ATDI- 65
Give your next program the powerhouse it deserves with a ATDI
Turbine
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The ATDI - 65 lb thrust Turbo jet Engine featuring a newly
developed brushless electric starter and a 1kw PMG Generator. This engine
is the result of a joint effort with Advance Turbine Design and
Orbital Machine
Works, although designed for use as a Glider sustainer propulsion system, this
engine would be suitable for many other applications such as propulsion systems
for UAV's, Experimental aircraft, the engine core could also be developed into a
Ground power generation unit up to 50kw. This technology has been
previously demonstrated at Advance Turbine Design. With it's robust construction
and the latest state of the art micro turbine technology and hundreds of hours
of both ground and flight testing this turbo jet is a proven performer.
ATDI's team properly designs engine cycles for each engine, drawing on extensive
experience with military and aerospace projects. ATDI has teamed with the
Aviation Applied Technology Directorate of the US Army, NASA, Hamilton
Sundstrand, and others in their years in the industry. The advanced engine
designs offered by ATDI Turbines reflect the high performance and high
efficiency expectations associated with these customers. ATDI completes a
rigorous design process, including combustor and fuel injector analysis,
advanced diffuser aerodynamic design, and in-depth thermodynamic cycle analyses,
driving the engineering of every ATDI Turbine engine to provide the kind of
reliability, power, and fuel efficiency that any customer would expect.
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ATDI - 65 Specifications
| Model: | ATDI -65 | | Diameter: | 6.50 | | Length: | 16" | | Weight: | 16 | | Compressor: | | | Air Flow lbs: | 1.73 | | Efficiency: | 0.73 | | Pressure Ratio: | 3.6 | | Combustor: | | | Loading: | 18700 | | Pressure Drop: | 5.4 | | Combustor Efficiency: | 0.98 | | Inlet Temp: | 1835 | | Turbine: | | | Turbine Efficiency: | 0.77 | | Turbine Pressure Ratio: | 1.84 | | Exhaust Gas Temp: | 900 | | Turbine Nozzle: | | | Nozzle Pressure Ratio: | 1.85 | | Engine Performance: | | | Design RPM: | 70000 | | Fuel Flow: | 11.5 | | Exhaust Jet Velocity: | 1989 | | Thrust: | 65 | | SFC: | 1.30 |
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Email us for current price and availability
advanceturbinedesign@advtdinc.com
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