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The next generation of civil turbofan engines targets the by-pass ratios of up to 20:1, requiring an innovative fan design with a low fan pressure ratio, low specific thrust and a radically increased fan diameter. The aerodynamic stability of such a large slow rotating fan is very sensitive against the back-pressure variations in the by-pass duct, especially during the take-off operations. The back-pressure regulation can be achieved significantly through a Variable Area Fan Nozzle (VAFN). This work deals with the design development of VAFN concepts for ultra-high by-pass ratio engines which was researched in EU funded program ENOVAL and received funding under grant agreement number 604999.
A system engineering approach was implemented for the VAFN development by following the requirements in conceptual, preliminary and detailed design phases. The design domains in the rear nacelle and under the core fairing were selected for the concept generation. Several qualitative and quantitative trade studies were conducted to down-select the best-fit solution during each design phase. These included the kinematic simulations of various types of VAFN modulations; analytical calculations to understand the thermodynamics of the selected VAFN kinematics; aerodynamic performance predictions using CFD simulations on a large number of preliminary designs; 3D CFD simulations for detailed performance assessments including the design optimization of individual features and distortions due to failed modulations; and FEM calculations for the topology generation and optimization of structural components. The overall weighted effect was determined for each output parameter and the results were presented in percentile changes relative to that with a fixed nozzle reference geometry.
Two VAFN concepts were selected for the final detailed design phase, Flaps in rear nacelle domain and Variable Inner Fairing Structure (VIFS). Both concepts showed better outputs in terms of specific fuel consumption, noise emission and fan’s safety margin during the take-off, with an over-area exhaust position than those with a fixed nozzle operation. During the climb phase, with an under-area VAFN position, both concepts resulted in drawbacks due to higher aerodynamic losses relative to the fixed nozzle. During MCR, both the VAFN concepts with stowed positions caused losses mainly due to leakages and higher structural weights relative to the fixed nozzle configuration. For each VAFN concept, a detailed system definition was developed and the function trees for each operation were explained. A discrete modulation type with two positions was described and recommended for both concepts. This included an over-area deployed position for the take-off phase and a stowed position for the rest of the flight, based on the beneficial performance of the VAFN concepts over the fixed clean nozzle configuration.
The investigation of novel structure-to-property relations of many transition metal trihalides MX₃ by downscaling to promising monolayer is still pending. However, the production of two-dimensional MX₃ sheets that are both high crystalline and thin is an experimental challenge. This thesis is focused on the rational synthesis planning and the derived targeted preparation of thin MX₃ nanosheets (≤ 100 nm) on suitable substrates by chemical vapor transport (CVT) as well as their characterization by complementary analytical methods. CVT of nanosheets directly on substrates benefits of low timescales, less material consumption and only few structural distortions. For the determination of optimal growth conditions, the CVT processes of investigated compounds were initially simulated by using the Calphad method (program package TRAGMIN). Thus, the occurring transport efficient gas species and temperature dependent, dominating vapor transport equilibria were calculated to optimize the growth process in a direct and straightforward way. Based on prior simulation results single crystalline sheets of MCl₃ (M = Ru, Mo, Ti, Cr) and CrX₃ (X = I, Br, Cl) were successfully prepared at temperatures between 573 – 1023 K on YSZ (yttrium stabilized zirconia) or sapphire substrates. The adjustable CVT parameters (transport duration, temperatures or weighed starting material) were optimized with respect to the targeted synthesis of either bulk or nanosheets at substrates. Microsheets with thicknesses of less than 4 μm (α-TiCl₃) and about 20 nm thin nanosheets (α-RuCl₃, CrCl₃ and CrI₃) down to ultrathin flakes (≈ 3 nm, α-MoCl₃ and CrBr₃) were obtained by CVT. As a highlight, monolayers of α-RuCl₃ and CrCl₃ were isolated successfully by means of a subsequent delamination. The MX₃ sheets morphology and dimension was described by optical and electron microscopy, highlighting their two-dimensional nature. By several X-ray spectroscopy and diffraction techniques the desired composition (M:X = 1:3), high crystallinity and phase-purity of thick and thin MX₃ platelets was confirmed subsequently. With respect to MX₃ nanosheets a slight increase (α-RuCl₃, α-MoCl₃ and CrBr₃) or decrease (CrCl₃) in phonon energies was observed in comparison to their bulk counterparts. The magnetic properties of CrCl₃ micro- and nanosheets were determined to be solely ferromagnetic and thus different than those of the bulk samples. Finally, the structure-to-property relations were investigated at a first example. The catalytic properties of α-TiCl₃ microsheets were investigated by gas-phase polymerization of ethylene. By downscaling the catalysts thickness by CVT, we obtained an activity improvement of 24 % in comparison to bulk α-TiCl₃.
With the rapid growth of renewable energy sources (RES) in the power generation mix in accordance with the German energy transition policy (‘Energiewende’), fewer baseload coal power plants will be required. Future power generation will be supplied through decentralized power utilities such as off-shore wind parks and also through high operational flexibility of existing conventional coal power units. High operational flexibility means conventional power plants have to increase cyclic operations to cope with feed-ins from variable-RES such as wind and solar.
Unlike medium and peak load power plants that can react quickly to load changes and power ramps, baseload power plants are not suited for such operations. Important technical requirements for flexible operation include among others; frequent start-ups and shut-downs, a minimum downtime, shorter startup time and short operational periods. Baseload coal power plants however do not meet these requirements.
This increased cyclic mode of operation can have severe impacts on vital power plant components such as superheater and reheater tubes resulting in high temperature cyclic oxidation/corrosion especially because these plants were not designed for frequent cyclic operations. To optimize plant operations, minimize material damage and reduce operational and maintenance cost, it is therefore important to understand the oxidation and corrosion risk to plants materials associated with this flexible mode of operation.
In this context, thermochemical modeling in FactSage 6.4ᵀᴹ as well as experimental investigations were carried out. For the experimental investigations, five commercial coal boiler superheater and reheater materials, namely T91, VM12-SHC, TP347-HFG, DMV304 HCu and DMV310 N were exposed for 1000 hours under discontinuous isothermal oxidation conditions and 1000 hours thermo–cyclic oxidation conditions at a metal surface temperature of 650 °C. The synthetic corrosive flue gas consisted of a mixture of CO₂, O₂, SO₂, N₂ and H₂O. The test material samples were partly covered in fly ash to investigate the effect ash deposits on the corrosion and oxidation behavior of the test materials. After exposure metallographic analysis by means of light microscopy and scanning electron microscopy (LOM and SEM–EDS) were carried out to study the oxide morphology and micro–structural properties of the materials. The oxidation kinetics (weight change) results showed significant oxide growth rates (weight gain) under cyclic oxidation conditions especially in the martensitic alloys – T91, VM12-SHC.
Furthermore, metallographic analysis revealed severe oxide spallation in the ash covered sections of these alloys. The austenitic materials (TP374-HFG, DMV310 N) with the exception of DMV304 HCu showed good oxidation behavior with minimal oxide growth both under isothermal and thermal cyclic conditions. However, severe grain boundary attack and internal sulphidation were found in these alloys. DMV310 N showed the best corrosion and oxidation performance. The thermochemical modeling calculations supported the experimental results.