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Turboprop engine TP100 and Turboshaft engine TS100

Time:2012-11-05 10:08Turbochargers information Click:

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Contact

Bohumil Antoš
Sales Manager

Phone: +420 566 822 304

 

Fax: +420 566 822 372

 

E-mail: sales@pbsvb.cz

 

Turboprop engine TP 100 and Turboshaft engine TS 100 Turboprop engine TP 100

PBS turboprop engine TP 100 on the test ramp, ready for testing

PBS turboprop engine TP 100

 


Newly developed turboprop engine TP 100 of the output of 180 kW. The basis of TP 100 is the proven engine TJ 100, which fulfils here the function of the gas generator, drives the free turbine and, via a gearbox, a three-bladed propeller with constant speed. The system is designed for use in both push and tractor configuration depending on its mounting on the air vehicle. Thanks to its low weight and output of 185 kW this engine is intended for the category of ultralight both piloted and pilotless air vehicles (UAV).

Engine availability

The engine is in the prototype test stage; the first series will be available by the end of 2012.

Turboshaft engine TS 100

PBS turboshaft engine TS 100 – prototype drawing, view of the gas generator

PBS turboshaft engine TS 100 - prototype drawing, shaft outlet

 


Turboshaft engine TS 100 is only a modified variant of the turboprop engine TP 100. The gearbox is modified for the operation with propeller blades. The engine is suitable as a driving unit of the ultralight helicopter.

Engine availability

The engine is in the development stage; the first series will be available after the launch of the TP 100 engine on the market, i.e. by the end of 2012.

Technical data

TP / TS 100

Main advantage of these engines are small buildup dimensions, low weight and high static thrust.

Engine parameters

  h = 0 m, v0 = 0 km/h h = 3000 m, v = 350 km/h

Output shaft power 180 kW 140 kW

Thrust with propeller AV723 5394 N 1357 N

Residual thrust 259 N 74 N

  TP 100 TS 100

Propeller speed 2158 ot/min (rpm) 6000 ot/min (rpm)

Other parameters

Weight (dry) 55 kg

Engine length 870 mm 843 mm

Width x Depth (without exhaust) 330 x 382 mm 390 x 330 mm

Reducer speed ratio 20.751 : 1

Fuel JET A, A1, B, TS-1, T2, RT

Oil MIL-L-23699

Engine ceiling of operation 9000 m 6000 m

Engine ceiling for starting 6000 m 4000 m


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