Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 15-Jan-2019

This is "General Motors Research Laboratory", a part of the conglomerate of sections and companies of the General Motors Group.

-For aviation engines its best standard was Allison.

-A group of GMRL engineers such as Goldthwaite, Hallet, Wittner, etc ... developed an idea of ​​higher performance engines based on the use of two-stroke cycle (double effective strokes of the four-stroke) but with twin cylinders and a common combustion chamber.

The12 cylinders (24) boxer from GMRL
“The12 cylinders (24) boxer from GMRL”

-The first demonstration was a project of 12 twin cylinders (total 24 cylinders). There was a 10-cylinder project to save weight and size.

Versión radial de la misma idea: el U-173
“Radial version with the same idea: the U-173”

-They needed supercharging to force the mixture into the cylinders. The intake was done through the base of one and the exhaust through the other one.

-The U-173 gave only 90 hp. With later models the power and the number of cylinders increased. The U-744 was a radial with six double cylinders.

U-744 radial engine
“U-744 radial engine”

-They made an engine with ten radially arranged cylinders, the U-1240, also in the early 1930's.

GMRL U-1240 side view
“U-1240 side view”

GMRL U-1240 rear view drawing
“U-1240 rear view drawing”

-The superchargers were generally Roots as on the U-250, but centrifugal ones were also used as on the X-250.

GMRL U-250, with the Roots compressor on the foreground
“U-250, with the Roots compressor on the foreground”

GMRL X-250 front view cross-section
“X-250 front view cross-section”

-This engine has a large-diameter, centrifugal compressor at the rear and taking in through the carburetor.

-They were used on unmanned aircraft around 1941.

GMRL X-250 drawing

GMRL X-250, with centrifugal compressor
"X-250, with centrifugal compressor"

Drone designed by Cessna with GMRL X-250 engine
"Drone designed by Cessna with X-250"

Engines of GMRL

Model: 10 cyl. 2-str. boxer

Arquitecture: 2-stroke10-cylinder Horizontally opposed
Cooling:
Total Displacement:
Bore / Stroke:
Power:
Weight:

Other details:
Model: 12 cyl. 2-str. boxer

Arquitecture: 2-stroke12-cylinder Horizontally opposed
Cooling:
Total Displacement:
Bore / Stroke:
Power:
Weight:

Other details:
GMRL 12-cylinder (24) boxer

"GMRL 12-cylinder (24) boxer"

Model: U-1000

Arquitecture:
Cooling:
Total Displacement:
Bore / Stroke: x
Power:
Weight:

Other details:
Model: U-1240

Arquitecture: 10-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power:
Weight:

Other details:
U-1240 side view drawing

"U-1240 side view drawing"

Model: U-173

Arquitecture: Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power: 90 HP
Weight:

Other details:
Radial version of the same idea: the U-173

"Radial version of the same idea: the U-173"

Model: U-250

Arquitecture:
Cooling:
Total Displacement:
Bore / Stroke: x
Power:
Weight:

Other details:
U-250, with roots compressor

"U-250, with roots compressor"

Model: U-744

Arquitecture: 6-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power:
Weight:

Other details:
Model: X-250, -1, -2, -3, -D

Arquitecture: X-engine
Cooling:
Total Displacement:
Bore / Stroke:
Power:
Weight:

Other details:
X-250, with centrifugal compressor

"X-250, with centrifugal compressor"

Model: XR-250

Arquitecture:
Cooling:
Total Displacement:
Bore / Stroke: x
Power:
Weight:

Other details: