首页> 外文期刊>Journal of the British Interplanetary Society >LOW-COST LIFE ASSESSMENT OF LIQUID ROCKET ENGINES by replacing full-scale engine tests with TMF panel tests
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LOW-COST LIFE ASSESSMENT OF LIQUID ROCKET ENGINES by replacing full-scale engine tests with TMF panel tests

机译:用TMF面板测试更换全尺寸发动机测试,液体火箭发动机的低成本寿命评估

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Liquid rocket engines are still key components of many space transportation systems. The combustion chamber of the engine itself is one of the most critical parts as it has to withstand severe temperatures, extreme temperature gradients and high pressures. Reusability and therefore cyclic loading can lead to failure due to rupture of the cooling channels in the inner liner of the combustion chamber. Those failures are induced by a progressing failure mechanism called doghouse effect. The doghouse effect causes thinning of the cooling channels until rupture. For the development of new engines numerical methods are used. In order to save costs for obtaining experimental data to validate numerical analysis methods, a Thermo-Mechanical Fatigue (TMF) test bench was set up at the Lampoldshausen site of German Aerospace Center (DLR) to reduce the need for expensive full scale rocket engine tests. The test bench uses so-called thermomechanical fatigue panels representing a small section of the geometry (5-7 cooling channels) of the hot gas wall. To simulate the heat load, a diode laser can provide thermal loading with heat fluxes up to q = 25 MW/m2 applied to an area of 10 mm ⅹ 34 mm. Supercritical Nitrogen at a temperature of T = 160 K and a pressure of p = 50 bar serves as coolant. The laser is cyclically powered on for typically 200 s until rupture is visible. The heat distribution on the laser-loaded surface of the TMF panel is measured with an infrared camera. The fatigue life is assessed by counting the number of laser cycles. With this method the appropriateness and response of different copper based alloys can be predicted for different use-cases like liquid core stage engines, liquid booster engines or liquid upper stage engines regarding thermomechanical fatigue by utilizing a cost-saving alternative to full scale rocket engine tests. This paper presents the detailed capabilities and potential of the TMF panel test bench at DLR Lampoldshausen as well as the recent results of a TMF panel made of CuCrZr alloy.
机译:液体火箭发动机仍然是许多太空运输系统的关键部件。发动机本身的燃烧室是最关键的部分之一,因为它必须承受严重的温度,极端温度梯度和高压。由于燃烧室内衬的内衬的冷却通道破裂,可重用性和因此循环负载可能导致失效。这些失败是通过称为狗座效应的进展失败机制引起的。狗屋效应导致冷却通道的变薄直至破裂。对于新兴发动机的开发,使用了数控。为了节省获得实验数据以验证数值分析方法的成本,在德国航空航天中心(DLR)的Lampoldshausen站点设立了热机械疲劳(TMF)测试台,以减少昂贵的全尺度火箭发动机测试。测试台使用所谓的热机械疲劳面板,该图案表示热气体壁的几何形状(5-7冷却通道)的一小部分。为了模拟热载荷,二极管激光可以提供热量的热量,热通量高达Q = 25 mw / m 2,施加到10mm 3 34 mm的面积。在T = 160k的温度下的超临界氮气和P = 50巴的压力用作冷却剂。激光器循环通电,通常为200秒,直到断裂可见。用红外相机测量TMF面板的激光加载表面上的热分布。通过计算激光循环的数量来评估疲劳寿命。通过这种方法,可以预测不同铜基合金的适当性和响应,如液体芯级发动机,液体增压发动机或液体上级发动机,通过利用节省级别的尺度火箭发动机测试来预测关于热机械疲劳的液体芯级发动机,液体增压发动机或液体上级发动机。本文介绍了DLR Lampoldshausen的TMF面板测试台的详细功能和潜力,以及由CucrZR合金制成的TMF面板的最近结果。

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