200M 400M 200M
RNG: 2.4 KM
BRG: 047°
ALT: 3,200 FT
SPD: 480 KTS
HDG: 012° N
TGT: ALPHA-7
MODE: SEARCH
PWR: NOMINAL
FREQ: X-BAND
STATUS: LOCK
NAVTGTWPNDEFRDRCOM
MIL-STD-1553IFF: ACTIVELINK-16: SYNC
SECTOR: ALPHA
THREAT: CLEAR
RADAR: ACTIVE
TRACK: 6 TGT
LAT 28.6213°N LON 77.3873°E
NX
Neometrix Target Acquired
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Aero-Engine Fuel Accessory Test Systems / Integrated Fuel Pump & Controller Calibration / MIL‑STD · ISO · IS / Noida · India 2026 · Product Page
FUEL PUMP & CONTROLLER BENCH · ATF · 50 LPM

Advanced Test & Calibration Bench for Integrated Fuel Pump and Controller — to 6,200 RPM at 22 ± 0.2 kgf/cm².

A multi-domain hydraulic, pneumatic and electrical test facility that replicates the operating environment of an integrated fuel pump and controller inside an aircraft engine. It calibrates and verifies fuel delivery, drive speed and ECU control-signal response under controlled laboratory conditions, then preserves the unit with a heated protective-oil circuit before installation or storage.

Advanced test and calibration bench for integrated fuel pump and controller in aircraft engines - CAD rendering of the Control Room, Test Cell and Motor Isolation Room layout by Neometrix
Fig · 01 CAD rendering · three-zone facility layout (Control Room / Test Cell / Motor Isolation Room), as designed
Designed to comply with:
MIL-STD ISO IS
Max Flow Rate
50LPM
HP Fuel Supply
22±0.2 kgf/cm²
Motor Speed
6,200RPM max
Final Filtration
3µm, β>1000
Preservation Oil
70±2 °C
01
Overview

One bench, three domains.

Hydraulic, pneumatic and electrical simulation combine to qualify a single critical engine accessory.

The integrated fuel pump and controller is a critical aero-engine accessory: it delivers fuel at precisely regulated pressures and flow rates while simultaneously adjusting compressor inlet guide vane (IGV) positions in response to engine speed, inlet air temperature, compressor discharge pressure and throttle commands. The Advanced Test & Calibration Bench replicates the hydraulic, pneumatic and electrical conditions this unit experiences in service, allowing engineers to calibrate, verify and document performance before installation.

Beyond live operational simulation, the bench incorporates a preservation system that circulates heated protective oil through the unit after testing — extending component life and preventing corrosion during storage or transportation.

“Calibrate, verify, preserve — one bench covers the unit’s full pre-installation life cycle.”
02
Layout

Three zones, one safety-first workflow.

The facility is physically separated to protect operators and keep noise, vibration and flammable media contained.

ZONE · 01

Control / Command Room

Houses the main operator panel, PLC/HMI interface and all instrumentation readouts, isolating the operator from noise, vibration and hazards in the test area.

ZONE · 02

Test Cell

Contains the hydraulic, pneumatic and preservation subsystems, arranged for maximum accessibility during setup and maintenance.

ZONE · 03

Motor Isolation Room

An acoustically dampened enclosure for the drive motor and gearbox, preventing high-frequency vibration and noise from coupling into the fuel system or test area.

Flammable or pressurised media stay within controlled areas, while electrical and control systems are housed in flameproof enclosures and kept at a safe distance from ATF handling equipment.

03
Hydraulic Circuit

Storing, filtering & delivering ATF.

The backbone of the test bench — conditioning and delivering Aviation Turbine Fuel at precisely regulated pressures and temperatures.

A 100-litre stainless steel (SS-300 series, 3 mm wall) service tank feeds two separate gear pumps. The high-pressure pump is rated at 50 LPM at 50 kgf/cm², driven by a flameproof, foot-cum-flange mounted motor, and supplies test lines regulated by constant-pressure valves to 22 ± 0.2 kgf/cm² and 11 ± 0.2 kgf/cm². A second 50 LPM / 10 kgf/cm² pump serves an independent circulation and filtration loop.

A low-level sensor on the tank is linked to an interlock that automatically shuts down the pumps to prevent cavitation damage, and a removable lid allows internal cleaning and inspection.

  • Multi-stage filtration: 16 µm pre-filter → 6 µm intermediate → 3 µm final, each β > 1000, with a differential-pressure gauge and a 3.5 bar bypass valve on every housing.
  • Air separator: removes entrained gas bubbles before the unit to prevent pressure-regulation error or cavitation damage.
  • Drain back pressure: a dome-regulated drain valve holds a constant 2 ± 0.2 kgf/cm² back pressure, simulating an engine fuel drain system.
  • Temperature control: a plate heat exchanger handles 50 LPM of ATF against chilled water at 6 kgf/cm², holding the 15–40 °C operating range.
04
Pneumatic Network

Bleed-air simulation & post-test drying.

Low- and high-pressure air services replicate engine bleed-air functions and dry the unit after fuel testing.

