Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 08-Oct-2020

After WWII, the Cameron Aero Engine Corporation made one of the few American inverted inline engines of the time.

Cameron C4-I-E1
"Cameron C4-I-E1"

-The C4-Y-E1 from 1946 with its four inverted inline cylinders had a displacement of 301 cu.in. and gave 125 hp.

-Before the war, in 1928, when it was called "National Aero Corp" it made the 60 hp engine with the same arrangement, and the 7-cylinder radial engine that gave 100 hp.

-Returning to the illustration, the 125 hp power output was achieved at 2,500 rpm, while at cruise speed they gave 110 hp at 2,200 rpm.

-Like in German Zündapp engines, the opposed valves in the cylinder heads needed the camshaft divided into two, one on each side of the engine.

-They were one of the first to use magnesium crankcase in the USA. These engines used an injection carburetor, that is, a mixture of carburetor and injection system called "Bendix-Stromberg Pressure Diaphragm Injection”.

-In relation to the picture of the Cameron engine with inverted cylinders and laterally arranged valves.

-There are two more designs for air-cooled engines around 1929.

-These engines were designed by Everett Cameron and built by the National Aero Corp.

-One engine was an upright four-cylinder giving 60 hp. This was the first Cameron, apparently.

Cameron, 60 hp
"Cameron, 60 hp"

-The originality of this engine was that it had four valves per cylinder but located horizontally, two on each side. The valve actuation device by camshaft was original.

Cross-section for Cameron cylinders
"Cross-section for Cameron cylinders"

-There was a version of a seven-cylinder radial engine that gave 100 hp. We can clearly see the side valves in each cylinder head, in twos.

-Presumably this system would present an engine with a smaller front area.

Cameron radial
"Cameron radial"

Edward Cameron with his radial
"Edward Cameron with his radial"

From Appendix 10: Formerly it was National Compression and Aero Compression. Designs of aviation engines were due to Edward Cameron.

-The 7-cylinder radial engine, of which we now have more illustrations, had a characteristic that distinguished it from its congeners: The position of the two valves in the cylinder head.

Two views for the Cameron radial engine
"Two views for the Cameron radial engine"

-The design is from around 1928. It seems that there are several valves per cylinder head. Two intake and one exhaust.

-It gave 100 hp at 1,800 rpm.

Cameron radial engine diagram
"Cameron radial engine diagram"

Engines of CAMERON

Model: 60 HP, in line, 4 cils.

Arquitecture: 4-cylinder In-line
Cooling:
Total Displacement:
Bore / Stroke:
Power: 60 HP @ rpm
Weight:

Other details:

It had four valves per cylinder but they were placed horizontally, two on each side.

Cameron, 60 HP

"Cameron, 60 HP"

Model: 60/100 HP, radial de 7 cils. (ver National Aero

Cameron radial

"Cameron radial"

Model: C4-I-E1, 125 HP

Arquitecture: 4-cylinder In line inverted
Cooling:
Total Displacement: 301 cu. in.
Bore / Stroke:
Power: 125 HP @ 2500 rpm
Weight:

Other details:

It had a max. power output of 125 hp at 2,500 rpm, while at cruise speed it gave 110 hp at 2,200 rpm.

Cameron C4-I-E1

"Cameron C4-I-E1"

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