Item 1610

DESIGN: AeroVantage ~ PropRotor - Disk - Rotor 1x2

Notes:

 

Specifications and Calculations - Hover:

 

 Hovering (ONLY):

Fore PropRotor:

Aft PropRotor:

Total, Ratio, Etc:

Notes:

 

PropRotor Radius.

5.5 ft.

4.375 ft.

 1.257:1

This ratio is fixed due to cruise.

 

Disk Area:

95.0 ft2

60.2 ft2

155.2 ft2

This ratio is fixed due to cruise.

 

Ratio of Disk Areas:

61.2%

38.8%

1.58:1

This ratio is fixed due to cruise.

 

Number of blades:

4

4

 

 

 

Airfoil:

VR-7

VR-7

 

 

 

Chord:

0.4 ft

0.4 ft

 

 

 

Taper:

0

0

 

 

 

Aspect Ratio:

11:1

10.9:1

 

 

 

Disk Loading:

9.0 lb/ ft2

7.8 lb/ ft2

 

 

 

Rotor Solidity Ratio:

0.0868

0.0873

 

 

 

Linear Twist:

-25º

-25º

 

 

 

Blade Cutout Ratio:

0.15

0.15

 

 

 

RRPM:

1,180

1,385

 

 

 

Tip Speed:

680 ft/sec

630 ft/sec

 

 

 

Tip Mach Nbr:

0.61

0.57

 

 

 

Gross Weight: (lb)

853

472

1325

Total is the fixed target.

 

Collective Pitch: (degree)

24.0

26.6

 

 

 

Thrust: (lb)

756

636

1,392

The fixed target is 1,325.

 

Length of Moment Arm: Item 1694

103.33"

110.26"

1:1.067

 

 

Moment: (lb-ft)

103 x 756 = 77,868

110 x 636=69,960

 

Must be equal.

 

Horsepower: BEMT

63

62

127 hp

Should be balanced.

 

Horsepower - Max available

62

62

124 hp

UniCopter's Lycoming

Balancing Longitudinal Moments of Fore and Aft PropRotors:

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

Last Revised: September 3, 2009