07 - Systems, Subsystems and Equipment
DEVELOPMENT OF AN ELECTRO-HYDROSTATIC NOSE LANDING GEAR ACTUATION AND STEERING SYSTEM
M.N. Duval¹, T. Lammering¹; ¹Liebherr-Aerospace Lindenberg GmbH, Germany
A self-sufficient, electro-hydrostatic based solution is proposed for to perform all functions of the nose landing gear of an aircraft. rnThe system works solely on electric power, and thus is an important brick towards the electrification of future aircraft.rnThe development process from concept selection to functional demonstrator in a representative environment is described.rn