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Level 6 Graduate Diploma in Engineering (9210-01) - City & Guilds

Level 6 Graduate Diploma in Engineering (9210-01) - City & Guilds

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Pr<strong>in</strong>cipal planes: the planes on which the pr<strong>in</strong>cipal stresses act. The shear stresses are zero on the<br />

pr<strong>in</strong>cipal planes.<br />

Outcome 3 Analyse and design beams under bend<strong>in</strong>g loads and calculate<br />

deflection of beams us<strong>in</strong>g several methods, <strong>in</strong>clud<strong>in</strong>g energy<br />

method.<br />

The learner can:<br />

1. Expla<strong>in</strong> and apply the flexure formula, slope and deflection of beams – relation between bend<strong>in</strong>g<br />

moment and slope; deflection determ<strong>in</strong>ate beams, double <strong>in</strong>tegration method (Macaulay’s<br />

method), derivation of formula for slope and elastic deflection for standard cases.<br />

2. Expla<strong>in</strong> and apply Mohr’s first and second theorems (Moment of Area method) to solve<br />

determ<strong>in</strong>ate problems.<br />

3. Expla<strong>in</strong> and apply Castigliano's theorem to solve problems.<br />

Outcome 4 Expla<strong>in</strong> buckl<strong>in</strong>g of columns under different load<strong>in</strong>g<br />

conditions.<br />

The learner can:<br />

1. Expla<strong>in</strong> columns and failure of columns.<br />

2. Expla<strong>in</strong> critical load of a column and slenderness ratio.<br />

3. Expla<strong>in</strong> and apply Euler’s formula for buckl<strong>in</strong>g load for column with different end conditions.<br />

4. Expla<strong>in</strong> the concept of equivalent length for various end conditions.<br />

5. Expla<strong>in</strong> Limitations of Euler’s formula, and Rank<strong>in</strong>e’s formula.<br />

6. Determ<strong>in</strong>e safe load on columns.<br />

Range<br />

Critical load - the maximum axial load that a column can support when it is on the verge of<br />

buckl<strong>in</strong>g.<br />

Ideal column - the column that is perfectly straight before load<strong>in</strong>g and made of homogeneous<br />

material, and the load is applied through the centroid of the cross section.<br />

Slenderness ratio - is L/r, where r is the smallest radius of gyration of the cross section. Buckl<strong>in</strong>g<br />

will occur about the axis where this ratio gives the greatest value.<br />

Outcome 5 Expla<strong>in</strong> k<strong>in</strong>ematic concepts of l<strong>in</strong>k mechanisms and their<br />

velocities and accelerations.<br />

The learner can:<br />

1. Expla<strong>in</strong> basic k<strong>in</strong>ematic concepts:<br />

• Inversions<br />

• S<strong>in</strong>gle and double slider crank cha<strong>in</strong>s straight l<strong>in</strong>e motion mechanisms<br />

• Four-bar mechanism k<strong>in</strong>ematics (velocity, acceleration, coupler curve)<br />

• Kennedy theorem of three centers and applied for four-bar mechanism<br />

• Grashof’s theorem to expla<strong>in</strong> categories of four-bar mechanism.<br />

2. Determ<strong>in</strong>e velocity and acceleration analysis <strong>in</strong> mechanisms:<br />

• Relative velocity methods<br />

• Instantaneous center of rotation<br />

• Kennedy theorem of three centres<br />

• Centrifugal acceleration, Coriolis acceleration<br />

• Velocity and acceleration diagrams<br />

• Accelerations <strong>in</strong> different directions (centrifugal acceleration, tangential acceleration, and<br />

Coriolis acceleration).<br />

<strong>Level</strong> 6 <strong>Graduate</strong> <strong>Diploma</strong> <strong>in</strong> Eng<strong>in</strong>eer<strong>in</strong>g (<strong>9210</strong>-<strong>01</strong>) 145

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