Aerospace Oxygen Test Bench – Precision Testing for Life Support Systems The Oxygen Test Bench is an advanced aerospace ground support equipment designed for precise aircraft life support system (LSS) testing. It enables comprehensive pilot oxygen system validation and oxygen regulator testing to ensure performance, reliability, and safety under simulated flight conditions. Engineered for high-accuracy oxygen flow calibration, the system supports multiple oxygen cylinder testing and pressure reducing valve test operations. This versatile LSS test rig is ideal for testing aviation oxygen valves, regulators, and other life support LRUs, making it a vital asset in aerospace oxygen system qualification and maintenance workflows. Compact, reliable, and fully instrumented, the Oxygen Test Bench ensures compliance with aerospace standards while enhancing operational readiness across defense and aviation sectors.

Advanced Life Support Oxygen Test Bench for Pilot Safety Systems

About

The Advanced Life Support Oxygen Test Bench is a precision-engineered testing platform developed to validate the reliability and safety of aircraft oxygen delivery components. It replicates in-flight pneumatic conditions—handling pressures up to 200 bar and flow rates up to 600 L/min—to comprehensively test filler valves, non-return valves, pressure-reducing regulators, and oxygen cylinder assemblies. Constructed entirely from SS-316L oxygen-compatible materials and integrated within a rugged, military-grade enclosure, the system combines dual-stage regulation, fine-flow measurement, high- accuracy instrumentation, and redundant safety mechanisms. Its controlled and repeatable testing environment enables detailed analysis of leakage, pressure stability, and functional response under realistic operating conditions. In doing so, the bench ensures that every life support component installed on an aircraft delivers consistent, contamination-free, and fail-safe oxygen supply, reinforcing the highest standards of pilot safety and airworthiness.
No Image

Image Gallery

Technical Details

Parameter Specification
Working Medium Gaseous Oxygen (99.5% purity)
Input Pressure Range 0 – 200 bar
Flow Range 0 – 600 LPM
HP Regulator Inlet 200 bar → Outlet 125 bar
LP Regulator Inlet 10 bar → Outlet 0.05 bar
Pressure Gauges 0–200 bar ×2, 0–20 bar, 0–15 PSI (SS316 Bourdon tube)
Safety Valves 126 ± 0.5 bar (HP), 10 bar (LP)
Filtration 25 µm SS filter, oxygen service compatible
Material SS316L for wetted parts, MS IS-2062 structure
Enclosure FRP military box, weatherproof
Temperature Range –30 °C to +70 °C
System Weight Approx. 85 kg
Power Requirement None (purely pneumatic)
Design Life 10 years (3 years storage + 7 years operational)
Certification ISO 17025 calibration · ISO 9001 manufacturing · Oxygen Service Cleaned
• Aircraft Production Lines: for acceptance testing of oxygen subsystem LRUs before aircraft installation.
• Maintenance, Repair & Overhaul (MRO) Facilities: for routine inspection and post-service validation.
• Aerospace Training Institutions: for maintenance personnel instruction and demonstration.
• R&D Laboratories: for design validation of new-generation oxygen valves, regulators, and system prototypes.
   
        

Key Features

  • High-precision oxygen test bench for validating pilot Life Support System components.
  • Handles pressures up to 200 bar and flow rates up to 600 LPM for full-range testing.
  • Dual regulation paths with HP (200→125 bar) and LP (10→0.05 bar) control modules.
  • All oxygen-wetted parts built in SS316L, degreased and cleaned to ASTM G93 standards.
  • Integrated safety valves, filtration, grounding, and anti-static oxygen-service design.
  • Provides complete functional and leak testing for valves, regulators, and cylinders.
  • Modular, transportable FRP enclosure with vibration isolation and weatherproof build.
  • ISO 17025 calibrated instrumentation ensuring reliable and traceable test results.

Media Gallery

Video Gallery

Download Gallery

×

Enquire Now

and we will get back to you.

Details

Introduction
The Advanced Life Support Oxygen Test Bench is a high-precision, aerospace-grade pneumatic testing system designed for functional validation, leak analysis, and calibration of oxygen distribution components used in aircraft pilot Life Support Systems(LSS).

In high-altitude flight, human life depends on an uninterrupted and correctly regulated supply of oxygen. As altitude increases, air density drops sharply, causing oxygen partial pressure to fall below the threshold required for normal brain and body function. Within seconds, hypoxia can set in — impairing cognitive response, muscle coordination, and eventually consciousness. The aircraft’s LSS mitigates this danger by automatically adjusting the flow and pressure of oxygen to the pilot’s breathing mask, maintaining safe and consistent oxygenation even during rapid altitude transitions or high-g maneuvers.

The LSS operates in an extremely harsh environment — subject to vibration, thermal variation, pressure cycling, and constant oxygen exposure. Every component within the system, from valves to regulators, must therefore meet stringent reliability and leak-free performance standards. Even microscopic contamination or a minor pressure irregularity can cause catastrophic oxygen system failure, posing direct risk to flight safety.

