Allison V-1710-121
to export the V-1710-F28R
sources:
www.unlimitedexcitement.com
http://www.lancastermuseum.ca/engine_allison.html
www.aviation-history.com
http://cs.wikipedia.org/wiki/Allison_V-1710
the archive of the author.
to export the V-1710-F28R
Manufacturer / Manufacturer: | Allison Engine Company |
Manufactured / Produced: | - |
Made / Number built: | - |
Arrangement of cylinders / Basic design: | inline dvanáctiválec with the cylinder to the In forming an 60° with reducer |
Chiller / Cooling: | a pressurized liquid 70% water and 30% etylenglykolu |
Swept volume / Capacity (dm3): | 28,031 |
Bore of cylinder / Bore (mm): | 139,7 |
Stroke / Stroke (mm): | 152,4 |
Compression ratio / Compression ratio: | 6,65 : 1 |
the Preparation of the fuel mixture / Carburation or injection: | Carburetor Bendix Stromberg PD-12K12 |
Valves / Valve Gear: | OHV, two intake and two exhaust for each cylinder |
Fuel / Fuel: | octane number / Octane No 100/130 |
cylinder Filling / Mixture charging: | turbo charged intercooled jednorychlostním compressor |
Length / Length (mm): | 2 502 |
Width /Width (mm): | 744 |
height / Height (mm): | 1 046 |
Mass / Weight (kg): | 705,3 |
Power / Ratings (horsepower / hp): | , p 1 425 hp at 3 000 rpm min the nominal 1 to 100 horses in the h= 8 534 m at 3 200 rpm./min the combat performance of the injection ADI 1 700 hp in h= 7 924 m at 3 200 rpm./min |
Note / Note: | - |
Usage: | Curtiss P-40Q Warhawk |
sources:
www.unlimitedexcitement.com
http://www.lancastermuseum.ca/engine_allison.html
www.aviation-history.com
http://cs.wikipedia.org/wiki/Allison_V-1710
the archive of the author.