Burn-through responses of aero-engine nacelle using fiber metal composites by ISO2685 propane-air burner
The paper presents experimental investigation on the behavior and burn through responses of a flat plate composite of fiber-metal laminates composites of aluminum alloy 2024-T3 with carbon and natural fibers subjected to environmental conditions in fire designated zone of an aircraft engine exposed...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Blue Eyes Intelligence Engineering & Sciences Publication
2019
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| Online Access: | http://psasir.upm.edu.my/id/eprint/80845/ http://psasir.upm.edu.my/id/eprint/80845/1/FIBER.pdf |
| _version_ | 1848858965812707328 |
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| author | Mohammed, Ibrahim Abu Talib, Abd. Rahim |
| author_facet | Mohammed, Ibrahim Abu Talib, Abd. Rahim |
| author_sort | Mohammed, Ibrahim |
| building | UPM Institutional Repository |
| collection | Online Access |
| description | The paper presents experimental investigation on the behavior and burn through responses of a flat plate composite of fiber-metal laminates composites of aluminum alloy 2024-T3 with carbon and natural fibers subjected to environmental conditions in fire designated zone of an aircraft engine exposed to fire. The main purpose of this study is to know the different burn through time responses of different forms of aluminum alloy with synthetic and natural fibers. The composites were designed and developed to improve the flame fire resistance in a fire designated zone of an aircraft engine in near future for prolonged burning through time that will at least withstand the fire flame for 15 minutes according to the ISO 2685 standard. The composites are fabricated by hand lay-up method in a mold of 300 mm x 300 mm and compressed by compression machine. Based on the obtained results, some of the composites are indicated to be fireproof while some others are fire resistant. It is shown that the carbon fiber reinforced aluminum alloy laminate with only aluminum at top and bottom (CF+AA) of the composites can resist more flame temperature than the carbon fiber reinforced aluminum alloy laminate with alternate layers of aluminum and carbon fiber (CARALL) with 7.86%, the sandwich of carbon fiber with flax with 18.2% and the sandwich of carbon fiber with kenaf with 23.43%. In conclusion, the study reveals that aluminum alloy 2024-T3 with carbon fiber and some types of natural fibers composites possess good properties of resisting high temperature of fire designated zone of an aircraft engine nacelle. |
| first_indexed | 2025-11-15T12:21:50Z |
| format | Article |
| id | upm-80845 |
| institution | Universiti Putra Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-15T12:21:50Z |
| publishDate | 2019 |
| publisher | Blue Eyes Intelligence Engineering & Sciences Publication |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | upm-808452020-10-15T21:45:31Z http://psasir.upm.edu.my/id/eprint/80845/ Burn-through responses of aero-engine nacelle using fiber metal composites by ISO2685 propane-air burner Mohammed, Ibrahim Abu Talib, Abd. Rahim The paper presents experimental investigation on the behavior and burn through responses of a flat plate composite of fiber-metal laminates composites of aluminum alloy 2024-T3 with carbon and natural fibers subjected to environmental conditions in fire designated zone of an aircraft engine exposed to fire. The main purpose of this study is to know the different burn through time responses of different forms of aluminum alloy with synthetic and natural fibers. The composites were designed and developed to improve the flame fire resistance in a fire designated zone of an aircraft engine in near future for prolonged burning through time that will at least withstand the fire flame for 15 minutes according to the ISO 2685 standard. The composites are fabricated by hand lay-up method in a mold of 300 mm x 300 mm and compressed by compression machine. Based on the obtained results, some of the composites are indicated to be fireproof while some others are fire resistant. It is shown that the carbon fiber reinforced aluminum alloy laminate with only aluminum at top and bottom (CF+AA) of the composites can resist more flame temperature than the carbon fiber reinforced aluminum alloy laminate with alternate layers of aluminum and carbon fiber (CARALL) with 7.86%, the sandwich of carbon fiber with flax with 18.2% and the sandwich of carbon fiber with kenaf with 23.43%. In conclusion, the study reveals that aluminum alloy 2024-T3 with carbon fiber and some types of natural fibers composites possess good properties of resisting high temperature of fire designated zone of an aircraft engine nacelle. Blue Eyes Intelligence Engineering & Sciences Publication 2019-11 Article PeerReviewed text en http://psasir.upm.edu.my/id/eprint/80845/1/FIBER.pdf Mohammed, Ibrahim and Abu Talib, Abd. Rahim (2019) Burn-through responses of aero-engine nacelle using fiber metal composites by ISO2685 propane-air burner. International Journal of Recent Technology and Engineering, 8 (4). pp. 9235-9238. ISSN 2277-3878 https://www.ijrte.org/wp-content/uploads/papers/v8i4/D9224118419.pdf 10.35940/ijrte.D9224.118419 |
| spellingShingle | Mohammed, Ibrahim Abu Talib, Abd. Rahim Burn-through responses of aero-engine nacelle using fiber metal composites by ISO2685 propane-air burner |
| title | Burn-through responses of aero-engine nacelle using fiber metal composites by ISO2685 propane-air burner |
| title_full | Burn-through responses of aero-engine nacelle using fiber metal composites by ISO2685 propane-air burner |
| title_fullStr | Burn-through responses of aero-engine nacelle using fiber metal composites by ISO2685 propane-air burner |
| title_full_unstemmed | Burn-through responses of aero-engine nacelle using fiber metal composites by ISO2685 propane-air burner |
| title_short | Burn-through responses of aero-engine nacelle using fiber metal composites by ISO2685 propane-air burner |
| title_sort | burn-through responses of aero-engine nacelle using fiber metal composites by iso2685 propane-air burner |
| url | http://psasir.upm.edu.my/id/eprint/80845/ http://psasir.upm.edu.my/id/eprint/80845/ http://psasir.upm.edu.my/id/eprint/80845/ http://psasir.upm.edu.my/id/eprint/80845/1/FIBER.pdf |