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TC4 Aerospace Milling Case

Coating validation trial on an aircraft reinforcement frame, leading to a 300-insert customer retest request.

4 HOURS

Best internal validation result

300 INSERTS

Best internal validation result

3 OPTIONS

Best internal validation result

PROJECT BACKGROUND

An internal coating-validation trial for a TC4 milling application.

This trial was part of an internal coating-validation process for a customer’s TC4 rough-milling application on an aircraft reinforcement frame at HRC 30. Before moving to a customer batch test, we compared three Premitools coating options against an incumbent insert that recorded 2-3 hours of tool life. The objective was to identify a more wear-resistant option without changing the listed cutting conditions.

WORKPIECE

Aircraft Reinforcement Frame

MATERIAL

TC4 · HRC 30

OPERATION

Rough Milling

INCUMBENT LIFE

2–3 hours

A Controlled Internal Benchmark Before Customer Batch Testing.

Built an internal benchmark: Vc 47 m/min, feed 1.17 as recorded, and ap 0.6 mm.

Screened three Premitools options: TP1815-TF, TP1815-TIS and TP1815 with SDMT090307-SM inserts.

Selected evidence for the next step: recorded tool life, cutting resistance at the change point, and post-test wear images.

Recorded Results

Tool / gradeInsert modelBrand originRecorded life
CompetitorSDMT0903China2-3 h
Premitools / TP1815-TFSDMT090307-SMChina3 h 40 min
Premitools / TP1815-TISSDMT090307-SMChina4 h
Premitools / TP1815SDMT090307-SMChina2 h 50 min

Recorded Outcome: The TF and TIS coating variants showed improved wear resistance. The report states an overall 25-30% improvement for the new coatings; the longest individual recorded life was 4 hours. The initial result supported moving to a customer small-batch retest.

CUSTOMER RESPONSE

After reviewing the initial validation results, the customer requested a small batch of 300 inserts for a second-round test.

This is a verified follow-up action, not a direct customer quotation.