A rotorcraft includes at least one first engine operatively connected to a first rotor, and a second engine operatively connected to at least one of a second rotor or an electrical generator for driving an electrical system, wherein the second engine is a different size than the first engine. The second engine can be smaller than the at least one first engine, for example.
ENGINE SYSTEMS FOR ROTORCRAFT
16.08.2018
Patent
Elektronische Ressource
Englisch
Rotorcraft convertible engine study
NTRS | 1983
|Rotorcraft Convertible Engine Study
NTIS | 1983
|Rotorcraft Convertible Engine Study
NTIS | 1982
|Rotorcraft convertible engine study
NTRS | 1982
|