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IMDS International Helo Safety Symposium

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Outline Navy/USMC Legacy Helicopter Fleet IMDS Description Functional Capabilities Safety-Enhancing Capabilities IMDS Growth and Future Applications Navy/Marine Corps ... – PowerPoint PPT presentation

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Title: IMDS International Helo Safety Symposium


1
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2
Outline
  • Navy/USMC Legacy Helicopter Fleet
  • IMDS Description
  • Functional Capabilities
  • Safety-Enhancing Capabilities
  • IMDS Growth and Future Applications

3
Navy/Marine Corps Legacy Helicopters
4
Navy HUMS Program Mandate
  • Result of a 1993 VH-60N mishap during a
    maintenance flight
  • H-53 designated lead-the-fleet platform for
    common helicopter IMDS
  • CNO mandate to incorporate avionics safety
    systems
  • Ground Proximity Warning System (GPWS)
  • Global Positioning System (GPS) navigation
  • Crash-Survivable Flight Incident Recorders
    (CSFIR)
  • Integrated Mechanical Diagnostic Systems (IMDS)
  • Production program for H-53 and SH-60 began in
    1997, with H-1 added in 1999.
  • Built by Goodrich Corporation, Fuel Utility
    Systems Div.

5
IMDS Description
  • Full-time onboard usage and diagnostic monitoring
  • Engines
  • Drive train
  • Rotor system
  • Also tracks
  • Operational limit exceedances
  • Operational and structural usage parameters
  • Flight data is downloaded post-flight for further
    diagnosis and reporting to NALCOMIS
  • System also on UH-1Y, AH-1Z, MH-60R/S, Army
    UH-60L/M and Sikorsky S-92

6
IMDS Enhances Flight Safety
  • IMDS provides valuable safety enhancement
  • Diagnostic drive train monitoring
  • In-flight alerting
  • Flight data recorder options
  • Supports systemic improvements, such as Military
    Flight Operations Quality Assurance
    (MFOQA)
  • IMDS reduces maintenance

7
Diagnostic Monitoring
  • IMDS monitors the complete
  • mechanical drive train
  • 27 gears
  • 28 shafts
  • 71 bearings
  • Automatic health calls are currently
  • not fully enabled
  • Requires adequate experience sample
  • to set appropriate triggers
  • Health calls being made by engineering, pending
    more data

8
Diagnostic Monitoring
Example SH-60B 1 High-Speed Shaft Coupling,
BuNo 161563
1 HSS Inspected and re-balanced. No visible
defect found
Replaced coupling at request of the IMDS team
Normal flight data after maintenance
9
Diagnostic Monitoring
Example CH-53E 1 Nose Gearbox, BuNo 162494
Gear tooth fragment found by chip detector
Gearbox removed
First chip detector fuzz burn-off noted
10
IMDS Success Stories
11
In-flight Alerting
  • All IMDS data is available to the crew
  • Not every IMDS find is brought to the crews
    attention in flight
  • System currently annunciates NATOPS
    exceedances
  • Alerting for imminent failures requires
  • Larger statistical sample of data
  • Rigorous safety hazard analysis
  • Expectation is that continuous,
    long-term trending will reveal failures
    early

12
Flight Data Recorder Interface
  • IMDS enables options for Cockpit Voice/Flight
    Data Recorder (CVFDR)
  • Current IMDS provides CVFDR interfaces
  • P3I version will combine the Main Processor Unit
    (MPU) with a crash-protected CVFDR
  • IMDS can provide any parameter it captures to a
    CVFDR
  • Limited only by available memory
  • IMDS data already provides
  • Complete data for every flight
  • Flight-to-flight trending
  • A powerful tool for mishap investigation

13
Military Flight Operations Quality Assurance
(MFOQA)
  • A knowledge management process
  • using flight data downloaded after every flight
  • to provide quantitative performance information
    regarding aircrew and aircraft performance
  • to improve training, operational readiness and
    safety.
  • IMDS data files support MFOQA applications
  • Sufficient parameters and data rates to be
    useable
  • No redundant data collection system required

14
IMDS Road Ahead
  • Vision for system maturation
  • Requires data from more installed systems
  • Target areas for improving the system
  • Reliable health calls throughout the mechanical
    drive train
  • Begin the move to condition based maintenance
  • Changes to maintenance concepts
  • More information in the hands of users
  • Application of HUMS as a mature tool
    in the next generation of rotorcraft

15
Cost Savings Through Diagnostics
  • Fault-based maintenance is an expensive practice
  • Reduces availability
  • Drives unscheduled maintenance
  • May involve collateral damage or flight mishap
  • Condition-based maintenance (CBM) is possible
    IF you
    can first assess condition
  • Reduced OS costs
  • Increased safety
  • Increased reliability and availability
  • More efficient use of personnel through
    application of technology

Diagnostic systems, such as IMDS, are key
enablers of CBM
16
Diagnostic Systems for the Future Helicopter
Fleet
  • NAVAIR is firmly committed to HUMS
  • Enhances current/future readiness
  • Reduces cost of doing our business
  • Improves agility of our forces

17
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