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Richard G Stretton: Engine core stand arrangement and method of removal and transportation of an engine core. Rolls-Royce, Oliff & Berridge, August 10, 2010: US07770292 (21 worldwide citation)

Transportation of larger diameter gas turbine engines can be problematic. In such circumstances it is known to separate the fan assembly (30) from the engine core (1) and other parts to facilitate transportation. Separation of the fan assembly (30) and engine core (1) can require a gantry which adds ...


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Stretton Richard Geoffrey: An engine core stand arrangement and method of removal and transportation of an engine core. Rolls-Royce, January 16, 2008: EP1878662-A1 (5 worldwide citation)

Transportation of larger diameter gas turbine engines can be problematic. In such circumstances it is known to separate the fan assembly (30) from the engine core (1) and other parts to facilitate transportation. Separation of the fan assembly (30) and engine core (1) can require a gantry which adds ...


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Richard G Stretton: Engine core stand arrangement and method of removal and transportation of an engine core. Rolls-Royce, Oliff & Berridge, January 17, 2008: US20080011932-A1

Transportation of larger diameter gas turbine engines can be problematic. In such circumstances it is known to separate the fan assembly (30) from the engine core (1) and other parts to facilitate transportation. Separation of the fan assembly (30) and engine core (1) can require a gantry which adds ...


5
Stretton Richard Geoffrey: An engine core stand arrangement and method of removal and transportation of an engine core. Rolls-Royce, pengwu, January 16, 2008: CN200710129163

Transportation of larger diameter gas turbine engines can be problematic. In such circumstances it is known to separate the fan assembly ( 30 ) from the engine core ( 1 ) and other parts to facilitate transportation. Separation of the fan assembly ( 30 ) and engine core ( 1 ) can require a gantry wh ...


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