Item 0865

DESIGN: UniCopter ~ Rotor - Hub - ARR- Bearing - Mast

See: OTHER: Mechanics - Bearing - Cylindrical Roller ??

 

Loading:

Due to Blade:

The normal (base) load will be during hover at gross weight. This load on the mast bearing will only be axial during hover since the centrifugal forces of all the blades will self cancel. The axial force on the mast bearing will have a value of only ((GW / 2) * secant(VM)) = 600 pounds, approximately. A vertical climb will not increase the loading much but maneuvers (cyclic activity) and perturbations (gusts) will greatly increase the loading.

Force and Moment from One Blade:

From: DESIGN: UniCopter ~ Rotor - Disk - Blade Generated Forces Currently 4-blade rotor only.

WAS from: DESIGN: UniCopter ~ Rotor - Blade - Composite - VR-7mod - Planform, Profile and Lift [OLD] ~ Blade Loading.

Thrust Force ~ Radial Load on One Blade: Copied from 0859

Operating: 6,735 in-lbs. @ 1G: From page: DESIGN: Rotor - Blade - Composite - VR-7mod - Planform for ARR (2)

Ultimate thrust: 8,221 x (4 [LLF] x 1.5 [SF] = 49,326 lb. (219,413 N)

 Due to Gears:

Probably not much compared to the above.

Crude Rough Calculation of Moment:

Re LAYOUT Item 0996:

The distance from the centerline of one bearing across the mast's centerline to the centerline of the other bearing is 7.0372".

The moment on one blade is 8,421 in-lbs from the center of the mast. (from 0850)

(4.0 [LLF - limit load factor] x 1.5 [SF - safety factor]) = 6 * 8,421 in-lb = 50,526 in-lb.

Transfer of 50% of the retreating blades load to the advancing side = 50,526 * 1.5 = 75,789 in-lb

The loading is 75,789 in-lb / 7 in. = 10,827 lbs. 48,161 N

With 50% ABC, the outer bearing is under 3 times the load as the inner bearing is. Maneuvers and gusts will increase the loading equally on both bearing, which will bring their comparative loads somewhat closer. This might imply that the outer bearing should be capable of handling a greater load.

FORM: Rotor - Hub - Mast Bearings ~ UniCopter ~ Bold is the prefered BUT IT IS VERY LIGHT

 

Location:

Inner Bearing:

Outer Bearing:

X-roller Brg:

 

Bearing:

SKF 51218

SKF 51144

 

SKF MMXC 1932

 

Basic Dynamic Load Rating: [C]

106,000

N

178,000

N

85,800

N

 

Basic Static Load Rating: [Co]

305,000

N

800,000

N

143,000

N

 

Radial Load Factor for the Bearing: [X]

1

 

1

 

1

 

 

Axial Load Factor for the Bearing: [Y]

1

 

1

 

1

 

 

Actual Radial Bearing Load: [Fr]

0

N

0

N

0

N

 

Actual Axial Bearing Load: [Fa]

48160

N

48160

N

58000

N

 

Equivalent Dynamic Bearing Load: [P]

48160

N

48160

N

58001

N

 

 

 

 

 

 

 

 

 

Bearing Type:

Thrust Ball

 

Thrust Ball

 

X-cylindrical Roller

 

 

 

 

 

 

 

 

 

 

Basic Rating Life (in millions of revolutions): [L10]

11 ??

 

50 ??

 

3 ??

 

 

Rotor Revolutions per Minute: [nn]

733

RRPM

733

RRPM

480

RRPM

 

Basic Rating Life (in hours): [L10h]

242

hours

1148

hours

112

hours

 

Reliability: [rr]

97

%

97

%

97

%

 

Adjusted Ratting Life: [Ln]

107

hours

505

hours

49

hours

 

 

 

 

 

 

 

 

 

Bearing contact angle: [Theta]

 

deg.

 

deg.

 

deg.

 

Momentum Load: [M]

 

in-lb

 

in-lb

 

in-lb

 

Bearing Pitch Diameter: [PD]

 

in.

 

in.

 

in.

 

Equivalent Radial Load: [Pr]

 

lb

 

lb

 

lb

 

Weight: (each)

1.7 kg

 

4.6 kg

 

3.65 kg

 

 

1 Newton = 0.2248 Pound Force

 

 

 

 

 

 

Previously Considered Bearing Selection:

Angular Contact Thrust Bearing:

Can these bearings be split or supplied as single row w/ 60-degrees?

Notes:

Moment Loads:

When the loads act eccentrically on the bearing paired single row angular contact ball bearings or tapered roller bearings work best when arraigned back-to-back.  

Kaydon Bearing Calculations: ~ Forget, since Kaydon cannot handle the speed.

Limiting speed :

N = (Fl * Cf * 1000)/ D ~ Actual speed 670 RRPM

 

N

RPM

150 RRPM

 

Fl

Derating factor

0.5 (guess)

 

Cf

Charted figures

3 (guess)

 

D

Bearing bore in inches

10

Type X Four-Point Contact:

Pr = (1.2M / PD Sin Θ) + 0.75Fr + 0.9Ft

 

Pr

Equivalent radial load

Never bothered to work out.

 

Fr

Radial load

300 lbs. (guess)

 

Ft

Thrust load

650 lbs. (hover at gross weight)

 

M

Moment load

38,545 (2 * 6,424 * 3G)

 

PD

Bearing pitch diameter in inches

11 inches

 

Θ

Bearing contact angle

30º for standard bearing

Life-Load-Speed Formulas:

Lh = (16,667 / S) * (C / P)3

 

Lh

L10 life in hours

Never bothered to work out.

 

S

Speed in RPM

 

 

C

Kadon dynamic load rating

 

 

P

Applied load

 

Same Page ~ Different Craft: ~ Electrotor-Simplex ~ Not quite, but probably in the future Dragonfly

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Last Revised: February 26, 2004