Master'sDefense, Military Engineering & Land Systems Applications open

Master’s in Rotorcraft Transmissions and Gearboxes Engineering

Online master's programme of 1,900 hours in rotorcraft transmission and gearbox engineering, with 12 modules covering transmission architecture, gear design to ISO 6336 and AGMA, epicyclic trains, bearings and shafts, lubrication and tribology, materials, dynamics, HUMS, CS-29 testing and certification, and root cause analysis, with an assigned technical tutor.

Duration1900 h
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute diploma
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Learning outcomes

What you will be able to do

01

Analyse the architecture of rotorcraft transmissions.

02

Design gears and epicyclic trains according to standards.

03

Select bearings, shafts and lubrication systems.

04

Specify gear materials and manufacturing processes.

05

Analyse the dynamics and vibration of transmissions.

06

Implement health monitoring and fault diagnosis.

07

Plan certification testing and maintenance.

Profile

Who it's for

  • Transmission engineers designing main, intermediate and tail gearboxes.
  • Gear engineers applying ISO 6336 and AGMA methods.
  • Tribology engineers working on lubrication, micropitting and scuffing.
  • HUMS analysts interpreting gear and bearing condition indicators.
  • Transmission test engineers running endurance and loss-of-lubrication tests.
  • Failure analysis engineers investigating root causes in drive systems.
  • Engineering or science graduates seeking to enter the aerospace industry.
Standards & tools

What you'll work with

  • ISO 6336 (calculation of load capacity of gears)
  • CS-29 (EASA certification specifications for large rotorcraft)
  • ANSI/AGMA 2001-D04 (rating factors for spur and helical gear teeth)
  • ISO 281 (rolling bearings: dynamic load ratings and rating life)
  • CAP 753 (helicopter health and usage monitoring, UK CAA)
  • EMAR 21 (European military airworthiness requirements)
  • SAE AS9100D (quality management systems for aviation, space and defence)
  • KISSsoft
  • Romax
  • Ansys Mechanical
  • MATLAB
  • MASTA (SMT)
Syllabus

12 modules · 1900 h

  1. 1.1Function of the transmission system
  2. 1.2Main gearbox
  3. 1.3Intermediate and tail gearboxes
  4. 1.4Drive shafts and couplings
  5. 1.5Freewheel and autorotation
  6. 1.6Driven accessories
  7. 1.7Typical reduction ratios
  8. 1.8Weight and power density requirements
  9. 1.9Tandem, coaxial and tiltrotor configurations
  10. 1.10Case study: analysis of the transmission architecture of a medium helicopter
  1. 2.1Geometry of spur and helical gears
  2. 2.2Spiral bevel gears
  3. 2.3Planetary gears
  4. 2.4Face gears
  5. 2.5Load capacity according to ISO 6336
  6. 2.6AGMA design standards
  7. 2.7Contact and bending stresses
  8. 2.8Profile and lead modifications
  9. 2.9Weight optimisation
  10. 2.10Lab: load capacity calculation of a gear according to ISO 6336
  1. 3.1Kinematics of planetary trains
  2. 3.2Load sharing between planets
  3. 3.3Flexible mountings
  4. 3.4Dynamics of planetary trains
  5. 3.5Mesh frequencies
  6. 3.6Characteristic failures
  7. 3.7Planet carrier design
  8. 3.8Lubrication of planetaries
  9. 3.9Load sharing tests
  10. 3.10Practical: load sharing model of a planetary
  1. 4.1Types of bearings in transmissions
  2. 4.2Bearing life according to ISO 281
  3. 4.3High-speed bearings
  4. 4.4Bearings integrated into gears
  5. 4.5Hollow shafts and their design
  6. 4.6Flexible couplings
  7. 4.7Supercritical tail drive shafts
  8. 4.8Shaft dampers
  9. 4.9Bearing failures
  10. 4.10Case study: design of a tail drive shaft
  1. 5.1Lubrication regimes
  2. 5.2Elastohydrodynamic lubrication
  3. 5.3Turbine and transmission oils
  4. 5.4Pressurised lubrication systems
  5. 5.5Operation with loss of oil
  6. 5.6Dry-running requirements
  7. 5.7Micropitting and scuffing
  8. 5.8Filtration and debris detection
  9. 5.9Oil analysis
  10. 5.10Lab: EHL film thickness calculation
  1. 6.1Carburising steels
  2. 6.2Heat treatment of gears
  3. 6.3Shot peening and surface finishing
  4. 6.4Gear grinding
  5. 6.5Magnesium and aluminium housings
  6. 6.6Corrosion in housings
  7. 6.7Additive manufacturing in transmissions
  8. 6.8Gear quality control
  9. 6.9Magnetic particle inspection
  10. 6.10Practical: specification of a carburising process
  1. 7.1Transmission error
  2. 7.2Mesh excitation
  3. 7.3Dynamic models of transmissions
  4. 7.4Gearbox noise
  5. 7.5Housing response
  6. 7.6Critical speeds of shafts
  7. 7.7Misalignment
  8. 7.8Interaction with the fuselage
  9. 7.9Vibration measurement
  10. 7.10Lab: spectral analysis of gear mesh vibration
  1. 8.1HUMS architecture
  2. 8.2Accelerometers and tachometers
  3. 8.3Synchronous averaging
  4. 8.4Gear condition indicators
  5. 8.5Bearing indicators
  6. 8.6Chip detectors
  7. 8.7Thresholds and alerts
  8. 8.8Remaining useful life prognosis
  9. 8.9Lessons from related accidents
  10. 8.10Practical: calculation of condition indicators with real data
  1. 9.1CS-29 transmission requirements
  2. 9.2Endurance testing
  3. 9.3Loss-of-lubrication testing
  4. 9.4Overtorque testing
  5. 9.5Regenerative test rigs
  6. 9.6Component fatigue testing
  7. 9.7Material qualification
  8. 9.8Management of non-conformities
  9. 9.9Military airworthiness requirements
  10. 9.10Case study: certification test plan for a main gearbox
  1. 10.1Gear failure modes
  2. 10.2Bearing failures
  3. 10.3Housing cracks
  4. 10.4Lubrication failures
  5. 10.5Fractography
  6. 10.6Metallurgical analysis
  7. 10.7Accident investigation
  8. 10.8Corrective actions
  9. 10.9Airworthiness directives
  10. 10.10Workshop: root cause analysis of a planetary failure
  1. 11.1Time between overhauls
  2. 11.2Condition-based maintenance
  3. 11.3Transmission overhaul
  4. 11.4Gear repair
  5. 11.5Management of life-limited components
  6. 11.6Life-cycle cost
  7. 11.7Obsolescence
  8. 11.8Sustainability and lubricants
  9. 11.9Safety and professional ethics
  10. 11.10Practical: maintenance plan for a transmission
  1. 12.1Transmission requirements
  2. 12.2Conceptual design
  3. 12.3Gear and bearing calculations
  4. 12.4Dynamic analysis
  5. 12.5Lubrication strategy
  6. 12.6Test plan
  7. 12.7Monitoring plan
  8. 12.8Conclusions
  9. 12.9Master's Thesis report
  10. 12.10Master's Thesis: defence before a panel
Methodology, software & labs

