Ferry flight engine fairing kit

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/00 (2006.01) B64D 27/10 (2006.01) B64F 5/00 (2006.01) F02C 7/20 (2006.01)

Patent

CA 2647753

A fairing kit for a gas turbine engine, where the engine has a core gas turbine engine (13), a fan rotor (26), and a plurality of external fan blades (24) attached to the fan rotor (26) and powered by the core gas turbine engine (13). The core gas turbine engine (13) has an annular splitter (34) for directing a portion (50) of incoming airflow into the core gas turbine engine (13). The fairing kit comprises: a) a fairing (80); b) a plurality of fasteners (88) for securing the fairing (80) to the core gas turbine engine (13); and c) a conformable seal (86) for sealing mating surfaces of the fairing (80) and the core gas turbine engine (13).

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