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Capabilities

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Our state-of-the-art multi-axis multi-pallet “lights-out” machining cells and highly experienced employees have enabled us to exceed our customers’ ever more critical quality, delivery, and pricing requirements. Tens Machine also has the capability to machine intricate monolithic cross sections over 120″ in length.

Tens Machine maintains a quality system that is ISO 9001 and AS9100 certified and registered.

Through our unique manufacturing processes, Tens Machine has been able to dramatically reduce cost and lead time on critical customer applications.

MAJOR ADVANTAGES:

  • Cost. Lower overhead and modern, efficient equipment run by experienced personnel, contribute to a consistent cost advantage.
  • Quality. We focus on quality and on-time delivery. We are especially proud of our cost-effective solutions to our customers’ complex machining requirements.
  • Delivery. Tens Machine has a track record of meeting delivery requirements, including just-in-time scheduling, and rush or AOG (Aircraft On Ground).
  • Risk Mitigation.
  • Disaster Recovery.
TENS MACHINE CAN PERFORM HOLE COLD EXPANSION PER THE FOLLOWING OEM SPECIFICATIONS AND BEYOND…

  • Bell Helicopter BPS-4592
  • Boeing &n bsp; BAC 5973
  • Boeing BAC 5768
  • Douglas DPS 3.67-74
  • Fairchild &nb sp; A-F302
  • Grumman GSS15350
  • IAI Israel PS55.1180
  • Lockheed General Dynamics FPS-3030
  • Lockheed General Dynamics &nbs p; FPS-3064
  • Lockheed General Dynamics FPS-3066
  • Lockheed STP52-715
  • McDonnell PS. 19180
  • Northrop & nbsp; FH-56
  • Sikorsky SS5098
Benefits of Split Sleeve Cold Expansion

  1. In most cases, at least 3:1 fatigue life improvement
  2. Arrests small crack growth
  3. Cost effective alternative to redesign
  4. Adds no weight to structure
  5. Simple, one-sided operation
  6. Works on all common aerospace materials

Tens Machine Machine can handle :

  • Any sizes..
  • Any specifications.
  • Any materials.
  • We can supply the completed machined part and the cold working operation/final hole sizing.
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