首页> 外文会议>12th European space mechanisms and tribology symposium (ESMATS 2007) >Effect of Ceramic Ball and Hybrid Stainless Steel Bearing/Wheel Combinations on the Lifetime of a Precision Translation Stage for the SIM Flight Project
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Effect of Ceramic Ball and Hybrid Stainless Steel Bearing/Wheel Combinations on the Lifetime of a Precision Translation Stage for the SIM Flight Project

机译:陶瓷球和不锈钢轴承/轮毂组合对SIM飞行项目精密平移台寿命的影响

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摘要

A study of hybrid material couples using the SpiralrnOrbit Tribometer (SOT) [1]-[3] was initiated torninvestigate both lubricated (Pennzane~? X2000 andrnBrayco? 815Z) and unlubricated Si3N4, 440C SS, Rexrn20, Cronidur X30 and X40 plates with Cerbec SN-101-rnC (Si3N4) and 440 C balls. The hybrid wheel/bearingrnassembly (Figure 2) will be used on the Linear OpticalrnDelay Line (LODL) stage (Figure 1) as an element ofrnthe NASA Space Interferometry Mission (SIM). SIMrnis an orbiting interferometer linking a pair telescopesrnwithin the spacecraft and, by using an interferometryrntechnique and several precision optical stages, is ablernto measure the motions of known stars much betterrnthan current ground or space based system. Thisrnmeasurement will provide the data to "infer" thernexistence of any planets, undetectable by otherrnmethods, orbiting these known stars.rnThe LODL is a motor driven, band drive rail systemrncarrying a Corner Cube Retro-Reflector Carriagernsystem running on a 1.54 m guide rail system wasrnconceptualized. Three Integrated Hybrid DuplexrnAngular Contact Bearing Wheel Assemblies (Figurern2), running on the precision rail system, are used tornlocate the carriage system on the rail, with preloadrnwheel assemblies opposite to these assemblies. Thernrequirement is a 5-year mission lifetime with a goal ofrn10 years total, using little or no lubricant in order tornreduce contamination to the nearby optics. The SOTrnresult indicates accelerated lubricant consumption raternbetween the ceramic ball and 440C SS and 52100rnbearing steel, but promising trend with the newerrnCronidur X30 and X40 bearing steel. The use of dryrnor no lubricant will require further investigation.
机译:开始使用SpiralrnOrbit摩擦计(SOT)[1]-[3]对混合材料对进行研究,以研究润滑的(Pennzane〜X2000和rnBrayco?815Z)和未润滑的Si3N4、440C SS,Rexrn20,Cronidur X30和X40带有Cerbec的板SN-101-rnC(Si3N4)和440 C球。混合车轮/轴承组件(图2)将在线性光学延迟线(LODL)平台(图1)上使用,作为NASA空间干涉测量任务(SIM)的一个组成部分。 SIMRIS是一种轨道干涉仪,它连接航天器内的一对望远镜,并且通过使用干涉测量技术和多个精密光学平台,能够测量已知恒星的运动,其效果要比当前的地面或太空系统好得多。该测量将提供数据,以“推断”其他方法无法探测到的绕过这些已知恒星运行的任何行星的存在。LODL是一种电动机驱动的带驱动导轨系统,其搭载在1.54 m导轨系统上运行的角锥后向反射镜架系统,这在概念上被概念化了。在精密导轨系统上运行的三个集成式混合双工角接触轴承轮组件(图rn2)用于将滑架系统定位在导轨上,而预载轮组件与这些组件相对。要求是5年的任务寿命,目标是总共10年,几乎不使用润滑剂或不使用润滑剂,以减少对附近光学器件的污染。 SOT结果表明,陶瓷球与440C SS和52100rn轴承钢之间的润滑剂消耗速率加快了,但是对于更新的Cronidur X30和X40轴承钢,趋势却是乐观的。使用干燥剂或无润滑剂将需要进一步研究。

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  • 会议地点 Liverpool(GB);Liverpool(GB)
  • 作者单位

    NASA Jet Propulsion Laboratory (reference CL#07-2072 dated July 9, 2007) Northrop Grumman Space Technology One Space Park, R9-1944, Redondo Beach, CA 90278, USA, E-mail: John.Lo@ngc.com;

    rnJPL, 4800 Oak Grove Dr., Pasadena, CA 91109, USA, E-mail: Kerry.Klein@jpl.nasa.gov;

    rnSest, Inc., 18000 Brookpark Road Suite 104, Brookpark, OH 44130, USA, Email: william.r.jones@grc.nasa.gov;

    rnUniversity of Toledo, 2801 W. Bancroft St, Toledo, OH 43606, USA, Email: mark.jansen@grc.nasa.gov;

    rnCerobear GmbH, Kaiserstrasse 100, 52134 Herzogenrath, Deutschland, E-mail: JeWem@cerobear.de;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 飞行力学 ;
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