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1) (60 points TOTAL) (65 points TOTAL) Part of the proposed Space Station Freedom will be a set of laboratory equip-ment for research into low gravity chemical and materials processing. One piece of this equipment will be a high speed centrifuge for separating solutions and applying a centrifugal load to a specimen. The main arm of the centrifuge, shown at the right, is fixed at a length of L, but the cross sectional area, A, is free. Because of the expense of launching equipment into space, minimizing the mass is the most important objective. To function, the centrifuge arm must also meet two constraints. First, It must not fail under use, essentially a tensile load of FTEST. |
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The operative constraining equations are given below. Use these to answer the following questions.

1.a) (5 points) What is the measure of performance for this design?___________
1.b) (15 points) Derive the performance index for the tensile (test) load constraint, M1, including the shape factor if appropriate.
1.c) (15 points) Derive the performance index for the side (start) load constraint, M2, including the shape factor, if appropriate.
1.d) (10 points) Derive the coupling equation for these two performance indices.
1.e) (15 points) In order to TRIPLE the performance of the centrifuge arm under a side load, how large a shape factor is required?
1.f) (5 points) Is this problem underconstrained, overconstrained, or fully determined? Explain your answer.
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1.a) The measure of performance is MINIMUM MASS: p = 1/m = 1/(rho L A).
1.b) For the tensile load constraint, there is no shape factor because the tensile properties do not depend on the cross sectional shape, only the cross sectional area.

1.c) For the side load constraint we do need to worry about the shape factor. In this case, we are worried about failure in bending, so the appropriate shape factor is phi(f-B).

1.f) The problem is overconstrained because it has two constraints, but only one free parameter.
Rule of Mixtures: An approximation for determining the properties of composites. The property of the composite material may be approxiamted from the properties of the components using
where Vm and Vr are the volume fractions of the matrix material and reinforcement material, respectively, and Pm and Pr are the properties of the matrix and reinforcement materials (see lecture notes).
Ceramic Whisker: A reinforcement material used in composite materials that consists of a ceramic single crystal, generally only a few microns in diameter and up to a few millimeters long. They are used as a discontinuous reinforcement (p. 129 Budinski and lecture notes).
Sintering: The fusing together of powder particles (usually ceramics, but also for powdered metals and some high temperature ploymers) by a high-temperature self-diffusion process, usually under pressure (p. 193 Budinski and lecture notes).
Al2O3 is a member of the oxides;
TiC is a member of the intermetallics:
pyrolytic graphite is a member of the carbons.