Low-pressure circuit

Designed for post-test drying. Compressed air enters through a moisture separator (drained periodically via a manual valve) and a fine particulate filter before being routed to the unit through a flexible hose, removing residual fuel from internal passages.

High-pressure circuit

Simulates bleed air supplied to temperature-sensing elements such as the TDK-Tp sensor. A high-precision regulator and fine filter feed a throttle valve that vents air to atmosphere in a controlled manner, simulating transient bleed events. Pressure is read on an analog gauge and logged via a high-accuracy transducer at the control panel.

05
Drive, Control & Preservation

Precise speed control, then corrosion protection.

Closed-loop drive control and ECU signal simulation, followed by a heated preservation cycle before storage.

Electrical drive & control

A high-speed motor coupled through a 1:4.32 gearbox drives the unit at speeds up to 6,200 RPM. A closed-loop, vector-controlled Variable Frequency Drive with encoder feedback resolves speed to within ±1 RPM, with the motor and gearbox mounted on vibration isolators inside the Motor Isolation Room.

The Command Room panel displays supply/drain pressures, pneumatic pressures, ATF and preservation-oil temperatures, electrical consumption and shaft speeds. A pulse duty-cycle generator outputs 27 VDC at 40 Hz (default 50% duty, front-panel adjustable) to actuate electro-mechanical valves on the unit, simulating ECU control signals. Safety systems include flameproof enclosures, an emergency-stop circuit, overpressure relief on both hydraulic and pneumatic lines, and the low-level fuel cut-off interlock.

Preservation & conditioning circuit

After testing, this circuit circulates heated protective oil through the unit's internal fuel passages to prevent corrosion, oxidation and residue build-up. It uses its own 100-litre stainless steel tank with a low-level sensor, a dedicated flameproof gear pump, and filtration identical to the main fuel system.

Oil is heated to 70 °C ± 2 °C for optimal coating and penetration into fine clearances. A bypass valve prevents overpressure on downstream blockage, and a relief valve diverts excess oil back to the tank. The circuit runs in static soak mode or continuous dynamic circulation mode.

06
Engineering Drawing

Facility layout, as engineered.

General-arrangement drawing (top, isometric, front and side views) plus supporting CAD renderings of the three-zone facility.

Advanced test and calibration bench for integrated fuel pump and controller in aircraft engines - general arrangement drawing, top / isometric / front / side views
Fig · 02 General arrangement drawing · Design 1
Advanced test and calibration bench for integrated fuel pump and controller in aircraft engines - aero-engine fuel flow and ECU calibration system by Neometrix, CAD rendering
Advanced fuel pump and controller calibration bench instrumentation panel - aircraft engine fuel management system performance verification by Neometrix, CAD rendering
Fig · 03–04 Additional facility renderings · Test Cell instrumentation and hydraulic skid
07
Specifications

Technical specifications.

Working FuelAviation Turbine Fuel (ATF)
Preservation FluidMineral-based preservation oil
Fuel Tank Capacity100 L (SS-300 series, 3 mm wall)
Preservation Oil Tank Capacity100 L (SS-300 series, 3 mm wall)
High-Pressure Supply22 ± 0.2 kgf/cm²
Low-Pressure Supply11 ± 0.2 kgf/cm²
Drain Back Pressure2 ± 0.2 kgf/cm²
Max Flow Rate50 LPM
Filtration Stages16 µm → 6 µm → 3 µm, β > 1000
Filter Bypass Pressure3.5 bar
Heat ExchangerPlate type, 50 LPM, chilled water 6 kgf/cm²
Air Simulation PressureRegulated, high and low circuits
Drive SystemElectric motor with 1:4.32 gearbox
Motor Speed Range500–6,200 RPM
Speed Accuracy± 1 RPM (encoder feedback)
Electrical Supply415 VAC ± 10%, 50 Hz, 3-phase
Control InterfacePLC/HMI with manual override
Pulse Duty Generator Output27 VDC, 40 Hz, adjustable duty
Oil Preservation Temperature70 °C ± 2 °C
Safety FeaturesFlameproof design, E-stop, overpressure relief, low-level shutdown
PipingSeamless SS-300, aerospace-grade fittings
Maintenance AccessFront-access filters, valves, instrumentation
08
Applications

Where the bench is used.

01Pre-installation calibration of integrated fuel pump and controller units.
02Verification of fuel system performance under simulated operational conditions.
03Research and development testing for aerospace fuel control systems.
04Quality assurance and certification of aircraft engine fuel accessories.
05Failure diagnosis and troubleshooting of pump-controller assemblies.
06Long-term preservation of fuel units before installation or shipment.
07Training platform for maintenance and testing personnel.
08Data collection for performance trend analysis and predictive maintenance.
09
Key Features

Built for repeatable results.

FEATURE · 01

HP gear pump at 50 LPM and 50 kgf/cm², regulated down to 22 ± 0.2 kgf/cm², delivers precise ATF to the fuel unit.

FEATURE · 02

Three-stage filtration (16→6→3 µm, β>1000) and an air separator ensure contamination-free fuel for all test runs.

