Mikron III JCV−360 Alfa T−422 ENGINES

ENGINES
Mikron III
The Mikron III is an inverted in−line
four−cylinder four−stroke, OHV petrol aero
engine, with a downdraught carburettor.
It is produced in several versions − for
lightplanes (A, AE, B ) and for ultralights
(AUL, BUL).
Left−hand turning,
cylinder bore 90 mm,
piston stroke 90 mm,
total swept volume 2,44 litre,
weight 69 kg (depending on version),
take−off power 55 kW (75 HP)
at 2 760 r.p.m.,
max. continuous power 51 kW
(69 HP) at 2 600 r.p.m.
Parma − Technik, s.r.o.
Uherskobrodská 962,
763 26 Luhačovice, Czech Republic
e−mail: [email protected]
e−mail: [email protected]
JCV−360
A brand−new twin−cylinder water−cooled
four−stroke petrol aero engine. Four
valves per cylinder. The engine
is slated to power paraglider trikes,
ultralight single−seaters and for other
applications
Length 58 cm,
width 34 cm,
height 36 cm,
weight 26 kg,
Operational r.p.m. 5500 − 6500,
power output 28 kW / 38 HP.
Verner Motor
Vikýřovice 562,
788 13 Šumperk,
Czech Republic
www. vernermotor.com
e−mail: [email protected]
Alfa T−422
This horizontally−opposed four−cylinder
aircooled fuel−injected single−OHC
direct−drive engine uses an electronic ignition and injection control unit by Ignitech.
Swept volume 2 183 cm3 ,
bore 95 mm, stroke 77 mm,
compression ratio 1:9,3,
max. take−off power 63 kW /85 HP)
at 2900 rpm,
dry weight
74 kg,
equipped weight
81 kg,
max. permitted rpm
3 600,
time to major overhaul
2 500 h.
Trefil Engine, s.r.o.
Suterova 2013,
709 00 Ostrava − M. Hory,
Czech Republic
www.trefil.net
e−mail: trefil@trefil−engine.cz
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CZECH AVIATION 2011
TJ 100
The TJ−100A engine is noteworthy by its
compact design, excellent thrust/weight
ratio and low fuel consumption for its
power category. The conception of this
engine is classical − with radial compressor and annual combustion chamber,
axial turbine and a fixed exhaust nozzle.
Max.diameter 272 mm,
length 625 mm,
dry weight (with accessories) 20,6 kg,
max. thrust 1 250 N,
min. specific fuel consumption
1.09 kg/DaN/h.
PBS Velká Bíteš, a.s.
Vlkovská 279,
595 12 Velká Bíteš,
Czech Republic
www.pbsvb.cz
e−mail: [email protected]
TP 100
The První brněnská strojírna Velká Bíteš,
a.s. began tests of a demonstrator turboprop engine, the TP−100, developed
from the TJ−100 jet. In the new guise the
jet engine serves as a gas generator,
feeding the free turbine. The latter drives
through a reduction gearbox a tractor or
a pusher three−bladed constant−speed
propeller.
Dimensions 330 x 382 x 870 mm,
weight 55 kg,
shaft output 180 kW (H=0 m, 0 km/h),
thust with Avia 723 propeller 5 394 N,
exhaust thrust 259 N,
propeller r.p.m. 2 158.
PBS Velká Bíteš, a.s.
Vlkovská 279, 595 12 Velká Bíteš,
Czech Republic
www.pbsvb.cz
e−mail: [email protected]
F200
The lateast model of this engine is a result
of 6 years of continous development and
testing. It is a powerful air cooled two
stroke engine with high reliability, specially
designed for paramotors and small, light
powered paraglider trikes.
Volume
Power
Max. rpm
Bore
Stroke
Reduction
Weight complet
Starter
200cc.
27 hp
7900
66 mm
56 mm
2,5/3,1
14 kg
electric
Fly Engine
Viktor Procházka
Tatiná 32, 330 11 p. Třemošná
Czech Republic
www.flyengines.com
[email protected]
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