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- W1995080240 abstract "An integrated engine-generator for aircraft secondary power generation is described. The concept consists of an electric generator located inside a turbojet or turbofan engine and both concentric with and driven by one of the main engine shafts. The electric power conversion equipment and generator controls are located in the aircraft. When properly rated, the generator serves as an engine starter as well as a source of electric power. This configuration reduces or eliminates the need for an external gear box on the engine and permits reduction in the nacelle diameter." @default.
- W1995080240 created "2016-06-24" @default.
- W1995080240 creator A5033890346 @default.
- W1995080240 date "1972-08-16" @default.
- W1995080240 modified "2023-09-24" @default.
- W1995080240 title "Integrated engine-generator for aircraft secondary power" @default.
- W1995080240 cites W2098893947 @default.
- W1995080240 doi "https://doi.org/10.2514/6.1972-1056" @default.
- W1995080240 hasPublicationYear "1972" @default.
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