Specifications

The following specifications are for the production engine and its

prototypes, known as the model DR-980:[11]

Type 4-stroke cycle diesel

Cylinders 9--static radial configuration

Cooling Air

Fuel injection Directly into cylinders at a pressure of

6000 psi

Valves Poppet type, one per cylinder

Ignition Compression--glow plugs for starting--air

compression 500 psi at 1000 deg. F.

Fuel Distillate or "furnace oil"

Horsepower 225 at 1950 rpm

Bore and stroke 4-13/16 in. x 6 in.

Compression ratio 16:1--maximum combustion pressure 1500 psi

Displacement 982 cu in.

Weight 510 lb without propeller hub

Weight-horsepower ratio 2.26 lb hp

Where manufactured U.S.A.

Fuel consumption .46 lb per hp/hr at full power

Fuel consumption .40 lb per hp/hr at cruising

Oil consumption .04 lb per hp/hr

Outside diameter 45-11/16 in.

Overall length 36-3/4 in.

Optional accessories Starter--Eclipse electric inertia; 6 volts.

Special series no. 7

Generator--Eclipse type G-1; 6 volts

[Illustration: Figure 17.--Longitudinal cross section, Packard diesel

engine DR-980. (Smithsonian photo A48845.)]

[Illustration: Figure 18.--Transverse cross section, Packard diesel

engine DR-980. (Smithsonian photo A48847.)]

[Illustration: Figure 19.--Right side view of engine, showing

accessories; Packard Motor Car Co. 50-hour test, 1930. A, starter; B,

oil filter. (Smithsonian photo A48323.)]

[Illustration: Figure 20.--Rear left view of engine, showing

accessories, U.S. Navy 50-hour test, 1931. Barrel valve type venturi

throttles. A, starter; B, oil filter; C, fuel circulating pump; D,

generator. (Smithsonian photo A48324C.)]

The First Airplane Diesel Engine: Packard Model DR-980 of 1928 · 第 16 / 44 题