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Study on Cryogenic Hybrid Journal Bearings for Rocket Thrbopumps

Study on Cryogenic Hybrid Journal Bearings for Rocket Thrbopumps
火箭血栓泵低温混合轴颈轴承的研究
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

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中文摘要
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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)
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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
  • 批准号:
    18560177
  • 项目类别:
    Grant-in-Aid for Scientific Research (C)
  • 资助金额:
    $2.46万
  • 财政年份:
    2006
  • 负责人:
    OIKE Mamoru
  • 依托单位:
Study on Instability of Subcooled Cryogenic Cavitating Flows
  • 批准号:
    16560156
  • 项目类别:
    Grant-in-Aid for Scientific Research (C)
  • 资助金额:
    $2.37万
  • 财政年份:
    2004
  • 负责人:
    OIKE Mamoru
  • 依托单位:
Study on Instabilities of Cryogenic Two-Phase Flows in a Pipe
  • 批准号:
    10450070
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
  • 资助金额:
    $8.58万
  • 财政年份:
    1998
  • 负责人:
    OIKE Mamoru
  • 依托单位:
海外基金