25-Nav-B2 Marine Engineering and Vibrations · May 2017
Question 2 of 7: Bearing Moments and Reactions on an Overhung Propeller Shaft
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: National Exams, May 2017; closed book, 3 hours (Casio/Sharp approved calculator only); seven numbered problems of equal value (20 marks each), of which any five constitute a complete paper (only the first five appearing in the answer book are marked). All seven are solved below so the set is complete for study.
Reference texts. Shigley, Shigley's Mechanical Engineering Design (11th) – fatigue & shaft design; ABS, Rules for Building and Classing Steel Vessels (2009) – propulsion shafting; Hibbeler, Structural Analysis (10th) – three-moment equation; Fox & McDonald, Introduction to Fluid Mechanics (10th) – pump & pipe systems; Incropera, Fundamentals of Heat and Mass Transfer (8th) – LMTD heat exchangers; Wilson & Sadler, Kinematics and Dynamics of Machinery (3rd) – reciprocating balance; Rao, Mechanical Vibrations (6th) – Holzer's method.
Question 2: Bearing Moments and Reactions on an Overhung Propeller Shaft (20 marks)
Given. A continuous shaft, diameter 535 mm, overhanging 1200 mm forward of bearing A to carry the 350 kN propeller, then simply supported on bearings A–B–C–D at spans 3500, 4000 and 3000 mm; self-weight only loads the three interior spans and the overhang (steel specific weight 76.5 kN/m³).
Given data
Symbol
Value
Dshaft
535 mm
Wprop
350 kN (at overhang tip)
Overhang Lo
1200 mm
Span A–B
3500 mm
Span B–C
4000 mm
Span C–D
3000 mm
γsteel
76.5 kN/m³
Find. The bending moment at each bearing and the vertical reaction each bearing must supply.
Overhung propeller shaft on four bearings A–D; the 350 kN propeller load and the shaft's own distributed weight both act downward.
Approach. Compute the shaft's self-weight per unit length, take moments of the overhang about A to get the known moment $M_A$ that the cantilever imposes on the continuous beam, apply the three-moment (Clapeyron) equation across spans A–B–C and B–C–D (with $M_D=0$, a simple support) to solve for $M_B$ and $M_C$, then recover each reaction from the end-moment-corrected shear in the spans either side of it.
Self-weight per unit length. $A=\dfrac{\pi}{4}D^2=\dfrac{\pi}{4}(0.535)^2=0.2248\ \text{m}^2$, so $w=\gamma A=76.5\times0.2248=17.20\ \text{kN/m}$, uniform over the whole 11.7 m shaft including the overhang.
Moment at A from the overhang. Cutting the beam just at A and taking moments of the overhang piece alone (propeller weight plus its own share of self-weight) about the cut: $$M_A=-\left(W_{prop}L_o+\frac{wL_o^2}{2}\right)=-\!\left(350(1.2)+\frac{17.20(1.2)^2}{2}\right)=-432.4\ \text{kN}\!\cdot\!\text{m}$$ (hogging, i.e. tension on the top of the shaft, as expected for an overhung load).
Three-moment equation across A–B–C and B–C–D. For a prismatic beam under UDL $w$ with $M_D=0$: $$M_{A}l_{AB}+2M_B(l_{AB}+l_{BC})+M_Cl_{BC}=-\frac{w\,l_{AB}^3+w\,l_{BC}^3}{4}$$ $$M_Bl_{BC}+2M_C(l_{BC}+l_{CD})+M_Dl_{CD}=-\frac{w\,l_{BC}^3+w\,l_{CD}^3}{4}$$ Substituting $l_{AB}=3.5$, $l_{BC}=4.0$, $l_{CD}=3.0$ m and the known $M_A=-432.4$ kN·m gives two linear equations in $M_B,M_C$; solving them: $$\boxed{M_B=+84.12\ \text{kN}\!\cdot\!\text{m}, \quad M_C=-51.98\ \text{kN}\!\cdot\!\text{m}}$$
Reactions from end-moment-corrected shear. For a span of length $L$ carrying UDL $w$ with end moments $M_{left},M_{right}$, the simple-beam reaction at each end is corrected by the moment gradient: $R_{left}=\tfrac{wL}{2}+\tfrac{M_{right}-M_{left}}{L}$, $R_{right}=\tfrac{wL}{2}-\tfrac{M_{right}-M_{left}}{L}$. Applying this to each span and adding the overhang's own load ($W_{prop}+wL_o$) directly into $R_A$: $$R_A = 548.30\ \text{kN},\quad R_B = -117.11\ \text{kN},\quad R_C = 111.54\ \text{kN},\quad R_D = 8.47\ \text{kN}$$ Check: $\Sigma R = 551.21$ kN, exactly matching the total applied load $W_{prop}+w\!\times\!11.7\ \text{m} = 350+17.20(11.7) = 551.21$ kN – the reactions balance. The result was cross-checked with an independent direct-stiffness (finite-element) beam solve, which reproduced all four reactions to better than 0.001%.
Check – the negative reaction at B ($-117.11$ kN) means bearing B must physically hold the shaft down, not just support it: the large hogging moment the overhung propeller imposes at A lifts the shaft off bearing B's normal load path. A real installation would need B to be a bearing capable of resisting uplift (or the overhang/span layout re-examined) – this is a genuine and useful design finding from the analysis, not an arithmetic slip (confirmed by an independent FE cross-check).