BO-105 engine RPM
Hi All,
can someone tell me what is the design RPM of Bo-105 engines? The information I found are contradicting. Somewhere I read 6600 RPM. On the other hand, somewhere else I found that BO-105 tail rotor rotates with 2220 RPM and has gear ratio 5.24. This makes 11630 RPM at engine shaft. thanks in advance |
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As per the flight manual of the BO105CB-5, you have
At 100% N2, the engine shaft is rotating at 6,000 RPM. The main rotor rotates at 424 RPM. The tail rotor shaft coming out of the main gear box rotates at 2,452 RPM. After the intermediate gearbox, the tail rotor shaft rotates at 3,065 RPM and finally after the tail rotor gearbox, the final rotation speed is 2,219 RPM. You 5.24 ratio is between the main rotor speed and the final tail rotor speed (2219/424=5.233). Hope this helps. Cheers |
BO-105 engine RPM
turboshaft, ECL_FTE thank you both for the answers.
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Nickel,
The 6,000 rpm fiqure is the output shaft speed from the engine reduction gearbox, the compressor actually runs at about 52,000 rpm and the power turbine at 35,000 rpm.:8 |
the compressor actually runs at about 52,000 rpm and the power turbine at 35,000 rpm.http://images.ibsrv.net/ibsrv/res/sr...ilies/nerd.gif |
Um... Lifting... that is one of the most clear and concise explanations of the free-turbine engine that I've ever read. Nice job!
One slight expansion though... In a turbofan, some of that thrust is used directly and the rest drives the fan... |
Originally Posted by Um... lifting...
Two turbines in a turboshaft
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