REG NASA-LLIS-1222--1998 Lessons Learned - Understanding specific operational characteristics of selected design options (threaded Inserts).pdf

上传人:ideacase155 文档编号:1018861 上传时间:2019-03-21 格式:PDF 页数:2 大小:12.83KB
下载 相关 举报
REG NASA-LLIS-1222--1998 Lessons Learned - Understanding specific operational characteristics of selected design options (threaded Inserts).pdf_第1页
第1页 / 共2页
REG NASA-LLIS-1222--1998 Lessons Learned - Understanding specific operational characteristics of selected design options (threaded Inserts).pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、Lessons Learned Entry: 1222Lesson Info:a71 Lesson Number: 1222a71 Lesson Date: 1998-09-30a71 Submitting Organization: JSCa71 Submitted by: John P. Badalich Jr./ Ronald A. MontagueSubject: Understanding specific operational characteristics of selected design options (threaded Inserts) Description of

2、Driving Event: Galling of threaded fasteners was experienced in the qualification test program of the Z1 Truss. Fasteners intended to be removable on-orbit galled during test. The fasteners were installed in locking threaded inserts (“KEEN“ type).Root cause: The inherent effect of the “Keen“-type, u

3、pset thread design is to bite hard into the fastener. After repeated installation and removal, the fastener will gall. These inserts work best engaged once, and are excellent in this application.Lesson(s) Learned: A full understanding of the intent of a design is mandatory to ensure that operational

4、 requirements can be metRecommendation(s): If threaded inserts of this type must be used, “condition“ the insert first with a sacrificial bolt of the same type. The sacrificial bolt will cold work the upset thread slightly to help mitigate the probability of galling during repeated use. Lab analysis

5、 of this cold working procedure was performed; results are available from the lesson initiator. Evidence of Recurrence Control Effectiveness: N/AProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Documents Related to Lesson: N/AMission Directorate(s): N

6、/AAdditional Key Phrase(s): a71 Parts Materials & Processesa71 Procurement Small Business & Industrial Relationsa71 Risk Management/Assessmenta71 Test & Verificationa71 Test ArticleAdditional Info: Approval Info: a71 Approval Date: 2002-06-27a71 Approval Name: Ronald A. Montaguea71 Approval Organization: JSCa71 Approval Phone Number: 281-483-8576Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 4538-1-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Narrow Series Dimensi.pdf AECMA PREN 4538-1-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Narrow Series Dimensi.pdf
  • AECMA PREN 4538-2-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Narrow Series Dimensi.pdf AECMA PREN 4538-2-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Narrow Series Dimensi.pdf
  • AECMA PREN 4539-1-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Wide Series Dimension.pdf AECMA PREN 4539-1-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Wide Series Dimension.pdf
  • AECMA PREN 4539-2-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Wide Series Dimension.pdf AECMA PREN 4539-2-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Wide Series Dimension.pdf
  • AECMA PREN 4540-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Technical Specification.pdf AECMA PREN 4540-2001 Aerospace Series Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner Elevated Load under Low Oscillations Technical Specification.pdf
  • AECMA PREN 4545-2000 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Plate 20 mm Less Than or Equal to a Less Than or Equal to 50 mm 1 080 MPa Less Tha.pdf AECMA PREN 4545-2000 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Plate 20 mm Less Than or Equal to a Less Than or Equal to 50 mm 1 080 MPa Less Tha.pdf
  • AECMA PREN 4549-2000 Aerospace Series Pipe Coupling in Heat Resisting Steel or in Heat Resisting Nickel Alloy Coupling End Welded Design Configuration Inch Series Edition P 1《航空航天系.pdf AECMA PREN 4549-2000 Aerospace Series Pipe Coupling in Heat Resisting Steel or in Heat Resisting Nickel Alloy Coupling End Welded Design Configuration Inch Series Edition P 1《航空航天系.pdf
  • AECMA PREN 4550-1-2000 Aerospace Series Pipe Coupling 37 Degree Spherical Design Configuration Inch Series Part 1 Male Sealing Ends Edition P 1《航空航天系列管接头 37度 球面设计配置英寸系列.第1部分 男密封完 P.pdf AECMA PREN 4550-1-2000 Aerospace Series Pipe Coupling 37 Degree Spherical Design Configuration Inch Series Part 1 Male Sealing Ends Edition P 1《航空航天系列管接头 37度 球面设计配置英寸系列.第1部分 男密封完 P.pdf
  • AECMA PREN 4550-2-2000 Aerospace Series Pipe Coupling 37 Degree Design Configuration Inch Series Part 2 Port Ends Edition P 1《航空航天系列管接头37度 设计配置系列 P.第1版》.pdf AECMA PREN 4550-2-2000 Aerospace Series Pipe Coupling 37 Degree Design Configuration Inch Series Part 2 Port Ends Edition P 1《航空航天系列管接头37度 设计配置系列 P.第1版》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1