Landing Gear Diagnostics and Prognostics

Structural Health Monitoring Systems

Since 2012, ES3 has been developing landing gear Structural Health Monitoring Systems (SHMS) in collaboration with the US Navy, US Air Force, commercial operators and an OEM. Today, ES3 has successfully tested our system on four fixed wing and rotorcraft platforms. We have performed qualification tests, completed flight test/certification on one aircraft, and delivered production units that are currently fielded and performing well on operational aircraft. The ES3 SHMS is custom configurable to provide and display such conditions as:

  • Aircraft/Rotorcraft Gross Weight
  • Aircraft/Rotocraft Balance
  • Conditioned Based Maintenance
    • Strut Servicing
    • Hard Landings
    • Brake Temperature Monitoring
    • Historical Data (via display or data output)

The ES3 SHMS requires no modification to the landing gear strut assemblies. It can be retrofit onto existing aircraft. The control unit has ARINC 429 output compatibility for transmitting information to an existing cockpit display.

Central Control Unit (CCU)
  • Integrated Display (Color or NVIS)
  • Diagnostic Unit
  • ARINC 429 Output
  • Built-in Test
  • Sortie Data Storage
  • High Reliability
Servicing Manifold Assembly (SMA)
  • Integrates Schrader Valve
  • Hermetically Sealed Sensor
  • No Strut Modification Required
  • High Reliability
Remote Data Concentrator (RDC)
  • Size, Weight, & Power Optimized (0.65 lb)
  • Precise Sensor Data collection
  • High Speed Data Transmission
  • High Reliability
  • Sensor Expansion Capability

Accuracy and reliability proven by successful operational deployment

ES3 has successfully deployed an On-Board Weight and Balance System (OBWBS). The ES3 OBWBS has been operational for more than 4 years on a fleet of 15 heavy military rotorcraft. During that time, accuracy better than plus or minus 3% gross weight has been achieved and all Reliability, Availability, and Maintainability (RAM) goals have been exceeded. The ES3 technology is not just a good concept; it is ready and proven. 

Environmental Qualification Testing Pedigree

Test DescriptionMilitary Testing MIL-STD-810*Commercial Testing RTCA/DO-160G
Altitude
Temperature
High Temp Diurnal
Temp Shock
Fluids
Solar Radiation
Rain
Humidity
Fungus
Salt Fog
Blowing Dust
Blowing Sand
Explosive Atmosphere
Immersion
Waterproofness
Acceleration
Vibration
Operational Shock
Crash Shock
Bench Handling
Transit Shock
Gunfire Vibration
Acoustic Noise
Decompression
Overpressure
Chemical Decontamination
Fire

*Testing performed to MIL-STD-810G and/or MIL-STD-810H, based on program requirements

Electromagnetic Interference (EMI) Qualification Testing Pedigree

Test CategoryTest SectionMilitary Testing
MIL-STD-461*
Commercial Testing
RTCA/DO-160G
Conducted EmissionsCE101
Conducted EmissionsCE102
Conducted SusceptibilityCS101
Conducted SusceptibilityCS114
Conducted SusceptibilityCS115
Conducted SusceptibilityCS116
Radiated EmissionsRE101
Radiated EmissionsRE102
Radiated SusceptibilityRS101
Radiated SusceptibilityRS103
Audio Frequency Conducted SusceptibilitySection 18
Induced Signal SusceptibilitySection 19
Radio Frequency SusceptibilitySection 20
Emission of RF EnergySection 21
Indirect Lightning StrikesSection 22
Direct Lightning StrikesSection 23
Electrostatic DischargeSection 25
Power QualityMIL-STD-704F

*Testing performed to MIL-STD-461F and/or MIL-STD-461G, based on program requirements

Landing Gear SHMS Team

Connect with the Landing Gear Structural Health Monitoring System (SHMS) Team to learn more about SHMS, including Onboard Weight and Balance Systems (OBWBS), Brake Temperature Monitoring Systems (BTMS), Hard Landing Indicators, and/or Strut Servicing Status. Contact us at sales@es3inc.com.

Advancing Aerospace Technologies for More Than 20 Years