Dear Jim,
that's one of the rare issues we have to disagree.
I can't see where the BMW 801 was a failure.
It was reliable in late 1942 and offers more Steig und Kampfleistung then any other german engine at 1942.
There are certain issues about BMW you have to consider.
BMW was with Bramo the two biggest radial engine producer at germany and both came from the civilian aviation line. Siemens didn't want to enlarge Bramo at the timeline 1934/1935, so Bramo was socialized from the RLM and sold to BMW. Both companys produced their civilian line BMW 132 (P&R 1630) and Bramo 323 (Bristol Jupiter), both heavy modified from both companys, but both had relative old production lines and tools.
The fusion of Bramo and BMW happened since 1937/38, BMW new engine factory was built not until 1938 (Junkers and DB factorys were built much earlier) and through the fusion, the civilian market and the failure of the BMW 139, BMW was very late in the military engine development with the BMW 801, which was developed out of the BMW 139 and Bramo 329.
The main issues for BMW/Bramo was the tooling of the new built engine factory at 1938, because it was this late, BMW had to fight with endless other companys about good around toolings to equip their engine factory. This fighting holded on till 1943 and BMW had not as much modern allround production tools as DB and Junkers.
Anyway from a rational viewpoint it was more then clear for the RLM to fund a a new military radial engine from this two fusioned engine companys (advertisement 1935), to get the human resources (engine engineers) and production lines to work for the military development.
BMW/Bramo was compare to DB and Junkers a very small company 50000 workmen at 1944 (half of this slave laboured) and was able to develop the BMW 801 and the BMW 003 and put both in mass production.
The BMW 801 is to my opinion absolutely comparable to the Wright 2600 and very equal in performance.
The most issues of BMW/Bramo was their late change to the military development of engines, so they had major issues with production tools, human resources (engine engineers) and not the reputation of Junkers and DB and were always number 3 at the RLM, also at the attention and treatment through the RLM.
Most important point here has nothing to do with the carburetor.R-2600-3 series engine failed its 150-hour type test (July 1939), largely because of the PD carburetor
R-2600 Case History
Most important point here has nothing to do with the carburetor.
1,600hp R2600 engine was conducting 150 hour test during July 1939. About three years before BMW801 engine could pass a similar test. Probably about the same time 1,600hp DB603 engine would have attempted a similar test if program funding hadn't been cancelled during 1937.
R2600 engine development began during 1935. DB603 engine development began during 1936 (before it was cancelled during 1937).
If RLM desires BMW to development a large radial engine they should fund development NLT 1936. By 1939 it's too late. Germany was staring war in the face so they must manufacture engines which are production ready or close to it.
In the 1930s, BMW took out a license to build the Pratt Whitney Hornet engines. By the mid-30s they had introduced an improved version, the BMW 132. The BMW 132 was widely used, most notably on the Junkers Ju 52, which it powered for much of that design's lifetime.
In 1935 the RLM funded prototypes of two much larger radial designs, one from Bramo, the Bramo 329, and another from BMW, the BMW 139. BMW bought Bramo soon after the projects started; unsurprisingly BMW folded the Bramo engineers into the BMW project, cancelling the Bramo design. The resulting proposal was essentially a two-row version of the BMW 132, the 1,550 PS (1,529 hp, 1,140 kW) BMW 139.
Radial engines were rare in European designs as they were considered to have too large an area for good streamlining and would not be suitable for high speed aircraft (the US Army agreed, see hyper engine). However, radials were often used in American and Japanese fighters at the end of the 1930s, and improvements in the cowlings for radial engines were reducing the concerns about drag.
If it's worthwhile then why wait until 1939 to begin development?
BMW132 was in production by 1934. That's when development of next generation radial engine should have begun.
The main concern was providing cooling air over the cylinder heads, which generally required a very large opening at the front of the aircraft. Tank's solution for the BMW 139 was to use an engine-driven fan behind an oversized prop-spinner, blowing air past the engine cylinders, with some of it being drawn through S-shaped ducts over a radiator for oil cooling. However this system proved almost impossible to operate properly with the BMW 139; early prototypes of the Fw 190 demonstrated terrible cooling problems. Although the problems appeared to be fixable, since the engine was already fairly dated in terms of design, in 1938 BMW proposed an entirely new engine designed specifically for fan-cooling that could be brought to production quickly.
The BMW 801 would eventually be fitted with a magnesium alloy cooling fan that rotated at 1.72 times the crankshaft speed (3.17 times the propeller speed).[2] This provided effective cooling although at the cost of about 70 PS (69 hp, 51.5 kW) required to drive the fan when the aircraft was at low speed. Above 170 miles per hour (270 km/h), the fan absorbed little power directly.[2]
This seems misleading. A Fw 190C with a DB 603 with 2000 hp would not be available until 1945. Even the DB 603E was stuck at 1,800 hp. I still have my doubts if DB 603s with methanol injection ever reached operational status.Focke Wulf tested 3 prototypes to assess performance of Fw 190 with DB 603. Fw 190 V-13, V-15 and V-16. The last one flew in August 1942. There were no major problems with the installation and in a few months production could have been started. I have created a graph comparing Fw 190 A and C performance.
If it's worthwhile then why wait until 1939 to begin development?
BMW132 was in production by 1934. That's when development of next generation radial engine should have begun.
Why did BMW require a lengthy vacation before beginning work on next generation air cooled radial?