METHOD FOR PROTECTING AIRCRAFT POWER PLANT FROM NEGATIVE THRUST IN FLIGHT
SEAL SYSTEM FOR GAPS WITH VARIABLE GEOMETRY IN AIRCRAFT SYSTEMS
SYSTEMS AND METHODS FOR PREVENTING FORMATION OF ICE ON AIRCRAFT PARTS
QUICK-RELIEF DEVICE FOR ENGINE WITH FREE AIRCRAFT TURBINE
METHOD (EMBODIMENTS) AND ENGINE COOLING SYSTEM CONTROL SYSTEM
SYSTEM AND METHOD FOR PROTECTING STRENGTH OF MOTOR PYLON
HOUSING STRUCTURE, INSTALLED BETWEEN THE ENGINE AND THE NACELLE USING THE PLATE WITH SCREWS