Technology

TUPAN 1000
PROPULSION TF-300 / Turbofan

Tupan Propulsion TF-300 is a turbofan engine, composed by a fan-compressor rotor driven by a two-stages turbine, and a direct flux annular combustion chamber.

TECHNICAL SPECIFICATION

Fan – Axial Single stage

Compressor: Diagonal Single-stage

Combustors: Annular

Turbine: two-stages axial

Dimension

Length: 420 mm

Diameter: 250 mm

Dry weight: 16 kg

Performance

Thrust: 300lbf

SFC: 0,9 kg/Kgf/h 

TUPAN 2000
PROPULSION TF-700 / Turbofan

Tupan Propulsion TF-700 is a turbofan engine, composed by a fan-compressor rotor driven by a two-stages turbine, and a direct flux annular combustion chamber.

TECHNICAL SPECIFICATION

Fan – Axial Single stage

Compressor: One axial stage and one diagonal single-stage

Combustors: Annular

Turbine: two-stages axial

Dimension

Length: 580 mm

Diameter: 300 mm

Dry weight: 45 kg

Performance

Thrust: 700lbf

SFC: 0,85 kg/Kgf/h 

TUPAN 3000
PROPULSION TF-1200 / Turbofan

Tupan Propulsion TF-1200 is a turbofan engine, composed by a fan-compressor rotor driven by a two-stages turbine, and a direct flux annular combustion chamber.

TECHNICAL SPECIFICATION

Fan – Axial Single stage

Compressor: One axial stage and one diagonal single-stage

Combustors: Annular

Turbine: Two axial stages

Dimension

Length: 960 mm

Diameter: 350 mm

Dry weight: 86 kg

Performance

Thrust: 1200lbf

SFC: 0,8 kg/Kgf/h 

TUPAN 4G Simulation

The application of CFD to aircraft design configurations and its influence on the aircraft development and support process is analyzed.

Results indicate that combining CFD and the wind tunnel can achieve design solutions that otherwise would not be found, and can also significantly reduce the length of the design cycle.

It is concluded that CFD provides for a better understanding of flow physics, achievement of design solutions that are otherwise unobtainable, and reduction of development flowtime.