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ACES Systems - Simple Solutions to Complex Aviation Vibration Problems

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DI 137 TABS Analyzer Balancing System

The DI 137 TABS Automated Tracking Analyzer Balancer System (ATABS) is a complete solution to portable vibration analysis, simplifying helicopter and fixed-wing maintenance tasks while increasing aircraft performance.

ROTOR BLADE TRACKING

Rotor blade tip path corrections and lead/lag characteristics can be measured either day or night, using the optional line scan camera on the DI 137 TABS.

BALANCING
  • Single- and Dual-plane balancing
  • Discrete Fourier Transform (DFT) calculates phase angle and amplitude of the imbalance
  • Rotor smoothing algorithms provide simultaneous, multiple-maintenance adjustments
VIBRATION SIGNATURE

Fast Fourier Transform (DFT) and 4-channel simultaneous data acquisition capabilities are employed to yield fast, accurate vibration analysis results.

DURABLE

ATABS is intended for use in harsh and demanding environments and has been designed to meet:

  • Environmental Requirements of MIL-STD-810D
  • Shock and Vibration Requirements of MIL-STD-810D
  • EMI Requirements of MIL-STD-810D

 

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CONTACT YOUR SALES REP
DI 137 TABS
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  • FEATURES
  • SPECIFICATIONS
  • APPLICATIONS
  • ACCESSORIES
  • Your needs are unique and our sales team is ready to create the kit you need to eliminate your vibration problems.
    Take the first step by filling out the Quote Request Form below.

    Our sales team will contact you to learn more about your needs and provide you with a comprehensive quote to get you on the path to smooth flying.
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  • Fast, 4-Channel Simultaneous Data Collection
  • Large, Easy-to-Read Color Display
  • Compact, Lightweight, Rugged Construction
  • Flight Line Viewable in Direct Sunlight
  • Time proven VATS/VBAS Operator Interface
  • Supports Night Time Operations
  • Built in Self-Test

*Subject to Change

 

Modes Of Operation

  • FFT Vibration Signature
    • Frequency
    • Order Tracking
  • Blade Tracking
    • Blade Tip Path
    • Lead/lag Characteristics
  • Balancing
    • Single & Multi Plane

Inputs

  • 5 Triaxial or 15 Single Axis Accelerometers  (10 mV/g – 100 mV/g)
  • 1 Hand Held Camera  (day/night or cloudy)
  • 2 Rotor Blade Tachometers  (Optical or Magnetic Pickup)
  • 2 RS-232C Serial Ports
  • 1 Parallel Port

Memory

  • 28 MB of Memory

Software

  • MSDOS compatible supporting Depot, Recall, Generic, and Erase Utilities

Front Panel

  • Color, TFT LCD with backlight
  • Large Viewing Area: 8.3” X 6.2”
  • High Resolution: 640 x 480 pixels
  • Tactile Feel Keypad

Physical Characteristics

  • Height: 13” • Width 13” • Depth 4”
  • Weight: 16 lbs

Power Requirement

  • +28 VDC – Direct Connection
  • 115 VAC – 115 VAC to 28 VDC converter

Printer Interface

  • Parallel

Built In Self Test

  • Go-No/Go testing with fault isolation

Data Acquisition

  • 1-4 channels of simultaneous data acquisition

 

TABS is intended for use in harsh and demanding environments and has been designed to meet:

  • Environmental Requirements of MIL-STD-810D
  • Shock and Vibration Requirements of MIL-STD-810D
  • EMI Requirements of MIL-STD-461C

Automatic test programs are created on your PC and downloaded to the TABS.  Pilots and technicians are guided through the data collection procedures by instructions displayed on the large, easy to read screen.

When data collection is completed, test results are displayed enabling the pilot or technician to quickly identify problem areas and the corrective actions necessary to solve them.

TABS supports all three Aircraft Maintenance Modes:

 Rotor Blade Tracking – Rotor blade tip path corrections and lead/ lag characteristics can be measured either day or night, using the optional line scan camera.

 Balancing – Single and dual plane balancing can quickly be performed.  A Discrete Fourier Transform (DFT) calculates phase angle and amplitude of the imbalance and rotor smoothing algorithms provide simultaneous, multiple maintenance adjustments.

 Vibration Signature – A Fast Fourier Transform (FFT) and four channel simultaneous data acquisition capabilities are employed to yield fast, accurate vibration analysis results.

Transducers

  • Triaxial – Model DI-103
  • Single Axis – Model DI-108

Speed Reference

  • Optical – Model DI-204
  • Magnetic – 3030AN

Blade Tracking

  • Model DI-206 Solid State CCD
  • Line Scan Camera

115 VAC 50/400Hz to 28 VDC Converter

  • Model DI-219

Printer

  • COTS Parallel/Serial Printer
  • Part# 1901-0067

Cables

  • Single Axis Accelerometers
  • Triaxial Accelerometers
  • Optical Tachometers
  • Magnetic Pickups
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  • Camera Data
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