Study on Cryogenic Hybrid Journal Bearings for Rocket Thrbopumps
Study on Cryogenic Hybrid Journal Bearings for Rocket Thrbopumps
批准号:
13555266
负责人:
OIKE Mamoru
金额:
$8.51万
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (B)
财政年份:
2001
资助国家:
日本
项目状态:
已结题
起止时间:
2001 至 2003
中文摘要
动静压混合轴承是一种兼具静压轴承和动压轴承特点的动静压滑动轴承。混合动力轴承的主要优点是设计尺寸小,承载能力好,准无限寿命(没有观察到的磨损),并使用工艺液进行润滑。在未来可重复使用运载火箭(RLV)的低温火箭发动机中,通过用动静压轴承替代低温涡轮泵中的自润滑球轴承,可以显著提高涡轮泵的寿命,并且可以广泛地延长涡轮泵转速的固有限制,而机械部件的寿命是一个关键问题。为此,开展了低温动静压轴承的试验研究,根据常规计算方法得到的分析结果,设计了转速高达12万转/分的试验动静压轴承。TES…More t轴承的直径为60 mm,L/D=0.42,游隙/半径=0.001,有9个凹槽。旋转试验是利用日本宇宙航空研究开发机构Kakuda推进研究中心的滑动轴承试验台进行的。向测试轴承提供液氮,压力约为5兆帕。对小孔直径为0.51 mm的轴承的试验结果表明,自激振动的幅度比同步振动大几倍,是由于液氮空化流动引起的气锤不稳定引起的。然而,小孔直径为0.80 mm的轴承可以在高达50,000 rpm的转速下运行,没有任何自激振动。试验结果与基于试验条件的动静压系数数值预测结果的对比表明,流体旋转引起的大耦合刚度系数引起的失稳被认为是在50000转/分以上的转速下开始产生的。因此,基于上述数值预测,设计并制造了一种具有更高动静压性能的新型动静压轴承。较少
英文摘要
A hybrid bearing is a fluid-film journal bearing with characteristics of both hydrostatic and hydrodynamic bearings. The main advantage of hybrid bearings are small design size, good load capacity, a quasi-unlimited life (no observed wear), and the use of the process fluid for lubrication. By replacement of the self-lubricating ball bearings in the cryogenic turbopumps by the hybrid bearings, a significantly higher lifetime can be obtained and the inherent limitation of the rotational speed of the turbopumps can be widely extended in cryogenic rocket engines for future reusable launch vehicles (RLVs), where the lifetime of mechanical components is a critical issue. Therefore, experimental study on cryogenic hybrid bearings was carried out to develop the high performance hybrid bearings forcryogenic turbopumps.Test hybrid bearings were designed to operate at a rotational speed of up to 120,000 rpm based on the analytical results obtained from the conventional calculation method. The tes … More t bearing has a 60 mm diameter with L/D = 0.42, clearance/radius = 0.001, and 9 recesses. Rotating tests were carried out using the journal bearing test apparatus in Kakuda propulsion research center of JAXA. Liquid nitrogen is supplied to the test bearing with a pressure of about 5 MPa. Test results for the bearing with a 0.51 mm orifice diameter show that the self-excited vibration having a several times larger amplitude than that of the synchronous vibration was induced by pneumatic hammer instability due to cavitating flow of liquid nitrogen. However, the bearing with a 0.80 mm orifice diameter can be operated at the rotational speed of up to 50,000 rpm without any self-excited vibration. Comparison between the test results and the numerical predictions of rotordynamic coefficients based on the test conditions shows that instability induced by large cross-coupled stiffness coefficients due to fluid rotation is considered to onset at the rotational speed over 50,000 rpm.Therefore, a new hybrid bearing with a higher rotordynamic performance has been designed and manufactured based on the numerical predictions described above. Less
期刊论文(6)
专著(0)
科研奖励(0)
会议论文
菊池 正孝: "DN値300万における極低温ハイブリッドセラミック玉軸受の性能"日本航空宇宙学会北部支部2003年講演会および第4回再使用型宇宙推進系シンポジウム講演論文集. 35-40 (2003)
Masataka Kikuchi:“DN 值为 300 万的低温混合陶瓷球轴承的性能”日本航空学会北方分会 2003 年会议和第四届可重复使用空间推进系统研讨会论文集 35-40(2003 年)。
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高田 仁志: "DN値300万における極低温ハイブリッドセラミック玉軸受の性能"日本航空宇宙学会北部支部2002年講演会および第3回再使用型宇宙推進系シンポジウム. 239-244 (2002)
高田仁:“DN 值为 300 万的低温混合陶瓷球轴承的性能”日本航空航天学会北方分会 2002 年讲座和第三届可重复使用空间推进系统研讨会 239-244(2002 年)。
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三橋 克則: "軸受荷重測定システムの誤差評価"日本航空宇宙学会北部支部2003年講演会および第4回再使用型宇宙推進系シンポジウム講演論文集. 53-58 (2003)
Katsunori Mitsuhashi:“轴承载荷测量系统的误差评估”日本航空学会北方分会2003年会议暨第四届可重复使用空间推进系统研讨会论文集53-58(2003)。
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Study on Instability of Densified Subcooled Liquid Oxygen Cavitating Flows
-
批准号:21560185
-
项目类别:Grant-in-Aid for Scientific Research (C)
-
资助金额:$2.91万
-
财政年份:2009
-
负责人:OIKE Mamoru
-
依托单位:
Study on Vibration Instability Induced by Cavitating Flow in Densified Subcooled Cryogenic Fluids
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批准号:18560177
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$2.46万
-
财政年份:2006
-
负责人:OIKE Mamoru
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依托单位:
Study on Instability of Subcooled Cryogenic Cavitating Flows
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批准号:16560156
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$2.37万
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财政年份:2004
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负责人:OIKE Mamoru
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依托单位:
Study on Instabilities of Cryogenic Two-Phase Flows in a Pipe
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批准号:10450070
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$8.58万
-
财政年份:1998
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负责人:OIKE Mamoru
-
依托单位:
海外基金