ATDI- 45
Give your next program the powerhouse it deserves with a ATDI
Turbine
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The ATDI-35 which was
originally developed for use in medium to large scale UAV
applications
has since been redesigned to produce 45 pounds of thrust as compared to
the original 35 pounds of thrust. The new ATDI-45
turbo jet contains a new highly efficient compressor
and redesigned diffuser, along with a re-matched turbine to increase
overall performance and efficiency. ATDI’s team properly designs engine cycles for each engine,
drawing on extensive experience with military and aerospace projects.
ATDI Turbines 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 Turbines engine to provide the kind of reliability,
power, and fuel efficiency that any customer would expect.
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ATDI - 45 Specifications
| Specifications: | ATDI 45 | | Diameter: | 5.3 | | Length: | 11.925 | | Weight: | 7.5 | | Compressor: | | | Air Flow lbs: | 0.66 | | Efficiency : | 71.5 | | Pressure Ratio: | 3 | | Combustor: | | | Loading: | 11800000 | | Pressure Drop: | 6 | | Combustor Efficiency: | 99 | | Inlet Temp: | 1694 | | Turbine: | | | Turbine Efficiency : | 77 | | Turbine Pressure Ratio: | 1.84 | | Exhaust Gas Temp: | 1461 | | Turbine Nozzle: | | | Nozzle Pressure Ratio: | 1.532 | | Engine Performance: | | | Design RPM: | 120000 | | Fuel Flow: | 49.3 | | Exhaust Jet Velocity: | 1632 | | Thrust: | 45.3 | | SFC: | 1.473 |
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(Note) This engine is no longer available it shows the
progress of our engines to where they are today.
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