I loko o ka honua kiʻekiʻe o ka hana aerospace, kahi e wehewehe ai ka micron-level precision i ka kūleʻa, ka Ultra-ThermalPaʻa Paʻa Hoʻoemipuka mai ma ke ano he mea hoololi holoholona. Hoʻolālā ʻia e hoʻopaʻa i ka cylindrical carbide a me nā mea hana HSS me ka pololei h6 shank, hoʻohana kēia mea paʻa i nā dynamics thermal kiʻekiʻe e hāʻawi i ka rigidity a me ka mana holo ʻole, ʻoiai ma 30,000 RPM.
Nā Hana Hou
Kūikawā Heat-Resistant Steel Alloy: Hoʻopili ʻia mai ke kila ISO 4957 HNV3, kū ʻo ia i ka 800 ° C induction heat cycles me ka ʻole o ka hoʻohaʻahaʻa ʻana.
ʻO Submicron Concentricity: ≤0.003mm TIR (Total Indicated Runout) e hōʻoia i ka pau ʻana o ke aniani ma nā lau turbine titanium.
Dynamic Balancing Mastery: Hōʻoia i ka ISO 21940-11 G2.5, e loaʻa ana <1 gmm imbalance ma 30k RPM - koʻikoʻi no ka 5-axis contouring o Inconel 718.
Nā Kūlana ʻenehana
4-Screw Balancing System: Hōʻike ʻia nā hiʻohiʻona i hoʻonui ʻia i nā wili radial e hoʻoponopono maikaʻi i ke kaulike ma hope o ka emi ʻana, e uku ana i ka asymmetry mea hana.
Hoʻomaʻamaʻa Cryogenic: Hoʻopaʻa ka hoʻoheheʻe ʻana ma hope o ka mīkini (-196 ° C) i ke ʻano molekala, e hōʻemi ana i ka neʻe ʻana o ka wela ma 70%.
Nano-Coated Bore: Kāohi ʻo TiSiN i ka hoʻopili ʻana i nā mea i ka wā kiʻekiʻe-frequency wela a me ka hoʻomaha ʻana.
Aerospace Case Study
Ua hōʻike ʻia kahi ʻenekini jet OEM machining compressor disks:
ʻO Ra 0.2µm Hoʻopau ʻili: Hoʻopau ʻia ka hoʻoliʻi ʻana ma hope o ka wili.
Mea Ola + 50%: Hoʻemi ʻia ka haʻalulu i hoʻonui ʻia i ke ola o ka carbide hope mill.
0.001° ʻO ka pololei angular: mālama ʻia ma luna o nā hoʻololi 8-hola.
Nā kikoʻī
Nā ʻano Shank: CAT40, BT30, HSK63A
Māhele Paʻa: Ø3–32mm
ʻO ka wikiwiki loa: 40,000 RPM (HSK-E50)
Hoʻohālikelike ʻia ka Coolant: Ma o-spindle a hiki i 200 bar
ʻO ka wā e hiki mai ana o ka mīkini wikiwiki kiʻekiʻe - kahi e hui ai ka pololei wela me ka hilinaʻi aerospace-grade.
Ka manawa hoʻouna: Mar-27-2025
