Parker 36E84-18QF Air Turbine Starter

Condition: Used (Tested)

Country of Origin: United States

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Description

Parker Air Space Products 36E84-18QF Air Turbine Starter (Assembly P/N: 92003)

The Parker 36E84-18QF (Assembly Identification: 92003) is a high-power-density, axial-flow pneumatic turbine starter designed to crank high-inertia gas turbines, aeroderivative marine propulsion systems, and heavy industrial gensets.

This unit converts compressed air or engine bleed air into dynamic rotational torque. The unit integrates a single-stage radial/axial expansion turbine wheel, a compound planetary reduction gear set, and an overrunning sprag clutch mechanism. The internal overrunning clutch automatically disengages the starter drivetrain once engine light-off occurs and spool-up exceeds starter operating speed, preventing dangerous back-drive into the reduction gear assembly.

 

Model Details:

  • Manufacturer: Parker Hannifin / Parker Air Space Products Division
  • Model Series: 36E84
  • Manufacturer Part Number (MPN): 36E84-18QF
  • Assembly / Stock Reference: 92003
  • NATO Stock Number (NSN) Correlation: 2995-01-Series (Turbine Engine Starters)
  • Standard Military/Aero Equivalents: Bendix / AlliedSignal / Honeywell 36E84 Series Interchangeable Platforms

 

Technical Details

Parameter Specification / Rating
Part Number (MPN) 36E84-18QF (Assembly: 92003)
Working Medium Dry compressed air, filtered plant air, or engine compressor bleed air
Operational Inlet Pressure Range 35 PSIG to 50 PSIG (Nominal: 40–45 PSIG)
Maximum Inlet Proof Pressure 90 PSIG
Operating Inlet Temperature Range -40°F to 450°F (-40°C to 232°C)
Turbine Wheel Operating Speed 45,000 to 65,000 RPM (dependent on supply pressure)
Rated Output Shaft Speed 3,200 to 4,800 RPM (continuous cranking limit)
Breakaway / Stall Torque 280 to 350 lb-ft (380 to 475 Nm) @ 45 PSIG nominal inlet
Clutch Mechanism Zero-backlash, centrifugal overrunning sprag clutch assembly
Clutch Disengagement Speed Engine self-sustaining idle trip (typically 4,800–5,200 output shaft RPM)
Electrical Terminal Allocation 28V DC nominal cut-out switch / magnetic speed pickup sensor (Pins A: +28V DC, B: Ground/Return, C: Speed Signal Pulse Output)
Air Supply Flange 3.0-inch V-Band clamp duct connection (SAE AS407 / QAD interface)
Mounting Interface SAE 8-bolt or Quick-Attach-Detach (QAD) accessory gearbox mounting flange
Output Drive Spline Involute spline, stub tooth configuration per SAE AS870 standard
Lubrication System Self-contained oil sump or engine-fed lubricating oil mist (MIL-PRF-23699 / MIL-PRF-7808 synthetic turbine oil)
Dry Weight Approx. 24.5 lbs (11.1 kg)

 

Features

  1. Compound Planetary Reduction Assembly: Case-hardened spur and planetary gears provide optimal speed reduction while handling maximum shock loads during unassisted cold start cycles.
  2. Bi-Directional Overrunning Clutch Safety: Built-in mechanical sprag clutch ensures instantaneous, friction-free disengagement the moment the turbine lights off and drives the pad faster than the starter output shaft.
  3. QAD (Quick-Attach-Detach) Flange Configuration: Minimizes mean time to repair (MTTR) with a positive-locking V-band mounting profile that eliminates drive-pad stud binding.
  4. Integrated Speed-Sensing Circuitry: Terminal provisions allow direct tie-in to turbine engine control units (FADEC / Woodward Governor) for automatic air shut-off valve (ASOV) actuation upon reaching ignition cutout speed.

 

Equipment Compatibility

  • Aeroderivative gas turbine engines (LM2500, LM1600, Allison 501-K / 570 series accessory gearboxes via standard QAD adapters)
  • Rolls-Royce Avon, Tyne, and Olympus auxiliary gear train systems
  • Industrial turbine generator sets (Solar Turbines, Dresser-Rand auxiliary starting mounts)
  • Aircraft GSE (Ground Support Equipment) and dedicated turbine starting carts

 

Applications

  • Commercial Marine Propulsion: Blackout recovery cranking and main propulsion gas-turbine start sequences on fast ferries, cruise ships, and naval auxiliary vessels.
  • Offshore Oil & Gas Platforms: Mechanical drive and emergency generator turbine starting where electric motor sparking risks explosive hazard zones.
  • Turbine Co-Generation & Peaking Plants: High-cycling industrial prime mover start systems running on compressed nitrogen or plant air storage banks.
  • Emergency Black Start Skids: Compressed air-bottle-driven black start cranking modules.

 

Frequently Asked Questions

What causes a pneumatic starter clutch to fail to engage or slip?

Clutch slippage typically occurs when the internal sprag elements become fouled with contaminated or gummy gear oil. Using incorrect high-viscosity or EP (extreme pressure) greased oils can prevent the sprags from tilting into locking contact under low initial rotational speed, resulting in spinning whine without engine shaft rotation.

Can the Parker 36E84-18QF run on compressed nitrogen?

Yes. Clean dry nitrogen N2 bottle banks are completely compatible and are frequently used in marine and offshore explosion-proof skid packages as a clean, dry, non-oxidizing pressure source. Operating pressure limits remain unchanged (35 to 50 PSIG).

What is the maximum cranking cycle duty limit?

Standard duty cycles recommend no more than 3 continuous crank attempts of 30 to 45 seconds each, separated by a 5-minute cooling period. This prevents thermal shock in the reduction gear bearings and avoids localized heat buildup in the turbine scroll housing.

How do I know if the starter drive spline matches my accessory gearbox?

The 36E84-18QF features an involute stub-tooth drive spline standard to industrial aero-derivative gas turbine engines. Measure the pitch diameter, number of teeth, and pressure angle, or compare the mating female drive adapter on your engine’s accessory drive pad against the SAE AS870 standard.

Shipping and Delivery

14 DAYS RETURN POLICY

RETURNS ARE ACCEPTED IN 14 DAYS. BUYER PAYS THE SHIPPING CHARGES. RESTOCKING FEES 20%.

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