The First Airplane Diesel Engine: Packard Model DR-980 of 1928Meyer, Robert B.
History
The First Airplane Diesel Engine: Packard Model DR-980 of 1928
Meyer, Robert B.
Airplanes -- Motors (Diesel)
[Illustration: Figure 32.--Front left view of engine from Packard Motor
Car Co. 50-hour test, 1930, showing butterfly valve type venturi
throttles. (Smithsonian photo A48325E.)]
[Illustration: Figure 33.--Front left view of engine from U.S. Navy
test, 1931, showing spiral oil cooler. (Smithsonian photo A48324A.)]
Crankcase: It was strengthened by having external ribs added. Note the
contrast between the first engine, figure 2, and a later model, figure
32.
Oil Cooler: The drum-shaped honeycombed cooler was replaced by a spiral
pipe type located between the engine cowl and the crankcase. Figure 3
shows an example of the former type of cooler located at the top of the
engine between two of the cylinders. Figure 33 illustrates the latter
type located between the cowling and the crankcase.
Cylinder Fastening: Early models had their cylinders strapped and bolted
to the crankcase. Later ones had them only strapped. Figure 2 shows a
bolt-fastened clamp between two of the cylinders on the first engine.
Figure 19 shows a later model without any bolts holding down the
cylinders.
Pistons: The pistons used in the 1929 engine had one compression ring
and one oil scraper ring above the piston pin, and one oil scraper ring
below it. There were three grooves, two above the piston pin, and one
below it.[17] Pistons used in 1930 had two compression rings, one oil
scraper ring above the piston pin, and one oil scraper ring below it.
There were four grooves, three above the piston pin, and one below
it.[18] The 1931 pistons had one compression ring above the piston pin,
and one compression ring and four oil scraper rings below it. There were
four grooves, one above the piston pin, and three below it.[19]
[Illustration: Figure 34.--Modified pistons after endurance run. U.S.
Navy test, 1931. (Smithsonian photo A48325D.)]
Combustion Chamber: In 1931 the contour of the cylinder head was changed
slightly. This improved the combustion efficiency to the extent that the
stroke of the fuel pumps could be decreased about 15 percent. The
specific fuel consumption then decreased about 10 percent. In addition
the compression ratio was reduced from 16:1 to 14:1.[20]
These changes were designed to eliminate smoke from the exhaust at
cruising speed, and to reduce it at wide-open throttle.
Valves: A two-valve-per-cylinder model was built, but not put into
production. It featured more horsepower (300), a higher rate of
revolutions per minute (2000), and a better specific fuel consumption
(about .35 lb/hp/hr).[21]
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