Invention Grant
US09346551B2 Engine installation 有权
发动机安装

Engine installation
Abstract:
A fuselage mounted gas turbine engine installation the installation includes at least one propeller stage and a gas turbine core arranged in use to drive the propeller stage. The core is external to the fuselage and the rotational axes of the core and propeller stage are offset with respect to each other.
Public/Granted literature
Information query
Patent Agency Ranking
0/0