B258

OTHER: Composite - General

Overview:

General information related to composites.

Items:

 

Name

Item

 

 OTHER: Composite - General - Tow

1073

 

 OTHER: Composite - General - Miscellaneous

1336

 

Reference:

 

 

 BUY: Composite - Tow - Carbon/Graphite - Towpreg

1370

Torsional Stiffness:

CarterCopter rotor blades are torsionally very stiff (4 layers of +/- 45 Carbon cloth are used in the rotor blade's skin) so they have never measured any blade flutter tendency. ~ from CarterCopter marketing page.

Weight Reduction:

It is estimated from the Army/Bell Advanced Composite Airframe Program (1986) plus later advances that the use of composite materials can reduce the airframe weight by 25% without sacrificing chrashworthiness or other strength concerns.

Code (from Tutorial)

(the axis is the direction of the thread, I think)

(x & y are the ply axis)

Sx

On-axis stress

looks like x is the longitudinal

Sy

On-axis stress

looks like y is the transverse

Ss

On-axis stress

 

 

 

 

(1 & 2 are the laminate axis)

S1

Off-axis stress

S2

Off-axis stress

S6

Off-axis stress

 

Ex

Strength – longitudinal

Ey

Strength – transverse

 

th the ply angle (is AN in Hollmann)

Laminator program

Code

Description

Default values

Stacking Sequence:

[0/45/-45/90/90/-45/45/0]

 

Material properties:

E1

 

19.4E+06 psi

 

 

 

 

E2

 

1.7E+06 psi

 

 

 

 

V12

 

0.38

 

 

 

 

G12

 

0.89E+06 psi

 

 

 

 

CTE1

 

1.1E-08 in/in/F

 

 

 

 

CTE2

 

12.5E-06 in/in/F

 

 

 

 

CHE1

 

0.0 in/in

 

 

 

 

CHE2

 

0.44 in/in

 

 

 

 

 

Material strengths:

Xt

 

204,000 psi

 

 

 

Xc

 

-197,000 psi

 

 

 

Yt

 

5900 psi

 

 

 

Yc

 

-20,700 psi

 

 

 

S

 

13,300 psi

 

 

 

Load vector:

Nx

X normal force

1000 lb/in

 

 

 

Mx

X moment

10 in-lb/in

 

 

 

Ny

Y normal force

Nxy = My = Mxy = 0.0

 

 

 

Material

Fabric

Unidirectional

E-glass

S-glass

M-glass

Intermediate Strength Carbon (graphite)

Kevlar

Bi-directional

Resin

Polyester

Epoxy

Core

 

Adhesive

 

Measurement of Pressure is in Pounds per Square Inch -or- Pascals

I.e. 306 Ksi

= 2110 Mpa

 

1000 Pascals

= 1 Kilopascals

1000 Kilopascals

= 1 Megapascal [Mpa]

1000 Megapascals

= 1 Gigapascal ?? [Gpa]

 

1000 psi

= 1 ksi

1000 ksi

= 1 msi

 

1 Pounds/Inch^2 [psi]

= 6894.757 Pascals

1 Pounds/Inch^2 [psi]

= 6.894757 Kilopascals

1 Pounds/Inch^2 [psi]

= 0.006894757 Megapascals [Mpa]

1000 Lb/Inch^2 [ksi]

= 6.894757 Megapascals [Mpa]

 

 

 

Therefor 1 ksi

= 6.894754 Mpa

 

 

1000000 Lb/Inch^2 [msi]

= 6.894757 Gigapascals [Gpa]

 

 

Therefor 1 msi

= 6.894757 Gpa

 

 

Beams/Spar

Consider Pultruded Carbon. "Spartuf", "Graphlite"

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Last Revised: July 19, 2005