ENTROPY ANALYSIS OF THERMAL RESISTANCE IN THE GAS TURBINE ENGINE COMBUSTOR AND 'EFFECT' OF AEROTHERMOPRESSION

B. Kh. Perelshtein

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ENTROPY ANALYSIS OF THERMAL RESISTANCE IN THE GAS TURBINE ENGINE COMBUSTOR AND 'EFFECT' OF AEROTHERMOPRESSION

机译：燃气轮机燃烧室热阻的熵分析及热压“效应”

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The hydraulic ideal Brayton cycle operating with the finite velocity that includes the processes of compression and heating, expansion and cooling consists of irreversible parts only where the symmetric action results in a response that is symmetric with respect to the sign of entropy being generated. Wave resistance in the supersonic compressor and thermal resistance in the combustor are connected with the local increase of entropy. The buildup of total pressure in the aerothermopressor (a complete thermodynamic antipode of a combustor) during flow cooling is the result of the local decrease in entropy. We develop theoretical prerequisites in order to create thermomechanical systems of a new type with elements of programmed self organization (synergetic processes).

机译：以有限速度运行的液压理想布雷顿循环，包括压缩和加热，膨胀和冷却过程，仅由不可逆部分组成，其中对称作用导致相对于所产生的熵的符号对称的响应。超音速压缩机的波阻和燃烧室的热阻与熵的局部增加有关。流动冷却过程中，空气加压器（燃烧器的完全热力学对映体）中总压力的增加是熵局部降低的结果。我们开发理论先决条件，以便创建具有程序化自组织（协同过程）元素的新型热机械系统。

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《Russian Aeronautics》 |2003年第1期|共5页
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B. Kh. Perelshtein;
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1. ENTROPY ANALYSIS OF THERMAL RESISTANCE IN THE GAS TURBINE ENGINE COMBUSTOR AND "EFFECT" OF AEROTHERMOPRESSION [J] . B. Kh. Perelshtein Russian Aeronautics . 2003,第1期

机译：燃气轮机燃烧室热阻的熵分析及热压“效应”
2. Entropy Analysis of Thermal Resistance in the Gas Turbine Engine Combustor and "Effect" of Aerothermopressor [J] . B. KH. PERELSHTEIN Известия　Высших　учебных　заведений: Авиационная　техника . 2003,第1期

机译：燃气轮机燃烧室热阻的熵分析及空气加压器的“作用”
3. Entropy Analysis of Thermal Resistance in the Gas Turbine Engine Combustor and "Effect" of Aerothermopressor [J] . B. KH. PERELSHTEIN Известия　Высших　учебных　заведений: Авиационная　техника . 2003,第1期

机译：燃气轮机发动机燃烧器中热阻的熵分析，“空气热压器”效应“
4. Non-Reacting and Reacting Flow Analysis in an Aero-Engine Gas Turbine Combustor Using CFD - 22nd Cliff Garret Turbomachinery Engineering Award [C] . V. Ganesan World Congress . 2007

机译：空气发动机燃气轮机燃烧器中的非反应和反应流动分析使用CFD - 22ND悬崖陀螺涡轮机械工程奖
5. Experimental Investigation of the Effect of Engine Representative Combustor Exit Temperature Profile and Disc Cavity Leakage Flow on the Film Cooling of Contoured Hub Endwall of a High Pressure Gas Turbine Rotor Cascade. [D] . Ayaskanta, Arya. 2013

机译：发动机代表性燃烧室出口温度曲线和圆盘腔泄漏流对高压燃气轮机转子叶栅轮廓轮毂端壁薄膜冷却影响的实验研究。
6. Dispersion of Entropy Perturbations Transporting through an Industrial Gas Turbine Combustor [O] . Yu Xia, Ignacio Duran, Aimee S. Morgans, -1

机译：通过工业燃气轮机燃烧室的熵扰动的扩散
7. Thermal Analysis and Creep Lifetime Prediction Based on the Effectiveness of Thermal Barrier Coating on a Gas Turbine Combustor Liner Using Coupled CFD and FEM Simulation [O] . Kanmaniraja Radhakrishnan, Jun Su Park 2021

机译：基于耦合CFD和FEM模拟的燃气涡轮机燃烧器衬里热阻涂层有效性的热分析和蠕变寿命预测

ENTROPY ANALYSIS OF THERMAL RESISTANCE IN THE GAS TURBINE ENGINE COMBUSTOR AND 'EFFECT' OF AEROTHERMOPRESSION

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