Methods for reducing flow-around noise on aircraft landing gears

LEGATO

Numerically determined alternating pressure field of a 2-wheel main landing gear (Arrows point to possible intense acoustic sources),

In the LEGATO joint project funded by the German Federal Ministry of Economics and Climate Action (BMWK), project partners from industry and science are developing technologies to reduce noise, emissions and resource consumption over the entire undercarriage product life cycle. In addition to classic landing gear topics such as actuation, production and repair, the focus is for the first time on noise generation on the undercarriage. The aim of the project is to establish a digital process chain for identifying and avoiding or mitigating acoustic sources on the nose and main landing gears of short- and medium-range aircraft. In a digital process chain, acoustic sources are first identified on a landing gear using numerical methods (Computational Aero Acoustic (CAA)). Based on this, the project partners develop noise reduction concepts and investigate their effectiveness. The primary focus of the research is on changes to the shape of landing gear components or modifications to the landing gear architecture. 

The DLR Institute of Aerodynamics and Flow Technology is working on the so-called "noise-optimized landing gear" in LEGATO together with the joint venture leader Liebherr Aerospace Lindenberg (LLI). The PIANO and DISCO methods developed by DLR and the externally developed Lattice-Boltzmann method ProLB are used. To validate the numerical results, the project participants will measure all variants of nose and main landing gear simulated using CAA methods in the Aeroacoustic Wind Tunnel Braunschweig. The final results are evaluated by LLI with regard to their feasibility on the product and by the DLR Institute of Aerodynamics and Flow Technology with a focus on the achieved noise reduction.

Project
LEGATO - Low Noise Landing Gear with Electromechanical Actuation and Sustainable 
Term
4/2023 - 3/2026
Partners
  • DLR Institute of Aerodynamics and Flow Technology
  • Liebherr-Aerospace Lindenberg GmbH (Leader)
  • BIAS - Bremer Institut für angewandte Strahltechnik GmbH
  • Boll Automation GmbH
  • ILT Fraunhofer
  • IWS Fraunhofer
  • Technische Universität Hamburg (TUH)
 Funding

Federal Ministry of Economic Affairs and Climate Action (BMWK), Aviation Research Program (LuFo VI-3), ref. no. 20Y2205B

Contact

Institute of Aerodynamics and Flow Technology