Rapid transformation of the workplace and a highly competitive labour market has changed the nature of graduate employability. In addition to discipline related knowledge, students now need to be proactive and adaptable in identifying career opportunities.  This paper presents a conceptual model that views employability as determined by an overarching professional purpose mindset.  This mindset reflects a person’s commitment to developing a professional future aligned to personal values, professional aspirations and societal outlook. Four specific mindsets are encapsulated within professional purpose (curiosity, collaboration, action and growth) and relate to three domains of development (self and social awareness; navigating the world of work and networks). Two studies were conducted to explore the professional purpose model.  Study one was a qualitative study in which 33 undergraduate students (19 female; 14 male) explored their career decision making.  Focus group and interview data showed that each of the four positive mindsets operated in many students’ proactive career related behaviours.  However, for other students, alternative mindsets negatively influenced their career related behaviour.  In the second study, 42 academics (28 male; 14 female)  identified unit learning outcomes in existing curricula related to the three domains of development.  All domains were evident but outcomes for navigating the world of work received most emphasis.  Implications of the findings for further development of the professional purpose model are discussed.

Accurate knowledge of the operating temperature of thermal barrier coatings (TBCs) is not currently available, therefore significant safety margins are employed during operation of gas turbines, which limit the engine efficiency. Recently, phosphorescent sensor TBCs have been used to detect coating temperatures with a reported accuracy under isothermal conditions up to 4 K. However, the thermal gradient through a TBC in modern gas turbines is of the order of 1 K µm−1­. The interpretation of the temperature provided by a sensor coating therefore requires a better understanding of the through thickness response of the material. Kubelka–Munk theory has been adapted to describe the light propagation and generation through the thickness of a sensor coating. The model indicates that the temperature measurement can be considered to come from a depth of 17 µm below the surface, depending on the coating type, thermal gradient and coating thickness. As such, the coating can be designed to suit the application, and the temperature variation due to the thermal gradient and coating thickness can be limited to 1%. Where coating design is restricted by its application, the sensor material can be embedded within the coating to avoid measurement errors due to thermal gradients, provided the sensor layer is sufficiently thin. This, however, causes a significant reduction in emission intensity, hence reducing the signal-to-noise ratio, and necessitating a compromise between signal amplitude and measurement accuracy.

Temperature profiling of components in gas turbines is of increasing importance as engineers drive to increase firing temperatures and optimize component’s cooling requirements in order to increase efficiency and lower CO2 emissions. However, on-line temperature measurements and, particularly, temperature profiling are difficult, sometimes impossible, to perform due to inaccessibility of the components. A desirable alternative would be to record the exposure temperature in such a way that it can be determined later, off-line. The commercially available thermal paints are toxic in nature and come with a range of technical disadvantages such as subjective readout and limited durability. This paper proposes a novel alternative measurement technique which the authors call thermal history paints and thermal history coatings. These can be particularly useful in the design process, but further could provide benefits in the maintenance area where hotspots which occurred during operation can be detected during maintenance intervals when the engine is at ambient temperature. This novel temperature profiling technique uses optical active ions in a ceramic host material. When these ions are excited by light they start to phosphoresce. The host material undergoes irreversible changes when exposed to elevated temperatures and since these changes are on the atomic level they influence the phosphorescent properties such as the life time decay of the phosphorescence. The changes in phosphorescence can be related to temperature through calibration such that in situ analysis will return the temperature experienced by the coating. A major benefit of this technique is in the automated interpretation of the coatings. An electronic instrument is used to measure the phosphorescence signal eliminating the need for a specialist interpreter, and thus increasing readout speed. This paper reviews results from temperature measurements made with a water-based paint for the temperature range 100–800 °C in controlled conditions. Repeatability of the tests and errors are discussed. Further, some measurements are carried out using an electronic hand-held interrogation device which can scan a component surface and provide a spatial resolution of below 3 mm. The instrument enables mobile measurements outside of laboratory conditions. Further, a robust thermal history coating is introduced demonstrating the capability of the coating to withstand long term exposures. The coating is based on thermal barrier coating (TBC) architecture with a high temperature bondcoat and deposited using an air plasma spray process to manufacture a reliable long lasting coating. Such a coating could be employed over the life of the component to provide critical temperature information at regular maintenance intervals for example indicating hot spots on engine parts.

