ryan t. casey
DESCRIPTION
RPI Masters Engineering Project: Preliminary Design and Optimization of Composite Tension-Torsion Strap for Rotor Systems 4/21/2010. Ryan T. Casey. CF Load Torsional Twist due to Pitch Input Small Flatwise Bending due to Pitch Housing Deflection. Tension-Torsion Strap . - PowerPoint PPT PresentationTRANSCRIPT
RPI Masters Engineering Project:Preliminary Design and Optimization of Composite Tension-Torsion Strap
for Rotor Systems4/21/2010
Ryan T. Casey
Tension-Torsion Strap
MD500 Rotor System
1. CF Load2. Torsional Twist due to Pitch Input3. Small Flatwise Bending due to Pitch Housing Deflection
Methodology
• Utilize Classic Laminate Theory to Determine Equivalent Material Properties
• Create ANSYS models (static)– Determine Kts– Determine Stresses & Strains in Pitch
Section, Lug-to-Pitch Section Transition• Lug Failure Modes• Optimize Geometry • Recommendations for Future Work
ANSYS Models
Preliminary Design Constraints• Lug Sizing - e/d = 2• Use IM7/8552 (Carbon/Epoxy) Unidirectional Tape
– Case1 (02/+-452/902/+-452/02)– Case2 (0/+-45/0)– Case3 (03/+-45/03)
• Length Varies between 12-18 in• CFmax = 30000lb, Max Pitch Angle = +/- 10deg
Equivalent Properties via Classic Laminate Theory Case Ex: psi Ey: psi Ez Gxy: psi Gyz Gzx n12 n23 n31
1 9.38E+06 6.68E+06 6.68E+06 3.70E+06 2.48E+06 3.70E+06 0.45 0.35 0.45
2 1.30E+07 3.61E+06 3.61E+06 3.32E+06 1.34E+06 3.32E+06 0.74 0.35 0.74
3 1.83E+07 2.68E+06 2.68E+06 1.97E+06 9.91E+05 1.97E+06 0.63 0.35 0.63
Stress Concentration (Kt)
Lug Analysis
ntnt FKt
tdWP )(
lbpsiinininPnt 38118)000,120(4.348).75.3(
MSnt = 0.27 for max CF load 30,000lb
Net Tension Failure Load (Pnt)
Bearing Failure
FEA Results
0.4% Elongation
FEA Results• Effect of Flatwise Bending Load on Shear Stresses
– 0.5 deg flatwise displacement
Shear XY Radius Shear XY Shear ZX
CF & 10 deg Twist 14900 psi 9024 psi 7300 psi
CF, 10 deg Twist, & Bending 15247 psi 8975 psi 7305 psi
Percent Variation (%) 2.33 -0.54 0.08
Final Configuration
Recommendations
Questions?