FEATURE · 03

VFD with encoder feedback drives the test unit at up to 6,200 RPM with ±1 RPM speed resolution via a 1:4.32 gearbox.

FEATURE · 04

Plate heat exchanger at 50 LPM maintains ATF between 15–40 °C, replicating engine temperature cycling conditions.

FEATURE · 05

Pneumatic simulation circuit replicates engine bleed-air pressure and post-test drying of internal fuel passages.

FEATURE · 06

Preservation circuit heats mineral oil to 70 °C ± 2 °C and circulates it through unit passages to prevent corrosion.

FEATURE · 07

27 VDC, 40 Hz pulse duty-cycle generator simulates ECU valve command signals during integrated controller testing.

FEATURE · 08

Flameproof enclosures, emergency stop, and overpressure relief in both circuits protect ATF bench operators always.

10
Downloads

Design drawing (PDF).

General-arrangement design drawing for the bench, available as PDF for procurement review and technical pre-screening.

11
FAQ

Common questions.

Plain-language answers from the engineering team.

Q · 01What is the Advanced Test & Calibration Bench for Integrated Fuel Pump and Controller?
It is a multi-domain hydraulic, pneumatic and electrical test facility designed and manufactured by Neometrix Engineering Pvt Ltd, India, that replicates the operating environment of an integrated fuel pump and controller in an aircraft engine — enabling calibration, functional verification and post-test preservation before the unit is installed.
Q · 02How is the test facility physically laid out?
The facility is divided into three zones: a Control/Command Room housing the operator panel, PLC/HMI and instrumentation; a Test Cell containing the hydraulic, pneumatic and preservation subsystems; and an acoustically isolated Motor Isolation Room housing the drive motor and gearbox, keeping vibration and noise away from the test article.
Q · 03What fuel delivery pressures and flow rates does the bench provide?
Two gear pumps deliver ATF at up to 50 LPM. The high-pressure line is regulated to 22 ± 0.2 kgf/cm² and a secondary line to 11 ± 0.2 kgf/cm² by constant-pressure valves, with a dome-regulated drain valve holding a 2 ± 0.2 kgf/cm² back pressure to simulate the engine's fuel drain system.
Q · 04How is fuel cleanliness and temperature controlled?
Fuel passes through three filtration stages (16 µm, 6 µm and a final 3 µm absolute, each β > 1000) plus an air separator to remove entrained gas. A plate-type heat exchanger, fed by chilled water at 6 kgf/cm², holds ATF temperature within the 15–40 °C operating band.
Q · 05What speeds and drive control does the bench achieve?
A high-speed motor driving through a 1:4.32 gearbox reaches up to 6,200 RPM. A closed-loop, vector-controlled Variable Frequency Drive with encoder feedback holds speed to within ±1 RPM, with the motor and gearbox isolated on vibration mounts.
Q · 06What does the pneumatic simulation network do?
A low-pressure circuit dries the unit after fuel testing through a moisture separator and fine filter. A high-pressure circuit simulates engine bleed air to temperature-sensing elements such as the TDK-Tp sensor, with regulated pressure monitored on both an analog gauge and a data-logging transducer.
Q · 07What does the preservation and conditioning circuit do?
After functional testing, a dedicated circuit circulates mineral-based preservation oil, heated to 70 °C ± 2 °C, through the unit's internal fuel passages to prevent corrosion and residue build-up during storage or transport. It can run in a static soak mode or a continuous dynamic circulation mode.
Q · 08How does the bench simulate ECU control signals?
A pulse duty-cycle generator outputs 27 VDC at 40 Hz with an adjustable duty cycle (50% default) from the front panel, actuating the electro-mechanical valves on the unit under test to simulate real ECU control signals during calibration.
Q · 09What safety features are built into the bench?
Flameproof enclosures house all electrical devices, with an emergency-stop circuit, overpressure relief valves on both the hydraulic and pneumatic lines, and a low-level fuel cut-off interlock on the service tank that automatically shuts down the pumps to prevent cavitation damage.
Q · 10Does the bench comply with recognised standards, and is it customizable?
The bench is built with seamless stainless steel (SS-300 series) piping, aerospace-grade Swagelok/Parker fittings and 37°/74° flare seals, designed to comply with applicable MIL-STD, ISO and IS requirements. Neometrix Engineering Pvt Ltd offers customized envelopes tailored to specific unit types and client acceptance criteria.
Q · 11How can I get a quotation for this test bench?
You can request a quotation by contacting Neometrix Engineering Pvt Ltd through the website, or by email or phone. Neometrix Engineering Pvt Ltd exports this test bench to customers in defence, aerospace and industrial sectors across multiple countries.
Get a proposal

Tell us your fuel pump/controller
unit and test requirements.

We configure the hydraulic, pneumatic and preservation circuits, and walk through the calibration and acceptance criteria with your QA team before you commit.

Request proposal +91 7777 876 876

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Engineered To Standards Used In UK, NATO & U.S. Defence Procurement
DEF STAN (UK MoD)
NATO STANAG
RTCA/EUROCAE DO-160
MIL-SPEC / MIL-STD
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