Orbital Cutting Tool with Axially Varying Edge Spacing
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Solution Overview
Problem
Conventional orbital drilling techniques often experience resonant coupling and vibrations due to regular spacing of cutting edges, which can lead to inefficiencies and poor control when drilling through composite materials like carbon fiber-reinforced polymers and stacks of different materials.
Innovation Solution
A cutting tool with cutting edges arranged in alternating helix angles along its longitudinal axis, where the circumferential spacing between adjacent edges varies axially, disrupting regular frequency coupling and reducing resonant vibrations by applying forces intermittently and at different angles.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of manufacture
If cutting edges are spaced at regular intervals around the circumference, then the cutting tool maintains simple manufacturing and consistent cutting pattern, but resonant coupling and vibrations occur at regular frequencies that couple to workpiece natural vibration frequencies
Solution Approach 1:
The patent applies asymmetry by varying the circumferential spacing between adjacent cutting edges along the helical path. Instead of equal spacing, the cutting edges are positioned at unequal intervals, which disrupts the regular frequency generation during orbital drilling. This asymmetric spacing prevents the formation of consistent vibrational frequencies that could couple with the workpiece's natural frequencies, thereby reducing resonant coupling and chatter while maintaining manufacturing feasibility.
2Stability of the object's composition
If cutting edges are uniformly distributed, then the cutting forces are evenly distributed, but resonant coupling develops due to regular frequency patterns matching workpiece natural frequencies
Solution Approach 1:
The patent applies local quality by creating non-uniform spacing between cutting edges at specific locations along the helical path. While the overall distribution remains balanced, the local spacing variations disrupt the regular frequency patterns that cause resonant coupling. This allows the cutting forces to remain generally distributed while introducing local irregularities that prevent resonance, thus maintaining stability without triggering harmful vibrational frequencies.
3Device complexity
If regular spacing is used between cutting edges, then the tool design is simple and consistent, but vibrations occur that lead to poor control and inefficiencies when drilling through composite materials
Solution Approach 1:
The patent applies dynamics by introducing variable spacing between cutting edges along the helical path, transforming the static uniform pattern into a dynamic non-uniform distribution. This dynamic spacing variation disrupts the regular frequency generation during orbital drilling, preventing resonant coupling and vibrations. The result is improved drilling efficiency and control through composite materials while maintaining relatively simple tool design, as the spacing variation can be incorporated into the standard tool manufacturing process.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
This design effectively inhibits resonant vibrations, allowing for more precise and efficient drilling through composite materials with reduced chip generation and heat, enabling the creation of holes with larger diameters than the drill bit, and maintaining a smooth finish without the need for extensive clean-up.
Implementation Method 1
During orbital drilling it is possible for resonances to develop through 'resonant coupling' where the workpiece or machine tool system has a natural vibration frequency that is driven by the cutting tool
Data Source
AI summary
A cutting tool for use in an orbital drilling machine may include a cutting-tool body having a longitudinal axis and a plurality of cutting edges supported on the cutting-tool body and distributed circumferentially around the cutting-tool body. Each cutting edge may extend along the longitudinal axis in a respective helix. A circumferential spacing may be defined between each pair of circumferentially adjacent cutting edges for each position of the longitudinal axis along which the cutting edges extend. The circumferential spacing between at least first and second cutting edges of the plurality of cutting edges may be different at spaced-apart first and second positions along the longitudinal axis.
