Emhlabeni wezinga eliphezulu wokwenziwa kwe-aerospace, lapho ukunemba kwezinga le-micron kuchaza impumelelo, i-Ultra-ThermalI-Shrink Fit Holderlivela njengoshintsho lomdlalo. Idizayinelwe ukubopha i-cylindrical carbide namathuluzi e-HSS anonemba we-h6 shank, lesi sibambi sisebenzisa amandla ashisayo athuthukisiwe ukuletha ukuqina okungenakuqhathaniswa nokulawula ukuphuma, ngisho naku-30,000 RPM.
I-Core Innovations
I-Special Heat-Resistant Steel Alloy: Yakhiwe ngensimbi ye-ISO 4957 HNV3, imelana nomjikelezo wokushisisa ongeniswayo ongu-800°C ngaphandle kokuwohloka kwesakhiwo.
I-Submicron Concentricity: ≤0.003mm TIR (Ingqikithi Ekhonjisiwe Yokuphela) iqinisekisa ukuqedwa kwesibuko kumablade e-titanium turbine.
I-Dynamic Balancing Mastery: Iqinisekiswe ku-ISO 21940-11 G2.5, ifinyelela <1 gmm ukungalingani ku-30k RPM - okubalulekile ku-5-axis contouring ye-Inconel 718.
Ukuthuthukiswa Kwezobuchwepheshe
Isistimu Yokulinganisa Ye-4-Screw: Amamodeli anwetshiwe afaka izikulufu zeradial ukulungisa kahle ibhalansi ngemva kokuncipha, okunxephezela i-asymmetry yamathuluzi.
Ukwelashwa kwe-Cryogenic: I-post-machining deep-freeze (-196°C) iqinisa ukwakheka kwamangqamuzana, inciphisa ukukhukhuleka okushisayo ngama-70%.
I-Nano-Coated Bore: Ukugqoka kwe-TiSiN kuvimbela ukunamathela kwempahla phakathi nemijikelezo yokushisa / yokupholisa ephezulu.
Isifundo se-Aerospace
Injini yejethi ye-OEM yokwenza ama-compressor disks ibikiwe:
I-Ra 0.2µm Surface Finish: Kuqedwe ukupholishwa kwe-post-mill.
Impilo Yethuluzi +50%: Kuncishiswe ukudlidliza okunwetshiwe ubude bokuphila komshini wokuphela kwe-carbide.
0.001° Ukunemba kwe-Angular: Igcinwe ngaphezu kwamashifu wamahora angu-8.
Imininingwane
Izinhlobo zeShank: CAT40, BT30, HSK63A
Ibanga lokubamba: Ø3–32mm
Isivinini esikhulu: 40,000 RPM (HSK-E50)
Ukuvumelana kokupholisa: ngokusebenzisa-spindle kufika ku-200 bar
Ikusasa Lomshini Wejubane Eliphezulu - lapho ukunemba okushisayo kuhlangabezana nokuthembeka kwebanga le-aerospace.
Isikhathi sokuthumela: Mar-27-2025