International audienceFurther improvements in the efficiency of gas turbines are recognised to come from increases in turbine entry temperatures. Accurate temperature measurements are crucial to achieve these increases whilst maintaining reliability and economic component life. The combination of phosphor thermometry and thermal barrier coating (TBC) technology has led to the development of functional temperature sensor coatings which have several advantages over conventional temperature measurement techniques. Developments in sol–gel processing indicate that this method could be used for the production, or particularly, the repair of TBCs in the future. This paper demonstrates, for the first time, that sol–gel processing can be used to make sensor TBCs. The optimum concentration of SmO1.5 was 2 wt.% in YSZ to achieve the brightest phosphorescence emission. Above this concentration the overall intensity of the emission reduces and the transitions from 4F3/2 were suppressed. Furthermore, a similar suppression of these transitions was observed when the product of the sol–gel was heat treated to 1100 ◦C. This was concluded to be due to a higher degree of crystallinity allowing a greater interaction between the dopant ions. The dependence of the phosphorescence spectrum on heat treatment temperature provides the first indication that YSZ produced through sol–gel could be used to detect historic temperatures. An evaluation of the subsurface measurement and temperature capabilities has shown that the phosphorescence can be detected from relatively thin layers, 20 µm, even under 50 µm of undoped YSZ coating. Although the temperature detection range, 400–700 ◦C, is too low for advanced TBCs the material could be used in low temperature regimes or for health monitoring purposes

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Existing thermal barrier coatings (TBCs) can be adapted enhancing their functionalities such that they not only protect critical components from hot gases but also can sense their own material temperature or other physical properties. The self-sensing capability is introduced by embedding optically active rare earth ions into the thermal barrier ceramic. When illuminated by light, the material starts to phosphoresce and the phosphorescence can provide in situ information on temperature, phase changes, corrosion, or erosion of the coating subject to the coating design. The integration of an on-line temperature detection system enables the full potential of TBCs to be realized due to improved accuracy in temperature measurement and early warning of degradation. This in turn will increase fuel efficiency and will reduce CO2 emissions. This paper reviews the previous implementation of such a measurement system into a Rolls-Royce jet engine using dysprosium doped yttrium-stabilized-zirconia (YSZ) as a single layer and a dual layer sensor coating material. The temperature measurements were carried out on cooled and uncooled components on a combustion chamber liner and on nozzle guide vanes (NGVs), respectively. The paper investigates the interpretation of those results looking at coating thickness effects and temperature gradients across the TBC. For the study, a specialized cyclic thermal gradient burner test rig was operated and instrumented using equivalent instrumentation to that used for the engine test. This unique rig enables the controlled heating of the coatings at different temperature regimes. A long-wavelength pyrometer was employed detecting the surface temperature of the coating in combination with the phosphorescence detector. A correction was applied to compensate for changes in emissivity using two methods. A thermocouple was used continuously measuring the substrate temperature of the sample. Typical gradients across the coating are less than 1 K/μm. As the excitation laser penetrates the coating, it generates phosphorescence from several locations throughout the coating and hence provides an integrated signal. The study successfully proved that the temperature indication from the phosphorescence coating remains between the surface and substrate temperature for all operating conditions. This demonstrates the possibility to measure inside the coating closer to the bond coat. The knowledge of the bond coat temperature is relevant to the growth of the thermally grown oxide (TGO) which is linked to the delamination of the coating and hence determines its life. Further, the data are related to a one-dimensional phosphorescence model determining the penetration depth of the laser and the emission.