درباره ما
MIL-DTL-87218E
CABLE, LOCKCLAD, FOR AIRCRAFT CONTROL
Organization:
DLA - GS5 - DLA Aviation - Richmond
Year: 2012
Abstract: This specification covers the requirements for lockclad control cable material used in aircraft flight controls and aircraft control cable assemblies that include lockclad as a portion of the assembly. Lockclad is defined as the resulting material of swaging aluminum alloy tubing onto MIL-DTL-83420, type I, nonjacketed wire rope to the extent necessary to comply with the elongation and coefficient of thermal expansion properties specified herein.Intended Use: The lockclad control cable assemblies and lockclad material covered by this specification are intended for use in aircraft control cable systems where low elongation under tension loads and/or a coefficient of thermal expansion more nearly matching that of a basically aluminum airframe is desired or required. Where these factors are not significant, unclad wire rope per MIL-DTL-83420 may be used for avoidance of the weight penalty of lockclad.
Collections
:
Show full item record
| contributor author | DLA - GS5 - DLA Aviation - Richmond | |
| date accessioned | 2017-09-04T18:00:31Z | |
| date available | 2017-09-04T18:00:31Z | |
| date copyright | 09/27/2012 | |
| date issued | 2012 | |
| identifier other | FWWKZEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsessionid=47037D83FCDCAC426159DD6E273C9FCD/handle/yse/183552 | |
| description abstract | This specification covers the requirements for lockclad control cable material used in aircraft flight controls and aircraft control cable assemblies that include lockclad as a portion of the assembly. Lockclad is defined as the resulting material of swaging aluminum alloy tubing onto MIL-DTL-83420, type I, nonjacketed wire rope to the extent necessary to comply with the elongation and coefficient of thermal expansion properties specified herein.Intended Use: The lockclad control cable assemblies and lockclad material covered by this specification are intended for use in aircraft control cable systems where low elongation under tension loads and/or a coefficient of thermal expansion more nearly matching that of a basically aluminum airframe is desired or required. Where these factors are not significant, unclad wire rope per MIL-DTL-83420 may be used for avoidance of the weight penalty of lockclad. | |
| language | English | |
| title | MIL-DTL-87218E | num |
| title | CABLE, LOCKCLAD, FOR AIRCRAFT CONTROL | en |
| type | standard | |
| page | 15 | |
| status | Active | |
| tree | DLA - GS5 - DLA Aviation - Richmond:;2012 | |
| contenttype | fulltext |