Alaska Aviation Museum - (unofficial)

Engines - Liberty L-12

Engines
Continental
Jacobs
Liberty
Liberty Maint
Lycoming
Pratt & Whitney
Wright
Wright Maint
Wright J5 Maint
Various
Overview
State
Signs

Liberty L-12

liberty12-3-4-side-view.jpg

The United States declared war on Germany on April 6, 1917. The Aircraft Production Board, then headed up by Howard E. Coffin of the Hudson Motor Car Co. and his assistant Edward A. Deeds, a major stockholder in Delco, set the basic parameters for what would come to be known as the Liberty. The new engine would be lighter and slightly more powerful than the Rolls-Royce Eagle. Modular construction, employing common cylinder and valve components, would slash development time and permit the engine to be used on all types of airplanes from trainers to heavy bombers. And all this would be accomplished within the strictures of a conservative design philosophy.

The first of many expedients was to telescope layout into a two-day (some say five-day) marathon at the New Willard hotel in Washington, DC that begun in the afternoon of May 31, 1917. At General Pershing's request, the L-8 was put on hold in favor of a 12-cylinder L-12 that would be more powerful than existing Allied engines. The first of these was tested in August, 1918.

The 45ยบ cylinder angle raised questions about torsional vibration. Robert J. Raymond demonstrated that the L-12 crankshaft underwent severe torque peaks at 1,333 rpm, 1,714 rpm and 2,000 rpm. Any of these inputs could result in failure. Raymond quotes two studies dating from the 1930s that indicate the presence of torsional vibration at certain operating speeds. One of these studies described Liberty crankshaft breakage as "epidemic."

The Liberty had other faults. C. Fayette Taylor, who was in a position to know, reported that half of the early production engines could not pass the 50-hr acceptance test. Burnt exhaust valves and, as has been pointed out, accessory-gear failures were common on all versions.

TBO, or time between overhauls, is the primary measure of durability. By 1926 Navy L-12s were averaging 75 hours between overhauls. Newer air-cooled engines had TBOs of 300 hours

Once the war ended, the problem became what to do with the engines, for which few airframes were available. Some were donated to the Air Mail Service and vocational schools, and others were sold as surplus for pennies on the dollar. Rum runners found that 400 hp gave them an advantage over Coast Guard cutters. Still, by 1924, 11,810 L-12s remained in inventory, enough to satisfy military needs for 26 years.

Although the Liberty had very limited application for military aircraft, the overhang made it difficult to justify acquisition of newer and more expensive power plants.

Attempts to convince commercial operators to adopt the engine on economic grounds failed. It vibrated, weighed more than it should, and had a reputation for unreliability. Army mechanics did their part by foregoing overhauls. When an L-12 needed work, they replaced it with a new one. That practice continued until 1929.

Liberty Maintenance

Used on the 1924 Douglas World Cruiser

enginehistory.org Notes on the Liberty Aircraft Engine

(Wikipedia) - Liberty L-12

Liberty L-12

General Characteristics
First Run: 1918
Number Built: 20,748
Type: 12-cylinder liquid-cooled Vee piston engine
Bore: 5 in 127 mm
Stroke: 7 in 178 mm
Displacement: 1,649 cu in 27.03 L
Length: 67.375 in 1,711 mm
Width: 27 in 685 mm
Height: 41.5 in 1,054 mm
Dry weight: 845 lb 383.3 kg
Components
Valvetrain: 1 inlet and 1 exhaust valve per cylinder
Fuel system: Two duplex Zenith Carburetors
Fuel type: Gasoline
Oil system: Forced feed, rotary gear pressure
and scavenge pumps, wet sump
Cooling system: Water-cooled
Performance
Power output: 449 hp at 2,000 rpm (takeoff) 334 kW
Specific Power: 0.27 hp/cu in 12.4 kW/L
Compression ratio: 5:1
Specific fuel consumption: 0.565 pt/hp/hour
≈28 gal/hour
0.43 l/kW/hour
Oil consumption: 0.0199 pt/hp/hour
≈1 gal/hour
0.0152 l/kW/hour
Power-to-weight ratio: 0.53 hp/lb 0.87 kW/kg

The Bulletin of the
Airplane Engineering Department, U.S.A.

Vol. 1     June 1918     No. 1
United States. Bureau of Aircraft Production
Airplane Engineering Department

Google Books - page 79

Date of Test - April 1, 1918

In order to obtain some idea of how much of the heat value in the gasoline used for running the high compression Army type of Liberty 12- cylinder engines goes into actual horsepower and how much is dissipated in friction, jacket water and exhaust, a test was recently run at McCook Field. It was found that the average brake horse power developed was 372, or 27.3 percent of the total theoretical horsepower, and that the average amount absorbed in the form of heat by the jacket water was 339 or 24.8 percent, while 44.4 percent was carried off in the exhaust, and the remaining 3.5 percent was lost in friction.

  Horsepower Percent
Average 372 27.3 %
Heat in Jacket Water 339 24.8 %
Heat in Exhaust 44.4 %
Friction 3.5%
Total Theoretical Horsepower

Fuel/Oil Consumption

  Lbs/HP/Hour 1 Hour Gallons
Gas 0.492 183.27 30.50
Oil 0.035 13.03 1.85
liberty-L-12 Hap Arnold
Major Henry H. Arnold standing beside the first Liberty 12 aircraft engine turned out for war use. “Hap” Arnold would later hold the 5-star rank of General of the Army and General of the Air Force. (U.S. Air Force)

Liberty-dwg-end.jpg

Liberty Dwg End

Liberty-dwg-side.jpg
Liberty Dwg Side
liberty-L-12
AAM - Liberty engine from the Douglas World Cruiser "Seattle"

liberty12-3-4-side-view.jpg

liberty12-ministry-of-munitions.jpg

liberty12-switchboard.jpg

liberty12-top-view.jpg