dc.contributor.author |
Adgamov R. |
|
dc.contributor.author |
Dmitriev S. |
|
dc.contributor.author |
Khairullin A. |
|
dc.date.accessioned |
2018-09-18T20:18:06Z |
|
dc.date.available |
2018-09-18T20:18:06Z |
|
dc.date.issued |
2012 |
|
dc.identifier.issn |
1068-7998 |
|
dc.identifier.uri |
https://dspace.kpfu.ru/xmlui/handle/net/138478 |
|
dc.description.abstract |
The quality control system for an aircraft engine that is continuously developed in the life cycle stages is considered. Main quality indicators and their control methodology are analyzed. The computer-aided tests are substantiated as part of the quality control system and their generalized technological process structure and its construction methodology are proposed. © 2012 Allerton Press, Inc. |
|
dc.relation.ispartofseries |
Russian Aeronautics |
|
dc.subject |
computer-aided test system |
|
dc.subject |
quality control system |
|
dc.subject |
quality indicators |
|
dc.title |
Computer-aided tests in the quality control system of aircraft engines |
|
dc.type |
Article |
|
dc.relation.ispartofseries-issue |
1 |
|
dc.relation.ispartofseries-volume |
55 |
|
dc.collection |
Публикации сотрудников КФУ |
|
dc.relation.startpage |
101 |
|
dc.source.id |
SCOPUS10687998-2012-55-1-SID84861686429 |
|