A 092
DESIGN: Dragonfly ~
Weight & BalanceBased on the complete helicopter
Dragonfly General Arraignment #1![]()
Outside Helicopters
Robinson R22:
Ultrasport 254 Center of Gravity Limits:
The center of gravity on the Ultrasport 254 must be between 4.5" and 1.5" in front of the mast.
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Dragonfly Power Train & Rotor / SynchroLite Fuselage
Rough Comparison of Weights:
|
|
Primary Group |
Ultrasport 254 Achieved |
SynchroLite Allocated |
Dragonfly Allocated |
|
|
Power Train / Rotor / Flight Control |
|
|
|
|
|
Power Train / Rotor Hub / Flight Control Assy |
~ |
~ |
100.00 (1) |
|
|
Power Train - Assembly - Final |
39.93 |
82.00 |
~ |
|
|
Rotor - Assembly - Final |
45.13 |
42.00 |
~ |
|
|
Rotor - Blade - Assembly |
~ |
~ |
28.00 (2) |
|
|
Fuselage / Engine |
|
|
|
|
|
Fuselage - Assembly - Final |
49.63 |
25.00 |
30.00 |
|
|
Landing Gear |
16.43 |
6.00 |
6.00 |
|
|
Tail Rotor |
1.68 |
0.00 |
0.00 |
|
|
Control - Flight - Assembly - Final |
11.85 |
14.00 |
6.00 (3) |
|
|
Engine & Exhaust & Tank |
81.26 |
72.00 |
70.00 (4) |
|
|
Miscellaneous |
8.05 |
12.00 |
13.00 |
|
|
Total |
253.96 |
253.00 |
253.00 |
Datum:
Origin (0,0,0) is the point midway between the centers of the two rotor hubs.
The reference point of the fuselage is the hole in the center back of the seat. This hole is 6.5" ahead of the Origin.
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Weight and Balance:
|
|
Full Name: |
BOM |
Wt. Ea. |
Qty. |
Length of Arm (in) |
Moment (lb-in) |
||||
|
|
|
|
(lbs.) |
|
X |
Y |
Z |
X |
Y |
Z |
|
|
Power Train / Rotor / Flight Control |
|
|
|
|
|
|
|
|
|
|
|
Power Train - Assembly - Final |
55 |
1 |
2 |
0 |
8 |
110 |
0 |
440 |
|
|
|
Rotor - Hub - Assembly |
18 |
2 |
x |
x |
x |
x |
0 |
0 |
|
|
|
Rotor - Blade - Composite VR-7 -Assy |
4.67 |
6 |
0 |
0 |
0 |
0 |
0 |
0 |
|
|
|
Control - Flight - Assembly - Final (1) |
6 |
1 |
0 |
0 |
24 |
0 |
0 |
120 |
|
|
|
Fuselage / Engine |
|
|
|
|
|
|
|
|
|
|
|
Fuselage - Assembly - Final |
30 |
1 |
18 |
0 |
30 |
540 |
0 |
900 |
|
|
|
Landing Gear - Rear - Composite Legs |
3 |
2 |
13 |
0 |
72 |
39 |
0 |
216 |
|
|
|
Control - Flight - Assembly - Final (1) |
8 |
1 |
-12 |
0 |
24 |
-96 |
0 |
144 |
|
|
|
Control - Power Train - Assembly - Final |
8 |
1 |
7 |
0 |
24 |
56 |
0 |
192 |
|
|
|
Instrument - Assembly - Final |
5 |
1 |
-34 |
0 |
36 |
-170 |
0 |
180 |
|
|
|
Electrical - Assembly - Final (5) |
0 |
0 |
0 |
0 |
24 |
0 |
0 |
0 |
|
|
|
Engine - Assembly - Final (2) put in assy page |
62 |
1 |
15 |
0 |
xx |
930 |
0 |
xx |
|
|
|
Engine - Assembly - Final (3) put in assy page |
0580 |
23 |
2 |
15 |
0 |
xx |
690 |
0 |
xx |
|
|
Exhaust - Assembly - Final |
8 |
1 |
12 |
0 |
24 |
96 |
0 |
192 |
|
|
|
Fuel - Assembly - Final |
6 |
1 |
2 |
0 |
42 |
12 |
0 |
252 |
|
|
|
Empty Weight: |
|
254 |
(4) |
Empty Moment: |
1445 |
0 |
xx |
||
|
|
Weight & Balance - Load - Baggage |
|
34 |
1 |
0 |
0 |
60 |
0 |
0 |
600 |
|
|
Weight & Balance - Load - Fuel |
|
30 |
1 |
-3 |
0 |
48 |
-90 |
0 |
1440 |
|
|
Weight & Balance - Load - Oil - in Power |
|
2 |
2 |
0 |
0 |
5 |
0 |
0 |
10 |
|
|
Weight & Balance - Load - Pilot |
|
230 |
1 |
-16 |
0 |
40 |
-3680 |
0 |
9200 |
|
|
Load: |
|
296 |
|
Load Moment: |
-3770 |
0 |
xx |
||
|
|
Total Weight: |
|
550 |
(4) |
Total Moment: |
-2265 |
0 |
xx |
||
|
|
|
|
|
CofG from Origins: |
-4.1" |
0" |
xx" |
|||
|
|
|
|
|
Symbol: |
xCG |
yCG |
zCG |
|||
Red BOMs are those for SynchroLite, and will be replaced.
Dimensions are in inches and weights are in pounds.
Total weight is item quantity times item weight.
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Last Revised: November 22, 2003