Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 26-Feb-2020

In 1935, Mr. E.W. Lamb of Middlesex presented an interesting three-cylinder, two-stroke radial engine with rotary head valves.

Lamb engine
“Lamb engine”

-As original design it presented two characteristics that we can see in the engine cross-section.

Schematic drawing of the Lamb engine
“Schematic drawing of the Lamb engine”

-The pistons were double bore, the lower one being the largest and the mixture was blowing towards the upper and smaller diameter working piston. (see Prini et Berthaud engine or simply Berthaud).

-The other feature is the rotary valve (Aspin Type) but instead of continually turning it did it with pulses because it made use of a mechanism known as "Maltese Cross".

Maltese Cross mechanism
“Maltese Cross mechanism” (PeT=Wikipedia)

-This device was also used by film projectors to match the frame with the full shutter opening.

Engines of LAMB

Model: 3 cyl, radial. rotary valve

Arquitecture: 3-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power:
Weight:

Other details:
Lamb engine

"Lamb engine"

The author of this edition of Aeroengines AtoZ, through Aeroteca, collaborated on Version 2 of this video, which is presented here.

To understand the operation of the connecting rods, the 1929 Continental R 670 single-cylinder engine was chosen.

A demonstration of Version 3, improved at the author's suggestion, is also available on YouTube at a later date. This version shows bronze valve guides, improved valve spring movement, and the split crankshaft counterweights and front bearing balls also move.

The design is from Juan Soler, Sant Cugat, Barcelona

Below we show a flash of version 3

Counting also with the coloboration of JMC of Enginys Mecanics in Mataro, Barcelona