Отрывок: Wing: cracks in tail part of wing, landing gear compartments doors, in wing fences; leakage fuel tanks placed in wing. Tail unit, control surfaces and wing high-lift devices: cracks in skin; tearing frictionless or slider bearing in hinges fitting; turning bearing cup in hinges fitting. Landing gear: cracks in welded seams and pin hinges landing gear; cracks in shock strut piston; deterioration and teases in shock strut bear...
Полная запись метаданных
Поле DC | Значение | Язык |
---|---|---|
dc.contributor.author | Mrykin S. V. | ru |
dc.contributor.author | Mrykin S. V. | ru |
dc.contributor.author | The Ministry of Education and Science of the Russian Federation | ru |
dc.contributor.author | Samara State Aerospace University (National Research University) | ru |
dc.coverage.spatial | самолетные системы | ru |
dc.coverage.spatial | функциональные отказы | ru |
dc.coverage.spatial | последствия функциональных отказов | ru |
dc.creator | Mrykin S. V. | ru |
dc.date.issued | 2011 | ru |
dc.identifier | RU/НТБ СГАУ/WALL/629.7.05/M 10-217066 | ru |
dc.identifier.citation | Mrykin, S. V. Functional Failure Effects Airplane Systems [Электронный ресурс] : Electronic Manual / S. V. Mrykin ; [tr. S. V. Mrykin] ; The Ministry of Education and Science of the Russian Federation, Samara State Aerospace University (National Research University). - Samara, 2011. - on-line | ru |
dc.description.abstract | Труды сотрудников СГАУ(электрон. версия). | ru |
dc.description.abstract | Используемые программы: Adobe Acrobat. | ru |
dc.description.abstract | Attributes classification of aircraft systems by failure effect, list and attributes special situations, arising owing to failures system according to AR-25 [1] are presented in the manual. List typical failures and examples of classification for special | ru |
dc.format.extent | Electronic text (1 файл : 367,0 Kb) | ru |
dc.language.iso | rus | ru |
dc.relation.isformatof | Functional Failure Effects Airplane Systems [Электронный ресурс] : Electronic Manual | ru |
dc.title | Functional Failure Effects Airplane Systems | ru |
dc.type | Text | ru |
dc.subject.rugasnti | 55.47 | ru |
dc.subject.udc | 629.7.05 | ru |
dc.textpart | Wing: cracks in tail part of wing, landing gear compartments doors, in wing fences; leakage fuel tanks placed in wing. Tail unit, control surfaces and wing high-lift devices: cracks in skin; tearing frictionless or slider bearing in hinges fitting; turning bearing cup in hinges fitting. Landing gear: cracks in welded seams and pin hinges landing gear; cracks in shock strut piston; deterioration and teases in shock strut bear... | - |
Располагается в коллекциях: | Методические издания |
Файлы этого ресурса:
Файл | Описание | Размер | Формат | |
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Mrykin S. V.Functional Failure.pdf | from 1C | 367.87 kB | Adobe PDF | Просмотреть/Открыть |
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