A 002

DESIGN: SynchroLite ~ Weight & Balance

Outside Helicopter

Comparison of Ultrasport 254 Actual and Previous 254# Ultralight SynchroLite Allocated

 

Primary Group

Ultrasport Achieved

SynchroLite Allocated

Difference

 

Power Train - Assembly - Final

39.93

 82.00

 

 

Fuselage - Assembly - Final

49.63

25.00

 

 

Landing Gear

16.43

6.00

 

 

Tail Rotor

1.68

0.00

 

 

Rotor - Assembly - Final

45.13

42.00

 

 

Control - Flight - Assembly - Final

11.85

 14.00

 

 

Engine & Exhaust & Tank

81.26

72.00

 

 

Miscellaneous

8.05

12.00

 

 

Total

253.96

253.00

 

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.

Mosquito:

Assuming a slope of 15 degrees for the seat back, the pilot's center of mass will be about 10" in front of the back of his head. If the mast has a 2" diameter then the pilot's center of mass is 11" in front of the mast.

SynchroLite

Datum:

Origin (0,0,0) is the point where the centerline of the 2 masts would meet if extended downward below the gearbox. I.e. the base of the V. 

Axes for Weight and Balance:

Note: The positive and negatives shown below are for weight and balance only. The signs are reversed when considering the helicopters axes system(s).

X-axis is for-aft (station). Positive is aft.

Y-axis is side-side (buttock). Positive is to port.

Z-axis is height (elevation). Positive is up.

 

Forces & Distances:

Moments & Rotation:

Location of Center of Weight & Center of Area:

At present, it is assumed that the center of the surface area weight coincides with the center of weight.

Is the Center of Area the Aerodynamic center?  Not on an airfoil.

Weight & Balance

Look in book "Aircraft Inspection and Repair], chapter 13. 

Rotation (Yaw) about Vertical Axis Caused by Air Flow

In a side wind it will probably be best to have the center of rotation at the mast (datum 0). This way the side wind will not want to rotate the craft and all yaw control input can be used to rotate the craft and not fight the side wind. 

In forward flight it will probably be best to have the center of rotation behind the mast. This way the horizontal air will help in keeping the craft on course. 

It would appear that the best location would be a compromise, where the center of rotation is located slightly behind the mast. Say 12"  

Center of Gravity re: Lightweight Pilot

A heavier person will move the center of gravity forward because this person will have greater depth at chest. longer legs and will weigh more. For a lighter pilot consider:-

1. Put a cushion behind pilot to move his center of weight slightly forward. Consider the relocation of pedals also.

2. Add weight to the front end of forward support tube, by the pedals. Assuming that the pedals are movable, this weight could be attached through the forward foot pedal crossbar hole, which is used by tall heavy pilots.

3. Move battery from extreme tail to extreme nose? The battery cable would be a permanent fixture running the full length of the spar and have connectors at both ends.

4. Re: Pilots of different weights: Normally the heavier pilots will be taller. Consider having an adjustable seat instead of the pedals. This will allow the balance arm length to increase as the balance weight decreases. The seat should move down slightly as it moves ahead (in-line with the tail tube?) so that the shorter person's ankle has the same angle with the pedals as the tall person. A problem with this is that the seat may no longer be a part of the structure.

Idea re drawing

There could be a drawing done for 0472. It would consist of an outline of the 3 views of the synchropter and on another layer a grid would be drawn based on the centerlines, and on another layer there would be 3 lines showing the centers of mass. 

____________________

February 4, 2005 re: Center of Gravity

It looks now that the center of gravity is too far aft. If so, this could be corrected by;

1/ Make the distance between fuselage and power train origins 1/2 to 2" more. This would allow the seat back slope to get back to around 15 degrees. This 15 degrees will be better for forward flight when the helicopter is nose down.

Empty Weight / Total Load:

The trend is toward 50/50. The SynchroLite is beyond that at 46/54. The lack of tail rotor losses will help a little but my calculations may be a little over optimistic.

Same Page ~ Different Craft: ~ Dragonfly ~ UniCopter

Introduction Page | SynchroLite Home Page | Electrotor Home Page | UniCopter Home Page | Nemesis Home Page | AeroVantage

Last Revised: February 4, 2005