Ford GAA engine

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Ford GAA
FordGAA 1.JPG
Overview
Manufacturer Ford Motor Company
Production1940-1950
Layout
Configuration 60° V8
Displacement 1,100 cu in (18 L)
Cylinder bore 5.4 in (137 mm)
Piston stroke 6.0 in (152 mm)
Valvetrain DOHC
Compression ratio 7.5:1
Combustion
Fuel system Naturally aspirated with Stromberg NA-Y5-G carburetors [1]
Fuel type Gasoline
Cooling system Liquid
Output
Power output 500 hp (373 kW) @ 2,600 rpm
Torque output 1,050 ft⋅lbf (1,424 N⋅m) @ 2,200 rpm
Dimensions
Length59.02 in (150 cm)
Width33.25 in (84 cm)
Height47.78 in (121 cm)
Dry weight 1,470 lb (667 kg)

The Ford GAA engine is an American all-aluminum 32-valve DOHC 60-degree liquid-cooled V8 internal combustion engine with a flat-plane crank designed and produced by the Ford Motor Company before and during World War II. It features twin Stromberg NA-Y5-G carburetors, [2] dual magnetos and twin spark plugs making up a full dual ignition system, [2] and crossflow induction. [3] It displaces 1,100 cu in (18 L) and puts out well over 1,000 pound-feet (1,400 N⋅m) of torque from idle to 2,200 rpm. The factory-rated net output was 500 hp (370 kW) at 2,600 rpm.

Contents

The GAA powered several models and derivatives of the M4A3 Sherman medium tank.

Development

After the start of World War II, UK was looking to manufacture complicated parts (notably the crankshafts) of the Rolls-Royce Merlin in the US, but negotiations with Packard stalled because the company insisted on making complete engines. In June 1940 production drawings arrived in North America and were seized by the US Treasury Department, that's when Ford engineers were able to copy them and soon derive a clone simplified for industrial production at Ford's factories.

It was a 60 degree V-12 of 1,650 cubic inch displacement with cylinder bore and stroke matching the Merlin aviation engine, using an aluminum block and head; dual overhead camshafts, and four valves per cylinder. The intention of this design was to help Ford break into the anticipated large market for aircraft engines. This engine was built to typical aircraft standards: it was light, high performance, and highly reliable. Everything was safety wired or staked with close attention to detail on every part. Available information suggests this design performed well.[ citation needed ]

However, it never went into production as an aircraft engine due to the United States Navy's decision to only use radial engines for its aircraft and the Army's contractual commitments to existing manufacturers.[ citation needed ]

With the approach of war, increasing orders for M4 Sherman tanks were causing supply issues with the 9-cylinder radial Wright R-975 Whirlwind engine used. The U.S. Army decided it needed to source additional engine suppliers, choosing a version of the Ford GAA cut down from twelve cylinders to eight for various vehicle applications.

In 1942 after the British Tank Mission visit to America in April, there was some pressure from British car and commercial vehicle manufacturers to use the new Ford V8 tank engine designed by Larry Sheldrick in British tanks, rather than the Meteor then under development by Rolls-Royce from the Merlin aero engine, as they believed that an adapted aero engine "would not be suitable as a rugged tank engine". The Ford engine prototype had a few hundred hours test-bed running by that time. It was a liquid-cooled Vee similar to the Meteor, but two-third the size and Rolls-Royce executive W. A. Robotham doubted its reliability at 600 bhp. The 600 bhp Meteor was designed to fit in the same space in the Crusader (tank) as the Nuffield Liberty L-12 engine of 340 bhp output. The Ford V8 developed only 500 bhp, and had problems which were not overcome until after the Normandy landings in 1944. [4]

Production

All-aluminum Ford GAF V8 tank engine, next to an M26 Pershing, The Tank Museum Bovington 091 Ford V8 1.jpg
All-aluminum Ford GAF V8 tank engine, next to an M26 Pershing, The Tank Museum

See also

Notes

    1. Berndt, Thomas. Standard Catalog of U.S. Military Vehicles (Krause Publications, 1993), p.193.
    2. 1 2 Berndt, p.190.
    3. Berndt, pp.190 & 193.
    4. Robotham 1970, pp. 160, 161, 183–185.
    5. Berndt, p.193.

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    References