Ire ọkụ penetration Fuel Testing System
Flame Penetration Fuel Testing System for Thermal Insulation and Sound Insulation Material
Product introduction of the Flame Penetration Fuel Testing System
The NexGen ụgbọelu mmanụ ụgbọala burner mma site FAA nke Federal Aviation Administration nke United States ga-eji na mmanụ ụgbọala combustion ule nke ọtụtụ ụgbọelu ihe. Dị ka Park DPL 3400, Lennox Model Ob-32 na Carlin Model 200 CRD mbụ ghọtara site FAA niile e kwụsịrị, FAA azụlitewo na NexGen burner maka ọgbọ ọzọ nke ụgbọelu mmanụ ụgbọala burners. NexGen combustor adopts ọrụ ụkpụrụ nke gara aga ọgbọ combustor, na ike n'ụzọ ziri ezi tụọ ule afọ nke input gas na mmanụ ụgbọala. N'otu oge ahụ, bụ ngwá nwere ike ikwado n'ọdịnihu upgrade nke FAA.
The flame penetration test of thermal insulation and sound insulation materials can be carried out by configuring a flame penetration test device and a dynamic load motion system.
Performance e ji mara
1. burner conical cylinder ka nke corrosion eguzogide na elu okpomọkụ na-eguzogide ọgwụ alloy.
2. NexGen ụgbọelu mmanụ ụgbọala burner agụnye nāpunara, mmanụ nozulu, igniter, mmanụ okporo ígwè, fixer, ventilashion tube na shei, mofla, now na-eguzogide ndị ọzọ mmiri.
3. N'ibu mmanụ ụgbọala mgbali nlele, mmanụ solenoid valvụ, mmanụ okpomọkụ nchọpụta ngwaọrụ, ikuku nduzi valvụ, ikuku okpomọkụ nchọpụta ngwaọrụ.
4. N'ibu gas na ikuku okpomọkụ akara ngwaọrụ ice bath na olu na-erughị 2 x 0,14 m3, na mmanụ ụgbọala okpomọkụ nwere ike na-achịkwa.
5. Site na-agbanwe mmanụ ụgbọala nozulu na ikuku input, dị iche iche ule ụkpụrụ nwere ike zutere.
6. mkpuchi blanket maka cover of burner, ekpuchi mmanụ ụgbọala pipeline na fuselage.
7. The oku okpomọkụ nye site NexGen ụgbọelu mmanụ ụgbọala burner bụ ihe na-erughị: 2000 + 50.
8. NexGen ụgbọelu mmanụ ụgbọala burner nwere ike inye dịghị ihe na-erughị 10.6w / cm2 nke ire ọkụ okpomọkụ eruba.
9. modul Units Iji NexGen burner Support System
10. Arọ-oru ígwè etiti nwere ike arụnyere na ule samples ịgbasapụ na ekwesị.
11. Seven seramiiki-encapsulated, metal n'ọbọ na ebe K-ụdị (nickel-chromium-nickel-aluminum) thermocouples na a dayameta nke 1.6 mm ga-eji maka mmezi. Ha na-eduzi ga nwere mpụga dayameta nke 0,254 mm, a cross-sectional ebe 0,0507 mm2 na a na-eguzogide nke 361_ / km (American waya nlele 30 AWG). The thermocouple ga-ofu na n'akuku ígwè mgbodo na-etolite a thermocouple mbo nke mere na ọ pụrụ enịm na sample mgbodo n'oge mmezi.
12. Kwes radieshon flọksi mmetụta, onwem na obi jụrụ ngwaọrụ, na arụnyere na ofu aka mgbodo.
Product parameters of the Ire ọkụ penetration Fuel Testing System
| size | 1500 mm (W) x 1800 mm (H) x 900 mm |
| ibu | 150KG |
| eletrik chọrọ | 220V, 10a |
| ihere okpomọkụ | 10 ℃ 35 ℃ |
| mmanụ ụgbọala chọrọ | ụgbọelu kerosin |
| gas chọrọ | dịghị ihe na-erughị 120 PSI ikuku Compressor |
| ngwa ebe | Aviation Materials |
| Standard | AITM 2,0056, BSS 7387, nnọọ IKPEHE 25 ODIDE NTụKWASị Ihe F Part VII |
