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The engine was fitted with a governor to allow the engine speed to be set somewhere between idling speed of 400 rpm and full power speed of 2,200 rpm, maintaining this speed against varying loads. The "belt hp" rating of the tractor was 23.9 hp although the tax rating of 20 hp gave the tractor its model number of TE20.
The larger displacement is achieved by increasing the stroke from 78 to 87 mm (3.1 to 3.4 in), but using the same bore of 86 mm (3.4 in). In aviation applications it is used as a direct drive engine, turning a propeller without a reduction drive. It employs a single electronic ignition system and produces 25 to 37 hp (19 to 28 kW) at 3600 rpm.
A higher power 7-HP model was made (Engine Model# 84330) for use in heavier duty machines such as the single stage Snow Commander (2001–2008) and 2 stage Power Max 726TE/6000 (2004–2008); the extra horsepower was obtained using transfer ports in the piston and cylinder wall, and this model ran at the same operating speed as the 6.5 hp ...
Argus As VI 700 hp V-12 [35] Argus As VIA [35] Argus As 7 9R 700 hp [37] Argus As 8 4-cylinder inverted inline [37] Argus As 10 8-cylinder inverted V [37] Argus As 12 16H 550 hp [37] Argus As 16 4-cylinder horizontally-opposed 35 hp [39] Argus As 17; Argus As 014 (aka "Argus 109-014") – pulse jet engine for V-1 flying bomb and Tornado boat ...
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The Phase II Vanguard was powered, like the Phase I, by a 2088 cc 4-cylinder "wet sleeve" engine, now with a modestly increased compression ratio, and producing 68 hp. This engine could be modified by using an additional intake system and two single-barrel Solex carburettors, producing 90 hp. Typically, the Phase II engine was one Solex ...
It was fitted with the same 2088 cc four-cylinder engine as used in the saloon. [35] Utility versions of the Vanguard were produced in Australia over the following years, [36] with production ending in 1964. [37] The Vanguard Utility was sold in the UK as a pickup truck. The main purchaser was the Royal Air Force, which had them in Phase I and ...
Even before the channel flight, Anzani was selling more powerful versions with larger bores: [7] a 120 mm bore, 4.4-litre (269 cu in) variant produced 26 kW (35 hp) and a 135 mm bore, 6.4-litre (390 cu in) engine gave 36 kW (45 hp). These fan engines remained in production until at least 1913, [8] though there were important improvements. The ...