MOOG D661-XXX-P30HAAF6VSX2-B ENGLISH TECHNICAL SPECIFICATION & MANUAL
June 05, 2026

MOOG D661-XXX-P30HAAF6VSX2-B ENGLISH TECHNICAL SPECIFICATION & MANUAL

1. Model Code Decoding(D661-XXX-P30HAAF6VSX2-B) 表格 Code Definition D661 MOOG D660 family integrated-amplifier ServoJet two-stage servo valve series XXX Custom factory part number / spool core customized code (flow core reserved field, P30 = Rated flow 30L/min @ΔP=35bar per land) P ServoJet pilot stage, no mechanical spool feedback (electronic closed-loop spool feedback built-in) 30 Nominal rated flow: 30 L/min @35bar pressure drop per control land H Internal pilot oil supply from P port; Pilot drain internal to T port(Y internal return)Moog Inc. AA 1st A: ±10VDC differential analog command input; 2nd A: ServoJet pilot spool structure, 4-way spool layout F Standard 6+PE round aviation connector (DIN standard pin assignment)Moog Inc. 6 Closed center / zero overlap spool, linear flow gain at null positionMoog Inc. VS Built-in 24VDC onboard amplifier, EMC optimized circuit, Viton fluorine rubber seal X2 Custom spool machining tolerance + factory preset null offset calibration B OEM customized version for special equipment/host machine

Description

2. Core Hydraulic Parameters

Pressure Rating

  • Main P/A/B port: Max working pressure 350bar(5000PSI)

  • T drain port(Y internal drain): Max allowable backpressure 210bar(3000PSI)

  • Pilot oil: Powered internally from main P pressure, working range 210~350bar

Flow Index

  • Rated flow: 30 L/min @ ΔP=35bar per single orifice

  • Zero leakage: ≤2.8 L/min at full rated supply pressure

  • Max full-open flow: ~35 L/min

Dynamic Performance(210bar supply, ISO standard oil)

  • 0~100% full stroke step response: 9~13ms

  • Hysteresis<0.3%FS; Resolution<0.05%FS; Temperature zero drift<0.1%/55KMoog Inc.

  • -3dB frequency response: 55~75Hz

Hydraulic Fluid Requirements

  • Oil cleanliness: ISO4406 17/14/11 minimum; recommended 16/13/10

  • Working oil temp: -20℃~+80℃, working viscosity:15~68mm²/s

3. Electrical SpecificationsMoog Inc.

  • Power supply: DC24V(allow 18~32VDC), steady current ≤0.75A

  • Command signal: Differential ±10VDC input(0V=zero flow; +10V full forward flow; -10V full reverse flow)

  • Connector: 6-pin+PE aviation plug standard pinout:

    Pin1=DC24V+, Pin2=0V(GND), Pin3=+Command, Pin4=-Command, Pin5/Pin6=spare, PE=valve body earth ground

  • Built-in LVDT spool position closed-loop amplifier, no external servo driver needed

4. Mounting Standard

  • Mounting face: ISO4401-05(NG10) standard installation pad

  • Mount surface flatness<0.01mm/100mm, Ra<0.8μm; mounting bolt M12×70, tightening torque:65~70N·m

5. Null Adjustment Procedure

  1. Cut off analog command signal, keep 24VDC power on for valve amplifier

  2. Remove small cover screw on electronic housing, access zero trim potentiometer

  3. Fine-tune trimmer within ±1 full rotation only, adjust until actuator no drift at zero command;

Note: X2-B customized pre-zeroed at factory, trim only when obvious long-term zero drift occurs.

6. Common Fault & Troubleshooting

  1. No output flow with valid ±10V command

    Check 24VDC supply voltage; verify signal wiring; clogged pilot filter inside valve or severe oil contamination

  2. Actuator drifts at zero command

    Spool jamming from dirty oil; zero offset needs potentiometer fine tuning; internal pilot contamination

  3. Slow dynamic response

    Supply pressure below 200bar; oil viscosity too high; blocked built-in pilot filter

  4. Flow fluctuation

    Unstable 24V power; signal cable near high-pressure pipeline causing EMI interference

7. Safety Notes

  1. Depressurize entire hydraulic circuit fully before disassembling piping or valve

  2. Never hot-plug electrical connector under powered status to avoid onboard amp burnout

  3. Do not disassemble valve body without professional MOOG authorized maintenance


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