JPE 04 H Hybryd

Informazioni Generali

Fuel Diesel fuel/jp4/jetA1
Engine type 4 in line –  turbo diesel common rail engine
Bore mm 82
Stroke mm 90.4
Cubic capacity 1910 cc
Peak chamber pressure 180 bar
Power output (EEC)

Hybrid Kw 230 ( 300 Hp )@ 4300 rpm for 30’’

            Kw 192 ( 250 Hp )@3700 rpm for 3 Min

            Variable from 155 up to 230 Kw 10 Min

154 Kw (200HP)@4.300 rpm (crankshaft)

130 Kw (180HP)@3700 rpm (crankshaft) continuous power

BestSFC @max power output 150 gr/HPh (203gr/kWh) from 5% to 95% power output
BestSFC @max power output 160 gr/HPh (218 gr/kWh) from 95% to 100% power output
Idle speed rpm 1000
Max. engine speed rpm 4500

Dimensioni

Lunghezza mm 871
Larghezza mm 560
Altezza mm 698

Pesi

a secco con alternatore standard 12V/8A Kg 180
Pronto al volo con alternatore, riduttore,starter, etc Kg 195

Ulteriori informazioni

Timing system Single level FADEC with Engine parameters Monitorcapability, UAV1553B Bus communication system, capability for compliances with DO178-B
Cooling 70% in weight Ethylene Glycol – 30% Water (kg 1.2 inside the engine)
Mechanical water pump
Maximum pressure allowed 1.5 bar
Max allowable temperature 115°C
Oil lubrication and cooling Internal heat exchanger.1 mechanically geared.
Maximum pressure allowed 6 bar.
Maximum allowable oil consumption 1kg every 25h.
Maximum allowable temperature 130°C
Oil type and quantity SAE 5W30 synthetic oil API SL/CF ACEA A3/B3/B4 Mercedes Benz 229.3, 4.5 kg
Oil filter Internal cartridge type
PRSU (Prop. Red. Speed Unit) /
Temperature range +/- 55 deg C
Fuel injection -50°C/+55°C ISACRDI System FADEC controlled
Engine mounts Rubber shock mounts required.
Service angles Rubber shock mounts required.Bank: 60°.Pitch: +45°/-45°
G loads +7 / – 2
TBO According to FAA 1.1 and 23.3 aerobatic category.Inverted flight allowed only with special kit.2,000h for standard use.

Comparazione Propulsori

FUEL USED MTOP/FF MCP/FF ECONOMY/FF WEIGHT TBO
LYNCOMING 0-540 A Fuel grade,
octane 80/87
192 Kw (250 hp)
20,5 gal/h (77 l/h)
176 Kw 230 hp)
16,5 gal/h (62 l/h)
146 Kw (190 hp)
15 gal/h (56 l/h)
185 Kg
(405 Lbs)
2000
LYNCOMING 0-5450 S Fuel grade,
octane 80/87
230 Kw (300 hp)
24 gal/h (90 l/h)
190 Kw (250 hp)
21 gal/h (79 l/h)
173 Kw (225 hp)
16 gal/h (60 l/h)
213 Kg
(475 Lbs)
1800
Continental TSIO-550 Fuel grade,
octane 80/87
230 Kw (300 hp)
24 gal/h (90 l/h)
N.A. N.A. 226 Kg
(497 Lbs)
N.A.
Safram SR305 Diesel (EN 590),
Jet A, Jet A-1
174 Kw (227 hp)
10,6 gal/h (38 l/h)
150 Kw (195 hp)
8 gal/h (30 l/h)
125 Kw (162 hp)
6,5 gal/h (25 l/h)
205 Kg
(455 Lbs)
2400
P2M JPE03 Diesel (EN 590),
Jet A, Jet A-1
190 Kw (247 hp)
10 gal/h (38 l/h)
170 Kw (221 hp)
9 gal/h (34 l/h)
154 Kw (200 hp)
8,2 gal/h (31 l/h)
160 Kg
(353 Lbs)
2000
P2M JPE H 04 Diesel (EN 590),
Jet A, Jet A-1
239 Kw (312 hp)
10 gal/h (38 l/h)
170 Kw (221 hp)
9 gal/h (34 l/h)
154 Kw (200 hp)
8,2 gal/h (31 l/h)
180 Kg
(397 Lbs)
2000

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