Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 28-Feb-2019

In 1938, mr. H.E. Hebrard, presented the design of a 2-stroke diesel engine with rigid rods.

Hebrard engine
“Hebrard”

-The principle is that of guided sliders, where the crankshaft main journal slides.

-It was tested at the Brandt Establishments. It is logical to think that with these engines the masses in motion seem greater than those of the classic engines.

-It is not the first engine that uses rigid cranks and an elongated hole for crankshaft rotation (see Bourke).

Engines of HEBRARD

Model: Diesel, 2-stroke (1938)

Arquitecture: 2-stroke
Cooling:
Total Displacement:
Bore / Stroke:
Power:
Weight:

Other details: