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Figure 63. Stator blade with film cooling holes in configuration 4: 3D view (left) and side view (right)..............................................................................................101 Figure 64. Midspan Mach number distribution and velocity vectors for configuration 1. The distribution is similar for the other configurations as well..................104 Figure 65. Midspan temperature distribution for the four configurations......................105 Figure 66. Stator blade surface temperature distribution for all configurations: Configuration 1 represents the basic case with uniformly distributed injectors in the circumferential direction; Configurations 2 and 3 represent the case with the indexed injectors; Configuration 4 represents the film cooled stator blade. .........................................................................................107 Figure 67. Film cooling effectiveness contours on stator blade, configuration 4: PS (left), SS (right)...............................................................................................108 Figure 68. Rotor inlet temperature distribution for the four configurations. .................110 Figure 69. UHEGT, cross section of the complete assembly. The assembly consists of three main components: Compressor on the left, connection piece in the middle, and turbine on the right......................................................................114 Figure 70. UHEGT, 3D model of the rotor and casing. .................................................115 Figure 71. Simulation schematic of UHEGT (by Schobeiri). ........................................116 Figure 72. Discretized flow path with changing cross section S=S(x); Reprinted from Schobeiri [1]. ..................................................................................................117 Figure 73. System components and their modular representation; Reprinted from Schobeiri [1]. ..................................................................................................121 Figure 74. Representation of an adiabatic turbine component in the row-by-row calculation. Each stage is decomposed into two rows that are connected via the middle plenum. .........................................................................................123 Figure 75. Tubular combustion chamber; Reprinted from Schobeiri [31].....................124 Figure 76. UHEGT injector component: Front view (top) and left view (bottom)........125 Figure 77. Schedule applied through fuel valve to the injector component...................126 Figure 78. Sinusoidal fuel schedule. ..............................................................................127 Figure 79. Sinusoidal schedule: Compressor sets’ mass flow rates...............................129 xviiiPDF Image | DEVELOPMENT OF AN ULTRA-HIGH EFFICIENCY GAS TURBINE ENGINE (UHEGT
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