Item 1489

DESIGN: Single-Bladed All Electric Rotor - Disk - Forces & Moments

Objective:

To determine the forces and moments at work on the rotor.

Reference: DESIGN: SynchroLite ~ Rotor - Disk - Centers, Radii & Moments

Symbols:

 

Symbol:

Name:

Definition:

Units:

 

T

Thrust

Thrust

pounds

 

L

Lift

Vertical component of Thrust

pounds

 

P

Pull

Horizontal component of Thrust

pounds

 

CF

Centrifugal Force

 

 

 

C

Centroid

Center of mass

 

 

M

Moment

 

 

 

D

Drag

 

pounds

 

CM

Moment of centrifugal force

Restoring moment of centrifugal force

 

 

WA

Weight Arm

Moment arm from teetering hinge to centroid

feet

 

TA

Thrust Arm

Moment arm from teetering hinge to ctr. of lift

feet

 

W

Weight

 

pounds

 

GW

Gross Weight

Gross weight of craft

pounds

 

RRPM

Rotor speed

 

rpm

 

Ω

Rotor speed

 

radians

 

B

Teeter angle

 

degrees

 

R

Restoring force

The restoring force of the centrifugal force

lb-ft

 

 

 

 

 

 

Subscripts:

 

Designated on drawing by preceding dash

 

 

b

Blade

 

 

 

cw

Counter Weight

 

 

 

hov

Hover

 

 

 

max

Maximum teeter

 

 

 

min

Minimum teeter

 

 

 

f

Fuselage

Gross weight less weight of rotors

 

 

t

Total

 

 

 

h

Hub

Hub excluding blades

 

 

ind

Induced - (drag & thrust)

 

 

 

pro

Profile (drag)

 

 

 

 

 

 

 

Thrust and Centrifugal Force: The 2-blade rotor is only for temporary reference and CF forces in the second and third drawings must be changed.

Algorithms and Calculations: The following is just approximations, at present, to get a feel for the requirements.

 

W b

10 lbs.

Value from ~ SynchroLite 3-rotor is 21# for 550 GW

 

W cw

20 lbs.

Arbitrarily set at half that of the blade's arm.

 

WA b

4.5 ft.

Tapered blade with 10 foot radius

 

WA cw

2.25 ft.

(10 lbs / 20 lbs ) * 4.5 ft.

 

Item:

Value:

Notes:

 

GW

550 lbs.

254# craft + 296# load

 

CF b

5,731 pounds

Centrifugal force of blade

 

CF cw

5,731 pounds

Centrifugal force of counterweight

 

β hov

2.5º

Tan(A) = a/b = 550/(6368 + 6368) Angle = 2.5º

 

T hov

551 lbs.

c = b/ cos(A) = 550/cos(2.5) = 551 lbs

 

P hov

24 lbs.

a = tan(A) * b = 0.0437 * 550 = 24 lbs

 

β max

14.5º

Maximum Teetering angle = 2.5º + 12º = 14.5º

 

T max

568 lbs.

c = b/ cos(A) = 550/cos1(4.5) = 568 lbs

 

P max

24 lbs.

a = tan(A) * b = 0.2586 * 550 = 142 lbs

 

β min

-9.5º

Minimum Teetering angle = 2.5º - 12º = -9.5º

 

T min

568 lbs.

c = b/ cos(A) = 550/cos(-10.5) = 559 lbs

 

P min

24 lbs.

a = tan(A) * b = -0.1853 * 550 = -102 lbs

 

Drag and Centrifugal Force:

Related Pages:

Back to top | SBAEC Home Page | SynchroLite Home Page | UniCopter Home Page | Dragonfly Home Page

Initially displayed: January 9, 2006 ~ Posted on PPRuNe; January 11, 2006; on Rotary Wing Forum; January 9, 2006~ Last Revised: Friday, February 3, 2006

The above utility invention is openly and publicly disclosed on the Internet to negate an entity from patenting it, to the exclusion of all others whom may wish to use it. ~ Reference patent law 35 U.S.C. 102 A person shall be entitled to a patent unless - (a) the invention was known ... by others in this country, ..., before the invention thereof by the applicant for patent.