A turboprop or turboshaft engine comprises a first spool including a first compressor drivingly connected to a first turbine, the first turbine further drivingly connected to a load. The engine comprising a second spool including a second compressor drivingly connected to a second turbine, the second compressor fluidly connected to the first compressor to receive compressed air therefrom. The engine further comprises a third spool including a third compressor drivingly connected to a third turbine, the third compressor fluidly connected to the second compressor to receive compressed air therefrom.
SPLIT COMPRESSOR SYSTEM ON MULTI-SPOOL ENGINE
SYSTEME DE COMPRESSEUR BIBLOC SUR MOTEUR MULTICORPS
2020-03-12
Patent
Electronic Resource
English
Cooled-Spool Piston Compressor
Online Contents | 1994
Cooled-Spool Piston Compressor
NTRS | 1994
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