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Application attachment means:
  • Flywheel to shaft.
  • Flywheel to hub (splined).
  • Shaft to shaft.
  • Floating shaft.
  • Many others.
Unit of Measure

Specifications

Shaft Rating at 2000 rpm

 N/A 75 to 2000 hp

Capacity per 100 rpm

 N/A 15.87 hp11.84 kW
Torque Rating TN1 N/A 10000 lbs-in1130 N-m
Approximate Slip Torque2 N/A 40000 lbs-in4.52 N-m
Torsional Rate kØ3 N/A 50000 lbs-in/rad5650 N-m/rad

Axial Rate KA

 N/A 3500 lbs/in612 N/mm

Radial Rate KR

 N/A 11500 lbs/in2012 N/mm

Weight Mass

 N/A 33 lbs14.96 kg

Inner Member Inertia

 N/A 0.59 lbs-in-sec20.067 kg-m2

Outer Member Inertia

 N/A 0.92 lbs-in-sec20.104 kg-m2
Pilot Outer Diameter4 N/A 13.875 in352.42 mm

B.C. Diameter

 N/A 13.125 in333.38 mm

Diameter C

 N/A 4.000 in101.60 mm
Diameter D5 N/A 4.625 in117.47 mm

Diameter E

 N/A 6.00 in152.40 mm

Length F

 N/A 3.06 in77.72 mm

Length G

 N/A 0.125 in3.18 mm

Length H

 N/A 0.1875 in4.76 mm

Length J

 N/A 0.75 in19.05 mm

Hole Diameter K

 N/A 0.406 in10.31 mm

Number of Holes L

 N/A 16

Hole Size M

 N/A 3/8-16 UNC-2B in

Number of Holes N

 N/A 3
Fits SAE Flywheel Number6 N/A 11-1/2 OR

Reference Diameter P

 N/A 11.38 in289.1 mm

Browning Bushing P/N

 N/A R1

Browning Bushing Bore Type 1 Diameter

 N/A 1-1/8 to 2-13/16 in28.16 to 71.4 mm

Browning Bushing Bore Type 2 Diameter

 N/A 2-7/8 to 3-3/4 in73.0 to 95.2 mm

General Description

N/A The Dynaflex coupling line has been developed to overcome numerous torsional problems associated with vehicular and industrial driveline systems. These couplings increase equipment life by protecting against torsional vibration, shock and misalignment. Other significant features and benefits are:

  • Vibration Isolation: extremely low torsional spring rate is achieved with the Dynaflex coupling, using elastomer in shear. This allows for low system natural frequencies and isolation of first mode driveline disturbances.

  • Damping at Resonance: the elastomer used in LCD couplings effectively reduces vibration at resonance.

  • Shock Protection: torsional shock loads are attenuated by large shear deflection of the elastomer. In the case of severe overloads, equipment damage is prevented by slippage between the elastomer and the outer housing.

  • Misalignment Accommodation: elastomer flexibility allows for angular, parallel and axial misalignment.

  • Long Service Life: Lord Dynaflex couplings have proven themselves under demanding and rugged service conditions.

  • Maintenance Free: elastomer flexibility accommodates all motion without wear, eliminates the need for lubrication.

  • Noise Reduction: no metal-to-metal contact; elastomer attenuates structure-borne noise and isolates vibration from components that would act as noise generators.

  • Attachment: fits many standard SAE flywheels.

  • Design Flexibility: standard rubber molds are used to produce each different size coupling shown in this catalog. Often it is necessary to change metal components for custom applications. This is common.

  • Systems Engineering: Lord has in-house computer capabilities for multi-mass torsional analysis to assist in proper coupling selection.

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    Note

    N/A Tapered.

    • 1 Prolonged exposure to temperatures in the 0 ºF range and below produces a significantly reduced slip torque prior to driveline warm-up. This condition may result in the coupling's inability to transmit adequate drive torque for applications experiencing unusual cold temperature related parasitic loading.
    • 2 Prolonged exposure to temperatures in the 0 ºF range and below produces a significantly reduced slip torque prior to driveline warm-up. This condition may result in the coupling's inability to transmit adequate drive torque for applications experiencing unusual cold temperature related parasitic loading.
    • 3 Prolonged exposure to temperatures in the 0 ºF range and below produces a significantly reduced slip torque prior to driveline warm-up. This condition may result in the coupling's inability to transmit adequate drive torque for applications experiencing unusual cold temperature related parasitic loading.
    • 4 Pilot diameter tolerances are + 0.000/ -0.005 in. for "A" and + 0.005/ -0.000 in. for "C" diameters.
    • 5 Pilot diameter tolerances are + 0.000/ -0.005 in. for "A" and + 0.005/ -0.000 in. for "C" diameters.
    • 6 Refer to SAE J620c for flywheel numbers 6-1/2, 10, 11-1/2, 16; to SAE J927a for numbers 60, 80, 100, 120, 160.