Safran Landing Systems proposes a global solution for landing, braking, steering and monitoring systems, as well as a wide range of electro-hydraulic or all-electric equipments, from design to assemby and integration onto the aircraft.
Aircraft Landing Gear Layouts and FunctionsSunil BhatVinod MogerJETIR(www.jetir.org)
the trend is to use carbon disk brakes. For other landing gear components, high strength steel is used for its robustness properties. The constant effort to develop new economic, lightweight, durable, robust materials for landing gear made it possible to replace some of its steel components by...
As well as the standard CMS functions, the LGCIU menu includes a specific page.The LGCIU SIMULATION function is displayed on the second MCDU screen, which is accessible through the scrolling keys.Using the first left key enables access to the LANDING GEAR SIMULATION.Using the second left key ...
Crane A&E launched the first antiskid brake system in 1947. Today, Crane's brake control systems, hydraulic landing gear components and landing gear proximity indication systems are part of various aircraft globally.
it is obvious that equivalent alterations and modifications will occur to others skilled in the art upon the reading and understanding of this specification and the annexed drawings. In particular regard to the various functions performed by the above described integers (components, assemblies, devices...
an electric taxi system with system components mounted within one or more nose or main landing gear wheels of an aircraft, wherein said electric taxi system components comprise at least an electric drive motor, an activatable drive system, and a source of electric power for said electric taxi ...
Confidential and proprietary document. DGLR Hamburg June 2008 Page 3 A380 Landing Gear Systems – An Overview Major Components and Systems 4ATA Chapter 32 Landing Gear Systems 4Gears – Nose Landing Gear (2 Wheels) – Body Landing Gear x2 (Bogie Type, 6 Wheels - 4 Braked) – Wing Landing...
the shock and vibration are dissipated throughout the fuselage structure. The shock loading also creates undesirable noise and vibrations for any passengers of the aircraft. Also, the shock loading and vibration may reduce the life of systems or structural components mounted on the landing gear ...
As an alternate method of measuring the amount of landing gear strut compression, the landing gear components have various unique physical features on both the upper stationary portion of strut body 3 as well as the lower telescopic piston 5, that are easily identified in photographs and can be...