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
2020-07-28
Patent
Electronic Resource
English
Rotorcraft Convertible Engine Study
NTIS | 1983
|Rotorcraft Convertible Engine Study
NTIS | 1982
|Rotorcraft convertible engine study
NTRS | 1983
|Rotorcraft convertible engine study
NTRS | 1982
|