Recognizing the need for repeatable, ground-based verification of oxygen system components, Neometrix Defence Ltd. developed this Advanced LSS Test Bench The rig reproduces the full pneumatic behavior of an in-flight oxygen delivery circuit — including static high-pressure storage, flow regulation, and low-pressure breathing simulation. It allows precise testing of each Line Replaceable Unit (LRU) in the oxygen supply chain, ensuring mechanical integrity, functional accuracy, and long-term stability before installation or post-maintenance release.

In essence, this system serves as the final ground gatekeeper of flight safety — guaranteeing that the oxygen subsystem protecting the pilot has been tested, measured, and verified before takeoff.

Purpose and Scope
The Advanced Life Support Oxygen Test Bench provides a single integrated platform for testing, verifying, and certifying all major oxygen-handling components that make up an aircraft’s LSS. It enables both pre-installation validation (before fitting the components onto the aircraft) and periodic recertification (during maintenance cycles).

The rig is capable of performing end-to-end functional testing of the following oxygen LRUs:
1. Filler Valve (P/N DKR-130) – validates sealing, inlet tightness, and crack pressure behavior during cylinder charging.
2. Non-Return Valve (P/N 2124A-3TT) – verifies directionality of oxygen flow, forward cracking pressure, and reverse leakage resistance.
3. Pressure Reducing Valve (P/N 444-00389-700) – simulates pilot-demand conditions to measure outlet pressure regulation, stability under varying flow rates, and relief-valve accuracy.
4. Oxygen Cylinder & Valve Assembly (P/N 211-6512) – checks cylinder leak rate, built-in gauge calibration, and valve seat performance over 48-hour pressure retention cycles.

Each component represents a safety-critical node in the pilot’s breathing circuit.
The filler valve governs charging safety, the NRV prevents backflow contamination, the PRV ensures regulated delivery pressure, and the cylinder assembly guarantees clean, stable oxygen storage.
The test bench allows engineers to simulate real pneumatic behavior of these subsystems using pressurized oxygen up to 200 bar, controlled depressurization, and measured flow rates up to 600 LPM — replicating the operational envelope of an aircraft LSS at altitude.

Design and Construction
The bench is engineered as a modular, transportable, and all-weather testing system, constructed with materials and safety features suitable for continuous oxygen service.
Mechanical Framework
• Base chassis fabricated from Mild Steel (IS-2062) for strength and vibration resistance.
• Powder-coated to RAL 5005 Signal Blue, 60–80 μm coating thickness, corrosion-resistant finish.
• Mounted inside a military-grade FRP outer case with internal vibration isolation foam to absorb mechanical shocks during transport.
• Ergonomic layout: all gauges, regulators, and controls positioned on a front control panel for direct visibility and operator accessibility.

Materials and Compatibility
• All oxygen-contact components made from SS-316L or equivalent austenitic stainless steel with low carbon content for corrosion and ignition resistance.
• Fittings and connectors are degreased and oxygen-cleaned to ASTM G93 and CGA G-4.1 standards.
• Sealing elements fabricated from PTFE or Viton O-rings, ensuring compatibility with gaseous oxygen under high pressure.
• No use of oil-based lubricants, zinc-plated materials, or elastomers prone to exothermic reactions in oxygen service.

Construction Highlights
• System built as a closed-loop pneumatic circuit with independent high-pressure (HP) and low-pressure (LP) regulation paths.
• Incorporates dedicated sub-panels for filtration, regulation, flow measurement, and safety interlocks.
• Designed for maintenance ease — modular manifolds with quick disconnect couplers, allowing easy replacement of test lines and adapters.

Subsystem Overview
1. High-Pressure (HP) Regulation Section
• Accepts oxygen inlet up to 200 bar from a high-pressure cylinder.
• Includes:
  - HP regulator (200 → 125 bar) with fine-thread control for gradual pressurization.
  - Dual Bourdon-tube pressure gauges (0–200 bar) for inlet and outlet monitoring.
  - Safety relief valve set at 126 ± 0.5 bar to prevent over-pressurization.
• The regulator assembly ensures steady, pulsation-free supply to downstream circuits and test articles.

2. Low-Pressure (LP) Regulation Section
• Utilizes a precision LP regulator (10 → 0.05 bar) to simulate low-pressure breathing environments.
• Provides fine control for flow-regulated tests such as PRV outlet verification.
• Includes calibrated gauges:
  - 0–15 PSI gauge for ultra-low pressure readouts.
  - 0–20 bar gauge for intermediate pressures.

3. Flow Measurement & Distribution Section
• Equipped with a transparent flow indicator (0–600 LPM) for direct visual and quantitative observation.
• Used for mapping pressure vs. flow curves during regulator and valve characterization.
• Fitted with isolation valves and needle valves for dynamic control during testing.

4. Filtration & Safety Section
• Integrates a 25-micron SS filter to remove particulates and moisture, maintaining oxygen purity.
• Bleed valve for pressure relief after each test cycle.
• Vent valve enables complete purging of trapped gases, ensuring safety and repeatability.

5. Electrical Grounding and Static Control
• The bench includes grounding terminals and anti-static braided hoses to prevent electrostatic discharge.
• All components meet intrinsic safety norms for oxygen service environments.

