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US 2021/0172368 A1Published application
Integrated hybrid power apparatus
AssigneeKorea Aerospace Research Institute
InventorsKeun Bae KIM, Byeong Gyu GANG
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Abstract
An integrated hybrid power apparatus provided in a flying body includes a generator including a stator and a rotor, at least one engine disposed adjacent to the generator and including a cylinder, and a cooler configured to cool the generator and the engine and perform water-cooling that allows a coolant to circulate in the generator and the engine.
Claims10
An integrated hybrid power apparatus provided in a flying body, comprising:
- a generator comprising a stator and a rotor;
- at least one engine disposed adjacent to the generator and comprising a cylinder;
- and
- a cooler configured to cool the generator and the engine,
- wherein the cooler performs water-cooling that allows a coolant to circulate in the generator and the engine.
2 more elements
An integrated hybrid power apparatus provided in a flying body, comprising:
- a generator comprising a stator comprising a magnetic substance, and a rotor disposed on an outer side of the stator and comprising a magnetic substance;
- and
- a first engine and a second engine that are disposed on both sides of the generator,
- wherein the first engine and the second engine are disposed symmetrically with respect to the generator.
1 more element
Dependencies are inferred from the claim text.