The present invention belongs to the field of aircraft engines, and particularly, it belongs to the technical field of nacelle architecture of turbo-propeller engines. In particular, an object of the present invention is to provide an improved engine air intake of a nacelle for a turbo-propeller engine of an aircraft.
NACELLE FOR TURBO-PROPELLER ENGINES
GONDEL FÜR TURBOPROPELLERMOTOREN
NACELLE POUR TURBOPROPULSEURS
2025-06-18
Patent
Electronic Resource
English
Thrust scheduling method for variable pitch fan engines and turbo-shaft, turbo-propeller engines
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European Patent Office | 2017
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European Patent Office | 2017
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