22-Mec-B4 Integrated Manufacturing Systems · December 2019
Question 1 of 7: Parts-Count Reliability and Mission Reliability
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, December 2019 —
16-Mec-B4 Integrated Manufacturing Systems. Three hours, OPEN BOOK, any
non-communicating calculator permitted. Seven questions are printed and
any five constitute a complete paper; all questions are of equal value,
so each is worth 20 marks of the 100 available. Note 1 of the paper invites the
candidate to state any assumption made where a question is open to
interpretation, and this solution uses that licence wherever the source withholds
a datum. Every one of the seven questions is worked below, because the set is a
study resource rather than a three-hour sitting.
Given. Part (a): a series subsystem of 190 components in three
part classes, with the quantities and constant hourly failure rates tabulated
above. Part (b): three independent subsystems in series, each with its own
required operating time within an 8-hour mission and its own life model.
Find. The mean time between failures of the electronic
subsystem, and the probability that all three subsystems survive their required
operating times on one mission.
Reliability block diagram for Question 1(b). The three subsystems are in series, so the mission reliability is the product of three survival probabilities — but each is evaluated at its own required operating time.
Approach. Both parts rest on the same idea: for items in
series the hazard rates add, so a parts-count prediction sums the population
failure rates to get one system rate whose reciprocal is the MTBF, and a mission
reliability multiplies the individual survival probabilities, each computed from
the life model that applies to that subsystem.
Part (a) — write the parts-count model for a series
subsystem. When every component is critical, the subsystem survives only
if all components survive, and for constant hazard rates the system rate is the
population-weighted sum
$$\lambda_s = \sum_{i} n_i \lambda_i$$
where $n_i$ is the quantity of part class $i$ and $\lambda_i$ its failure rate
per hour. No reliability is computed component by component; the rates simply
add.
Accumulate the three contributions. Taking each row in turn,
$$n_1\lambda_1 = 40 \times 74.0 \times 10^{-6} = 2960 \times 10^{-6}\ \text{h}^{-1}$$
$$n_2\lambda_2 = 100 \times 3.0 \times 10^{-6} = 300 \times 10^{-6}\ \text{h}^{-1}$$
$$n_3\lambda_3 = 50 \times 10.0 \times 10^{-6} = 500 \times 10^{-6}\ \text{h}^{-1}$$
Adding the three and re-adding them as a check gives
$\lambda_s = 3760 \times 10^{-6} = 3.760 \times 10^{-3}\ \text{h}^{-1}$.
The transistors carry 78.7 per cent of the system failure rate on 21.1 per cent of
the component count, which is the first thing a reliability review would act
on.
Invert the system rate to get the mean time between failures.
For an exponential time to failure the mean is the reciprocal of the rate,
$$\text{MTBF} = \frac{1}{\lambda_s} = \frac{1}{3.760\times10^{-3}}$$
$$\boxed{\ \text{MTBF} = 266\ \text{hours}\ }$$
(265.96 h before rounding). Two sanity figures follow immediately: over an
8-hour mission this subsystem alone has
$R = e^{-3.760\times10^{-3}\times 8} = 0.9704$, and at $t = \text{MTBF}$ the
reliability is $e^{-1} = 0.368$ — the exponential model always gives 36.8
per cent survival at the mean, never 50 per cent.
Part (b) — convert subsystem A's median life into a
rate. The phrase "50 per cent of subsystems will last at least 14 hours"
states the median, not the mean. For an exponential life the median
$t_{0.5}$ satisfies $e^{-\lambda t_{0.5}} = 0.5$, so
$$\lambda_A = \frac{\ln 2}{t_{0.5}} = \frac{0.6931}{14} = 0.049511\ \text{h}^{-1}$$
which corresponds to a mean life of $1/\lambda_A = 20.20$ h, not 14 h. Over its
required 8 hours,
$$R_A = e^{-0.049511 \times 8} = e^{-0.39609} = 0.6730$$
Take subsystem B from the normal life model at 3 hours. With
$\mu = 6$ h and $\sigma = 1.5$ h the standardised required time is
$$z = \frac{t - \mu}{\sigma} = \frac{3 - 6}{1.5} = -2.00$$
and the subsystem survives if its life exceeds 3 h, so
$$R_B = 1 - \Phi(-2.00) = \Phi(2.00) = 0.9772$$
Recognise that subsystem C's Weibull collapses to an
exponential. A Weibull with shape $\beta = 1.0$ is the
exponential distribution, whose mean equals its characteristic life, so a mean
life of 40 h means $\theta = 40$ h and
$$R_C = e^{-(t/\theta)^{\beta}} = e^{-4/40} = e^{-0.1} = 0.9048$$
Multiply the three survival probabilities. The subsystems are
independent and all three are needed, so
$$R_{\text{mission}} = R_A R_B R_C = 0.6730 \times 0.9772 \times 0.9048$$
$$\boxed{\ R_{\text{mission}} = 0.595 \quad (59.5\ \text{per cent})\ }$$
Subsystem A is the weak link by a wide margin: it contributes 67.3 per cent where
B and C contribute 97.7 and 90.5 per cent, so any reliability-growth effort
belongs there.
Check: each subsystem is evaluated at its own required operating time,
not at the 8-hour mission length. The table gives A eight hours, B three
and C four, which is the whole point of the "Required Operating Time During
Mission" column — B and C are duty-cycled, not run continuously. Evaluating
all three at 8 h gives $0.6730 \times 0.0912 \times 0.8187 = 0.0503$, an order of
magnitude too pessimistic, and it is the single commonest error on this question
type. The second reading worth declaring is A's "50 per cent last at least 14
hours" as a median; if a marker intended it as a mean, $\lambda_A = 1/14$ and
$R_A = 0.5647$, giving $R = 0.499$.