22-Mec-B4 Integrated Manufacturing Systems · December 2018
Question 3 of 7: Mean Time Between Failures and Mission Reliability
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 16-Mec-B4 Integrated Manufacturing Systems,
National Exams December 2018 — a three-hour open-book examination;
any non-communicating calculator is permitted. The cover page states that
“Any five (5) questions constitute a complete paper” and that only the first
five as they appear in the answer book will be marked, and that “All questions are
of equal value”, so each of the seven printed questions is worth 20 marks against a
100-mark paper. Note 1 invites the candidate to submit a clear statement of any
assumptions made where a question is open to interpretation — this paper needs that
licence twice, and both places are flagged below in a Check box. Note 5 warns
that some answers are wanted in essay form, where clarity and organisation carry marks.
All seven questions are worked here, because the set is a study resource rather than a
timed attempt.
Reference texts. D. C. Montgomery, Introduction to Statistical
Quality Control, 8th ed. (Shewhart charts for the mean and the range, control-chart
factors, process capability); A. J. Duncan, Quality Control and Industrial
Statistics, 5th ed. (chart practice, natural tolerance versus specification,
statistical tolerance intervals); E. S. Buffa and R. K. Sarin, Modern Production /
Operations Management, 8th ed. (cost structures and break-even analysis, production
planning and control, order types and dispatching); R. B. Chase, F. R. Jacobs and
N. J. Aquilano, Operations and Supply Chain Management, 16th ed. (shop-floor
control and the volume–process relationship); C. E. Ebeling, An Introduction to
Reliability and Maintainability Engineering, 3rd ed. (series systems, exponential,
normal and Weibull life models, safety margin and stress–strength interference); and
M. P. Groover, Automation, Production Systems, and Computer-Integrated
Manufacturing, 5th ed. (numerical control, and robot control resolution, accuracy and
repeatability). Canadian practice follows the same texts: CSA and ISO 9001 quality-system
requirements sit above the chart methods used here, and CSA Z434 governs the safeguarding
of the industrial robots discussed in Question 7.
Question 3: Mean Time Between Failures and Mission Reliability (20 marks)
Given. Two reliability problems: a component population with constant
failure rates, and a three-subsystem mission profile in which each subsystem must survive
its own duty period.
Part (a) — component failure-rate data
Component
Quantity $n_i$
Failure rate $\lambda_i$ (per hour)
Silicon transistor
40
$74.0 \times 10^{-6}$
Film resistor
100
$3.0 \times 10^{-6}$
Paper capacitor
50
$10.0 \times 10^{-6}$
Part (b) — mission profile, total mission length 8 hours
Subsystem
Required operating time
Life distribution
Reliability information
A
8 hours
exponential
50 per cent last at least 14 hours
B
3 hours
normal
mean life 6 hours, standard deviation 1.5 hours
C
4 hours
Weibull, $\beta = 1.0$
mean life 40 hours
Find. (a) the mean time between failures of the electronic system;
(b) the reliability of the three-subsystem system over the 8-hour mission.
Check: what part (b) asks for. The paper prints the mission data and
the table but never states the quantity to be computed. The only question the data
support — a required operating time and a life distribution for each subsystem, with
nothing said about redundancy or repair — is the reliability of the system for
the stated mission, and that is what is answered here, with each subsystem's
reliability reported on the way so that partial credit is visible. Stated as an assumption
under Note 1: the three subsystems are functionally in series (all three are needed) and
their failures are statistically independent.
Approach. Part (a): for a series population of exponential components
the system hazard is the quantity-weighted sum of the component hazards, and the mean time
between failures is its reciprocal. Part (b): convert each subsystem's reliability
information into the parameter of its own distribution, evaluate that distribution at
that subsystem's required operating time, and multiply.
Figure 3.1 — Reliability block diagram for
part (b). The three subsystems are in series, but each is evaluated at its own required
operating time, not at the 8-hour mission length.
Part (a) — sum the hazard contributions. With every component
critical, the system is a series of $40 + 100 + 50 = 190$ items, and constant hazards add:
$$\lambda_s = \sum n_i \lambda_i
= 40(74.0) + 100(3.0) + 50(10.0) \ \text{per } 10^{6} \text{ h}$$
$$\lambda_s = (2960 + 300 + 500) \times 10^{-6} = 3760 \times 10^{-6}
= 3.760 \times 10^{-3} \text{ per hour}$$
The transistors alone account for 2960 of the 3760, that is 78.7 per cent of the total
hazard, which is where any reliability-improvement effort should start.
Part (a) — invert to get the mean time between failures. For an
exponential life the mean is the reciprocal of the constant hazard:
$$\text{MTBF} = \frac{1}{\lambda_s} = \frac{1}{3.760 \times 10^{-3}}
= 265.96 \text{ hours}$$
$$\boxed{\;\text{MTBF} \approx 266 \text{ hours}\;}$$
As a sanity figure, the reliability of that system over an 8-hour mission would be
$e^{-\lambda_s(8)} = e^{-0.03008} = 0.9704$.
Part (b) — subsystem A from its median life. The statement that
50 per cent survive at least 14 hours makes 14 hours the median, not the mean.
For an exponential life the median is $\ln 2/\lambda$, so
$$\lambda_A = \frac{\ln 2}{14} = \frac{0.69315}{14} = 0.049511 \text{ per hour},
\qquad \text{MTTF}_A = \frac{1}{\lambda_A} = 20.20 \text{ hours}$$
$$R_A(8) = e^{-\lambda_A (8)} = e^{-0.39608} = 0.6730$$
Part (b) — subsystem B from the normal life model. Subsystem B
is only needed for 3 hours of the 8-hour mission, so it is evaluated at 3 hours:
$$z = \frac{t - \mu}{\sigma} = \frac{3 - 6}{1.5} = -2.00,
\qquad R_B(3) = 1 - \Phi(-2.00) = \Phi(2.00) = 0.9772$$
Part (b) — subsystem C from the Weibull model. A Weibull life
with shape $\beta = 1.0$ is exponential, and for $\beta = 1$ the mean life equals the
characteristic life, so $\theta = 40$ hours and
$$R_C(4) = \exp\!\left[-\left(\frac{t}{\theta}\right)^{\beta}\right]
= e^{-(4/40)^{1.0}} = e^{-0.100} = 0.9048$$
Part (b) — combine in series. The three are independent and all
are required, so the mission reliability is the product:
$$R_{\text{sys}} = R_A R_B R_C = (0.6730)(0.9772)(0.9048)$$
$$\boxed{\;R_{\text{sys}} = 0.5951, \text{ that is about } 59.5 \text{ per cent}\;}$$
Subsystem A contributes essentially all of the shortfall: it is the only one asked to run
the full 8 hours, and it does so on a mean life of only 20 hours. Even a perfect A would
cap the mission at $R_B R_C = 0.8843$. A cold-standby unit for A alone, giving
$R_A = e^{-\lambda_A t}(1 + \lambda_A t) = 0.9395$, would lift the mission reliability to
0.8308 without touching B or C; doubling A's mean life is not enough on its own, since it
raises $R_A$ only to 0.8203 and the mission to 0.7254.