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![]() Morgans wrote: "bbutlergps" wrote The Mercedes-Benz A Class 1.7 from Thielert Centurion even being light alloy weighs in at just under 300 lbs. Too much for the 701. Being that the smaller mercedes 3 cylinder diesel has been put in some planes including the 701, 601 FK-9 as well as ultra lights but I feel that they lack the HP needed. Keep in mind that the diesel engines in airplanes tend to give the same performance as a gas engine of up to 25% more HP. Would that make a difference in the HP figures, in your case? -- Jim in NC Still haven't gotten any information on the Smart Mercedes 3 cyl. 95 hp diesel found in the Smart ForFour of the Mitisibishi Colt such as weight. I did however come across VW Lupo engine. This 1.2 engine is found in Audi A2 and VW Lupo. It is all aluminum. Diesel engines Three cylinder 3L 1.2 TDI This inline three cylinder is notorious for being the powerplant of the Lupo 3L and A2 3L, both VAG cars with a low consumption of only three liters per hundred kilometers (94 mpg/78 US mpg). It is based on the 1.4 TDI version but the block is made of aluminium and the elements are lighter. Configuration Diesel 1191 cc inline three cylinder Block bore × stroke 76.5 × 86.4 mm, aluminum Head aluminum, 2 valves, overhead camshaft, 19.5 compression ratio Aspiration turbocharger Fuel Pump direct injection (PD Pump injector, Pumpe-Düse) Dimensions 100 kg Output 45 kW (61 hp) @ 4000 rpm, 140 N·m between 1800 and 2400 rpm, 80% available from 1300 rpm Applications Audi A2, VW Lupo 3L references Audi AG (1999-11-28). Audi A2 1.2 TDI: The three-litre car from Audi. Press release. This engine can be chipped up to 75 hp. I know, don't believe the chip turners, figure in cooling, PSRU, etc weight while and there is other powerplants out there. But I am in for discussion of LSA diesel power aircraft that the power plant doesn't cost more than the aircraft. Thanks, Bill |
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![]() "bbutlergps" wrote in message ps.com... Morgans wrote: "bbutlergps" wrote The Mercedes-Benz A Class 1.7 from Thielert Centurion even being light alloy weighs in at just under 300 lbs. Too much for the 701. Being that the smaller mercedes 3 cylinder diesel has been put in some planes including the 701, 601 FK-9 as well as ultra lights but I feel that they lack the HP needed. Keep in mind that the diesel engines in airplanes tend to give the same performance as a gas engine of up to 25% more HP. Would that make a difference in the HP figures, in your case? -- Jim in NC Still haven't gotten any information on the Smart Mercedes 3 cyl. 95 hp diesel found in the Smart ForFour of the Mitisibishi Colt such as weight. I did however come across VW Lupo engine. This 1.2 engine is found in Audi A2 and VW Lupo. It is all aluminum. Diesel engines Three cylinder 3L 1.2 TDI This inline three cylinder is notorious for being the powerplant of the Lupo 3L and A2 3L, both VAG cars with a low consumption of only three liters per hundred kilometers (94 mpg/78 US mpg). It is based on the 1.4 TDI version but the block is made of aluminium and the elements are lighter. Configuration Diesel 1191 cc inline three cylinder Block bore × stroke 76.5 × 86.4 mm, aluminum Head aluminum, 2 valves, overhead camshaft, 19.5 compression ratio Aspiration turbocharger Fuel Pump direct injection (PD Pump injector, Pumpe-Düse) Dimensions 100 kg Output 45 kW (61 hp) @ 4000 rpm, 140 N·m between 1800 and 2400 rpm, 80% available from 1300 rpm Applications Audi A2, VW Lupo 3L references Audi AG (1999-11-28). Audi A2 1.2 TDI: The three-litre car from Audi. Press release. This engine can be chipped up to 75 hp. I know, don't believe the chip turners, figure in cooling, PSRU, etc weight while and there is other powerplants out there. But I am in for discussion of LSA diesel power aircraft that the power plant doesn't cost more than the aircraft. Thanks, Bill My own concern with reprogrammed chips is not so much whether the results are credible, although that is certainly an issue, but the possible effect on reliability. I would expect engine manufacturers program their engine controls based a compromise between the performance they can demonstrate and the costs of reliability problems and attendant warranty costs. Therefore, I am less than enthusiastic about the idea of "souping up" an engine for use in an aircraft--especially single engine. Peter I've been wrong before... |
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