In postulatione mundi Aerospace et industria sector machining, in IV-tibita LV °Anguli radius finem molendiniEmersit sicut ludum-verso ad processui calor-repugnant alloys sicut Inconel DCCXVIII et TI-6ALAL-4v. Engineered ad defy ad limitations of Traditional instrumenta, hic dressuges infestantibus geometria, provectus coatings, et inpulsa, repugnans consilio eripere unmatched perficientur in extrema conditiones.
Precisione Engineering ad Unyielding Materials
Quod LV ° per nasum Design ensures meliorem chip evacuatione cum maintaining a acri acutam acies, critica ad obscuratis calor buildup in Nickel-fundatur superalloys. Key innovations includit:
Alcrn / Tisin Hybrid coating: Resistit temperaturis ad 1,100 ° C, reducendo oxidation gerunt per LX% comparari vexillum tialn coatings.
Geometria Geometriam absorbing infringit, asymmetric IV-tibia layout disrupts harmonic vibrationum per intermittitur intermissa (eg, turbine ferrum radix machining).
Super-centrum secans marginibus: plenus imo secans facultatem excludit opus prae-dentura in clausis-sinum operationes.
Probatur in Aerospace Applications
A Jet Engine Component Manufacturer nuntiavit:
LXX% Iustioribus Mors Principium Vita: De XII ad XX partes per ore cum machining Inconel DCCXVIII combustione gazophylacia.
A. 0.8μm superficiem metam: effectum sine secundarium politura.
XXXV% citius feed rates: enabled per XXXV ° Helix angulus et magna core diameter, boosting MRR ad XLV cm³ / min.
Technical Edge
Submicron-gradu molere: ≤2μm ore constantiam per omnes tibia.
0.5mm-16mm diameter range: cum anguli Radii ex R0.2 ad R2.5.
Hsk-63a Shank compatibility, ad summus stabilitatem machining centers.
Nam shops proelia lenta alloys, hocfinis molendiniUltimate fusionem diuturnitatem et praecisione.
Post tempus: Mar-24-2025
