NANNY

Innovative propulsion and lift systems for the next generation of light to medium-weight helicopters

NANNY

The overall goal of the NANNY joint project is the further development of propulsion and lift systems for the next generation of light to medium-weight helicopters. The DLR contribution comprises the improvement of the prediction accuracy of phenomena in the field of rotor-structure coupling and the associated stability analysis.

Motivation and background

DLR is making an important contribution to high-performance and efficient aviation by improving the simulation methods for design and verification and thus optimising the overall design. In particular, the prediction of rotor-structure coupling phenomena early in the design and before prototype production is important for the efficiency of the overall design in order to avoid subsequent changes. Such phenomena can lead to high vibration input, structural fatigue or even instability and failure. By linking complex structural dynamic and aerodynamic models, the accuracy of predictions can be improved and the helicopter can be better designed at the design stage. Any subsequent changes as countermeasures for problems that arise would have a negative impact on the development time and, if additional damping elements were required, also on the weight and therefore on the performance, efficiency and costs of the helicopter as a whole.

Challenges

The long-term research topic is the complete digitalisation of the helicopter development process. The aeromechanical design process must be fully integrated into the design of the overall helicopter. Further increases in performance and cost reductions can be achieved through holistic optimisation of the overall helicopter system, including all relevant operating conditions. Finally, digital testing and, if necessary, simulation-based certification of helicopters and eVTOLs will significantly reduce the technical and economic development risk as well as the development time.

Objective

  • Linearised geometrically accurate beam model for the rotor simulation code Versatile Aeromechanics Simulation Tool (VAST). Evaluation of accuracy and numerical stability compared to non-linear modelling.
  • Improved modelling of viscous effects. Implementation and testing of modelling for boundary layer displacement and viscous profile wakes in the panel method UPM developed by DLR.
  • Aeromechanical overall model for stability analyses. Time-step accurate coupling of the UPM panel method with the Simpack multi-body simulation software and the VAST helicopter simulation method as tools for aeromechanical analyses and stability prediction.
  • Aeroelastic stability assessment. Accurate evaluation of an aeroelastic helicopter model using innovative identification-based analysis methods.
  • Concept study of damping enhancement. Design of damping in the transfer path between main gearbox and airframe.

Project

NANNY - Innovative propulsion and lift systems for the next generation of light to medium-weight helicopters

Duration

09/2021 - 12/2025

Partners

  • Airbus Helicopters Deutschland (joint project lead)
  • DLR Institute of Aeroelasticity (project lead)
  • DLR Institute of Aerodynamics and Flow Technology
  • DLR Institute of Flight Systems
  • DLR Institute of Software Technology

Type of project

Research project in the aviation research program VI-2

Funding organisations

Federal Ministry for Economic Affairs and Climate Action (BMWK) over Projektträger Jülich (PTJ)

Contact

Dipl.-Ing. Jürgen Arnold

Group leader Aeroelastic Stability and System Response
German Aerospace Center (DLR)
Institute of Aeroelasticity
Bunsenstraße 10, 37073 Göttingen
Germany