AVIA AVIATURN 35 CNC LATHE

AVIA AVIATURN 35 AVIA AVIATURN 35 CNC LATHE equipment image

Equipment Overview

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OEM
AVIA
Model
AVIATURN 35
Year of Manufacture
-
Category
CNC LATHES

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Technical Description

This CNC lathe features an 8.27-inch chuck and a maximum bar capacity of 2.56 inches, making it suitable for medium-sized workpieces. It operates on 2 axes (X and Z), ideal for performing precise turning operations along diameter and length dimensions. The machine is powered by a 20.1 hp motor, achieving up to 5,000 RPM spindle speed, enabling efficient machining of various materials. With a maximum turning diameter of 13.78 inches and a swing of 22.05 inches, it accommodates relatively large-diameter parts up to these dimensions. The machining length capacity extends to 23.62 inches, allowing for the production of sizable parts. The lathe includes a tailstock to support longer workpieces during machining, enhancing precision and stability, but it lacks live tooling and a sub-spindle, indicating it is optimized for conventional turning operations without milling or secondary spindle functions. Control is provided via CNC with two advanced system options: FANUC 0i-TF with a 15" Manual Guide i interface or SIEMENS Sinumerik 828D with a 15" ShopTurn 3D interface, both offering high precision, user-friendly programming, and modern CNC capabilities for consistent, repeatable production. This configuration suits manufacturers requiring accurate, reliable 2-axis turning with moderate power and size capacity for general industrial applications and prototyping.

Technical Attributes

Max Spindle Speed
5000 RPM
Max Swing
22.05 ''
Spindle Bore Diameter
2.56 ''

Data Accuracy and Verification

Specifications and technical details are compiled from manufacturer documentation, historical records, and third-party industry sources. While care is taken to ensure accuracy, this information is provided for reference purposes only and may contain errors or omissions. Users should independently verify all details before relying on them.

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