6. Dimensions and Mobility
• Approximate system envelope: 1100 mm (L) × 700 mm (W) × 510 mm (H).
• Weight: ~85 kg (without gas source).
• Rugged handles and lockable castors for easy relocation.

Functional Testing Capability
Each LRU undergoes a complete functional validation sequence:
Filler Valve (DKR-130)
• Inlet pressure varied 3.5–125 bar; verify no inlet leakage.
• Crack-open pressure confirmed ≤ 8 bar (116 psi).
• Tested for sealing consistency under cyclic pressurization.

Non-Return Valve (2124A-3TT)
• Forward opening verified at > 0.5 psi.
• Reverse pressure held at 50, 400, and 1000 psi for 60 seconds each; zero leakage permissible.
• Ensures unidirectional protection against backflow contamination.

Oxygen Cylinder & Valve Assembly (211-6512)
• Cylinder filled to 128 bar (1850 psi).
• Static leak test for 48 hours: mass loss ≤ 4 g (equivalent 0.001 LPM).
• Pressure gauge correlation:
  - At 100 bar → 100 ± 7.5 bar.
  - At 50 bar → 50 ± 7.5 bar.
• Confirms long-term seal integrity and gauge accuracy.

Pressure Reducing Valve (444-00389-700)
• Regulator performance mapped across variable flow conditions:
Flow (LPM) Supply Pressure (bar) Expected Output (bar) Remarks
0 125 ≤ 6 (no-flow setpoint) Stable regulator baseline
1 125 5 ± 0.8 Fine regulation test
150 125 5 ± 0.8 Flow endurance
1 14 ≥ 3.45 Low supply response
100 14 ≥ 3.45 Minimum delivery assurance
Relief Test – 8 +1/–0.8 · Relief valve activation check
• Ensures pressure stability and relief mechanism accuracy under varying inlet and outlet conditions. Operational Procedure 1. Preparation: Ensure all control valves are closed. Connect oxygen source. Check that gauges read zero pressure. 2. Pressurization: Gradually open inlet and adjust HP regulator to desired setpoint. 3. Functional Testing: Route oxygen to the LRU under test using ON/OFF valves. Observe gauge and flowmeter readings. 4. Data Recording: Compare observed performance with acceptance criteria. Log results for certification. 5. Depressurization: Close all valves. Vent through bleed valve. Confirm complete pressure discharge. Safety, Quality, and Compliance • Classified as Type-4 Ground Test Equipment (TTGE) under aerospace ground support standards. • Manufactured in ISO 9001 / ISO 14001 / ISO 45001 certified facilities. • Oxygen components meet ASTM G93, ISO 7291, and EN 12021 requirements. • Every gauge, flowmeter, and regulator delivered with traceable calibration certificate (ISO 17025). • Safety features include: - Redundant relief valves on HP and LP circuits. - Anti-spark grounding connections. - Pressure decay monitoring before disconnection. - Fail-safe vent path for trapped gases. • Rig designed for –30 °C to +70 °C ambient temperature range, ensuring reliability across climatic conditions. Applications • Aircraft Production Lines: for acceptance testing of oxygen subsystem LRUs before aircraft installation. • Maintenance, Repair & Overhaul (MRO) Facilities: for routine inspection and post-service validation. • Aerospace Training Institutions: for maintenance personnel instruction and demonstration. • R&D Laboratories: for design validation of new-generation oxygen valves, regulators, and system prototypes. Technical Summary
Parameter Specification
Working Medium Gaseous Oxygen (99.5% purity)
Input Pressure Range 0 – 200 bar
Flow Range 0 – 600 LPM
HP Regulator Inlet 200 bar → Outlet 125 bar
LP Regulator Inlet 10 bar → Outlet 0.05 bar
Pressure Gauges 0–200 bar ×2, 0–20 bar, 0–15 PSI (SS316 Bourdon tube)
Safety Valves 126 ± 0.5 bar (HP), 10 bar (LP)
Filtration 25 µm SS filter, oxygen service compatible
Material SS316L for wetted parts, MS IS-2062 structure
Enclosure FRP military box, weatherproof
Temperature Range –30 °C to +70 °C
System Weight Approx. 85 kg
Power Requirement None (purely pneumatic)
Design Life 10 years (3 years storage + 7 years operational)
Certification ISO 17025 calibration · ISO 9001 manufacturing · Oxygen Service Cleaned
Conclusion The Advanced Life Support Oxygen Test Bench represents the culmination of Neometrix Defence Ltd.’s experience in aerospace pneumatic systems, combining precision engineering, robust safety design, and oxygen-service expertise into one versatile testing solution. This system ensures that every valve, regulator, and oxygen assembly destined for flight is validated under real conditions — for leak integrity, stability, repeatability, and safety. It serves as both a quality assurance instrument and a pilot protection system validator, directly contributing to aircrew survivability. With its modular construction, fully oxygen-compatible architecture, and adherence to the highest international standards, the Advanced Life Support Oxygen Test Bench stands as the definitive tool for oxygen system testing in modern aviation and defence applications.

Trending Products

Share This Page