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NOVALT16 BEARING #2 OIL SYSTEM DESIGN - TEST RIG ARCHITECTURE, FUNCTIONAL TESTS AND DESIGN CHALLENGES

机译:NOVALT16轴承#2石油系统设计-试验台结构,功能测试和设计挑战

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This paper describes the test rig and the functional tests that have been carried out to define a satisfying solution for the bearing #2 of NovaLT16, the GE Oil & Gas latest high-efficiency Gas Turbine. The bearing #2 is a journal bearing located inside the compressor discharge casing and for this reason it is exposed to high temperatures. As a consequence, the lube oil provided to the bearing should not only lubricate the bearing pads but also cool the bearing housing and for this reason it should be more than what required by the pads. This large amount of oil is gathered by two bearing housing sumps and then drained by gravity through two pipes. Scavenge pumps are not required. The bearing housing also includes two circumferential labyrinth seals able to prevent oil leakage through the gap between the bearing housing and rotor. Both seals are purged by air extracted from the gas turbine compressor; the air not only creates a barrier to oil leakage but facilitate the draining inside the sumps. An insufficient draining system may increase the oil levels in the bearing housing sumps above the safety limit and therefore it may generate oil leakage through the labyrinth seals. If the leakage reaches the external high-temperature zone then it can lead to oil degradation, decrease in GT performances and engine tripe due to smoke in the GT package in the worst case. The draining system was therefore tested with an advanced test rig. The test rig was a 1:1 scale including the bearing housing, the bearing with its pads and also a mock-up of the shaft. The shaft was driven by an electric motor and therefore it was possible to verify the full operating speed range of the gas turbine. The gas turbine discharge compressor casing environment was simulated through electric resistances able to provide heat all around the bearing housing. During the functional tests there have been simulated design and off-design conditions including extreme values of oil pressure, oil temperature, pitch and roll angles (for offshore application), shaft speed and buffering air. The results were mainly evaluated in terms of sump oil levels, shaft temperatures and bearing housing temperatures. The full test campaign allowed to identify and validate a satisfying configuration both for on-shore and off-shore applications and to properly tune all the main bearing parameters in order to guarantee a robust configuration. The NovaLT16 test campaign is part of the continue evolution in the GE O&G bearing #2 area design, started with the previous gas turbines (such as MS5002E and GE10).
机译:本文介绍了为确定NovaLT16#2轴承(GE石油和天然气最新型高效燃气轮机)的令人满意的解决方案而进行的试验台和功能测试。轴承#2是位于压缩机排气箱内部的轴颈轴承,因此,该轴承承受高温。结果,提供给轴承的润滑油不仅应润滑轴承垫,而且还应冷却轴承箱,因此,它的含量应超过轴瓦的要求。大量的油被两个轴承箱的油槽收集,然后通过重力通过两个管道排出。不需要扫气泵。轴承箱还包括两个周向迷宫式密封件,能够防止油通过轴承箱和转子之间的间隙泄漏。从燃气轮机压缩机抽出的空气清除了两个密封件。空气不仅会造成漏油的障碍,而且还会促进油池内部的排油。排放系统不足可能会使轴承箱中的油位增加到超过安全极限,因此可能通过迷宫式密封产生漏油。如果泄漏到达外部高温区域,则可能导致机油降解,GT性能下降以及由于最坏情况下GT封装中的烟气而导致发动机三角架损坏。因此,排水系统使用了先进的测试设备进行了测试。测试台架为1:1比例,包括轴承箱,带垫的轴承以及轴的模型。轴由电动机驱动,因此可以验证燃气轮机的整个运行速度范围。通过能够在轴承箱周围提供热量的电阻来模拟燃气轮机排气压缩机壳体的环境。在功能测试期间,已经进行了模拟设计和非设计条件,包括机油压力,机油温度,俯仰角和侧倾角(用于海上应用),轴速和缓冲空气的极值。主要根据油底壳油位,轴温和轴承座温度对结果进行了评估。全面的测试活动可以识别和验证用于陆上和海上应用的令人满意的配置,并适当调整所有主要轴承参数,以确保配置稳健。 NovaLT16测试活动是GE O&G 2号轴承区域设计不断发展的一部分,该设计始于以前的燃气轮机(例如MS5002E和GE10)。

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