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This study delves into the analysis of cutting forces in axial-compliant systems,
focusing specifically on the comparison between axially spring-compensated 90° conical tools and
rigid chamfering tools. The research incorporates a predictive model for chamfer size calculation in
the axially spring-compensated tools, verified through experimental tests on representative parts. The
study aims to control chamfer size within tolerances by adjusting process conditions and optimizing
processing efficiency. By exploring the fundamentals of the chamfering process, this research offers
insights into breaking sharp edges on components with positional errors and shape deformations,
with a particular emphasis on aero-engine casings. The integration of theoretical modelling and
experimental validation enhances the understanding of force performance, chamfer size, and process
parameters such as feeds and cutting speed. Through the use of representative test parts made of
Inconel 718, commonly used in aero-engine manufacturing, this work contributes to advancing the
knowledge and practical applications in chamfering operations and edge finishing in the
manufacturing industry.
 

  • Internet havola
  • DOI
  • UzSCI tizimida yaratilgan sana 16-08-2024
  • O'qishlar soni 31
  • Nashr sanasi 14-08-2024
  • Asosiy tilIngliz
  • Sahifalar70-75
English

This study delves into the analysis of cutting forces in axial-compliant systems,
focusing specifically on the comparison between axially spring-compensated 90° conical tools and
rigid chamfering tools. The research incorporates a predictive model for chamfer size calculation in
the axially spring-compensated tools, verified through experimental tests on representative parts. The
study aims to control chamfer size within tolerances by adjusting process conditions and optimizing
processing efficiency. By exploring the fundamentals of the chamfering process, this research offers
insights into breaking sharp edges on components with positional errors and shape deformations,
with a particular emphasis on aero-engine casings. The integration of theoretical modelling and
experimental validation enhances the understanding of force performance, chamfer size, and process
parameters such as feeds and cutting speed. Through the use of representative test parts made of
Inconel 718, commonly used in aero-engine manufacturing, this work contributes to advancing the
knowledge and practical applications in chamfering operations and edge finishing in the
manufacturing industry.
 

№ Havola nomi
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