How you'll learn

The programme is delivered 100% online on the SEIUM campus, with downloadable material, recorded classes and an assigned technical tutor. There are no fixed timetables: you progress at your own pace within each intake, making it compatible with work.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is KISSsoft, Romax, Ansys Mechanical, MATLAB and MASTA (SMT), in free, academic or evaluation versions. Testing is studied through real procedures for gear and bearing load capacity calculation, vibration analysis and HUMS monitoring, and root cause analysis of transmission failures. Assessment is continuous by module, plus the final Master's Thesis.

Standards covered: ISO 6336, CS-29, ANSI/AGMA 2001-D04, ISO 281, CAP 753, EMAR 21 and SAE AS9100D.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of ISO 6336, CS-29 and ANSI/AGMA 2001-D04 applied to real cases, not as a theoretical annex.
Industry software:KISSsoft, Romax, Ansys Mechanical, MATLAB and MASTA (SMT), in free, academic or evaluation versions.
Master's Thesis with defence:a complete rotorcraft transmission project covering conceptual design, gear and bearing calculations, dynamic analysis, lubrication strategy, and test and monitoring plans, defended before a panel.
Flexible format:100% online, no fixed timetables, compatible with full-time work.
Capstone project

Build it end to end

Your final project follows the real engineering workflow, step by step, reviewed by your tutor.

Gear rating
Calculate the load capacity of gears according to ISO 6336.
Planetary load sharing
Model load sharing in a planetary train and size its bearings.
Lubrication and vibration
Calculate EHL film thickness and analyse gear mesh vibration spectra.
Certification and HUMS plan
Draw up a main gearbox certification test plan and a HUMS monitoring plan.
Master's Thesis
Develop a complete rotorcraft transmission project, defended before a panel.
Career opportunities

Where this takes you

Transmission engineerGear engineerTribology engineerHUMS analystTransmission test engineerFailure analysis engineer
Admissions & scholarships

Requirements

  • University degree in engineering, science or architecture, or equivalent demonstrable professional experience.
  • Internet connection and a computer capable of running the programme software.
  • English sufficient to read technical standards.

Ready to start?

Send your application today. Our admissions team replies within 72 hours with your study plan and funding options.

FAQ

Frequently asked questions

The programme totals 1,900 hours over 12–14 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.

You work with KISSsoft, Romax, Ansys Mechanical, MATLAB and MASTA (SMT), using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.

A SEIUM Institute diploma, awarded on passing the continuous assessment and the Master's Thesis. It is SEIUM's own qualification, not an official state degree; its recognition depends on the programme completed and the regulations of each country.

Yes. Modules passed in a course or postgraduate diploma in the same area are recognised in the higher programme. Ask about the recognition policy when you enrol.

A university degree in engineering, science or architecture (or equivalent professional experience), a computer able to run the programme software, and English sufficient to read technical standards.

Start dates are set by SEIUM's faculty for each intake. Our admissions team will confirm the next available date when you apply.

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