Updated: 24-Feb-2020
Aviation engines built at the “Labor” car factory in Neuilly.
-Particularly applied to the Bleriot and Hanriot planes among others and during a certain time.
-In 1911, Labor participated with a four-cylinder in the Reims Military Contest of that year, on a Savary biplane.
“Labor engine cross-section”
-It had two camshafts and combustion chambers in "T", Claudel carburetor, magneto ignition and water cooling.
“Side view of the Labor engine”
-A recently located unpublished exhaust side view, in which we can see the the water pump drag, which in turn drives the magneto.
-We also can see the lubrication tubes that go to each cylinder wall. The engine gave 70 CV.
-In the rear view we see the uncovered distribution gears and above it there are the grease pumps as a whole with their different outputs.
-On the right there is a control that alternately drives a greasing piston.
-The best known engines were those with a power of 42 CV (90 x 150 mm cylinder size) at 1,300 rpm.
-And the those with 73 CV at 1,350 rpm (100 x 120 mm).
-The perpendicular axis of the cylinders was misaligned 10° in reference with the crankshaft. Called "desaxe engine"
-As we see, the distribution was uncovered.
“Labor, photo”
Engines of LABOR
Model: 4 cyl. inline, 42 CV
Arquitecture: 4-cylinder In-line
Cooling:
Total Displacement:
Bore / Stroke: 90 x 150
Power: 42 CV @ 1300 rpm
Weight:
Model: 4 cyl. inline, 70/73 HP
Arquitecture: 4-cylinder In-line
Cooling:
Total Displacement:
Bore / Stroke: 100 x 120 mm
Power: 72 CV @ 1350 rpm
Weight: