|
|
|
UL260I specs
|
Displacement |
: |
2592 cc [158.17 cu in] |
|
Bore |
: |
105.6 mm [4.157 in] |
|
Stroke |
: |
74 mm [2.913 in] |
|
Compression Ratio |
: |
8.16 : 1 |
|
Firing Order |
: |
1 - 3 - 2 - 4 |
|
Direction of Rotation |
: |
Clockwise - seen from cockpit |
|
Maximum Torque |
: |
207 Nm [152.7 ft.lb] @ 2500 rpm |
|
Power rating |
: |
95 hp @ 3300 rpm / 82 hp @ 2800 rpm |
|
All up dry weight |
: |
72.3 kg [159.3 lbs] (including all accessories such as electric fuel pump, filters, oil cooler, alternator and exhaust system) |
|
DC output |
: |
35 Amp (+/- 20 Amp available above engine/fuel pump needs) |
|
Oil capacity |
: |
2.5 L [0.66 US gal] |
|
Fuel |
: |
Regular unleaded automotive gasoline with min. 95 Octane RON (87 MON =
91 AKI) |
|
Maximum dimension in X direction (length)* |
: |
540 mm [21.3 inch] |
|
Maximum dimension in Y direction (width)* |
: |
654 mm [25.7 inch] |
|
Maximum dimension in Z direction (height)* |
: |
472 mm [18.6 inch] |
|
Distance from aircraft engine mount
frame to |
: |
455 mm [17.9 inch] |
|
* Subject to change during further development |
||
|
|
|
|
|
|
|
|
|
To view a
larger image of the engine against a 10x10mm [0.3937 in.] grid click on
an image above. |
||
|
Basic engine (incl. starter & alternator) |
: |
60.1 kg |
[132.5 lb] |
|
Ignition Coils & Leads |
: |
3.2 kg |
[7.0 lb] |
|
ECU & wiring loom |
: |
1.7 kg |
[3.7 lb] |
|
Exhaust, bolts, springs & seals |
: |
4.1 kg |
[9.0 lb] |
|
Electric Fuel Pump |
: |
0.8 kg |
[1.8 lb] |
|
Fuel Filters (pre-filter & fine filter) |
: |
0.2 kg |
[0.4 lb] |
|
Oil/Air Separator & hoses |
: |
0.8 kg |
[1.8 lb] |
|
Rectifier Regulator |
: |
0.1 kg |
[0.2 lb] |
|
Rubber Engine Mounts |
: |
0.3 kg |
[0.7 lb] |
|
Optional Oil Cooler |
: |
1.0 kg |
[2.2 lb] |
|
Engine Oil (2.5 litres) |
: |
2.2 kg |
[4.9 lb] |
|
TOTAL WEIGHT |
: |
74.5 kg |
[164.2 lb] |
Centre of
Gravity |
|
X-coordinate |
Y-coordinate |
Z-coordinate |
|
Basic engine including starter, alternator, rubber engine mounts, air
filter, |
+161 mm |
+3 mm |
-35 mm |
Click on a picture to
enlarge...
|
|
Y-coordinate* |
Z-coordinate* |
|
|
Point 1 |
125 mm [4.92 inch] |
95 mm [3.74 inch] |
|
|
Point 2 |
-125 mm [-4.92 inch] |
95mm [3.74 inch] |
|
|
Point 3 |
125 mm [4.92 inch] |
-165mm [-6.49 inch] |
|
|
Point 4 |
-125 mm [-4.92 inch] |
-165mm [-6.49 inch] |
|
>> Position of mounting points are identical to the Jabiru 2200 engine |
* Center of crankshaft is origin (0,0 coordinate) |
|
|
Direction of rotation : |
counter clockwise, looking towards face of flange |
|
Outer flange diam. : |
125mm |
|
|
P.C.D. 101.6mm [4 inch] : |
12 holes of 14mm dia. |
The power and torque curve of the engine has been established by repeated dyno tests on our second prototype, which were performed at sea level and in weather conditions close to the ISA standard. The following graph shows the real, available power and torque coming from the crankshaft of the UL260i engine corrected to the International Standard Atmosphere conditions at sea level.
A site by Terry Pappas
