A gas turbine engine for an aircraft with an engine shaft which is in operative connection with auxiliary units. The operative connection includes interengaging gear wheels. At least one gear wheel of the operative connection is configured as a beveloid gear wheel.
GAS TURBINE ENGINE FOR AN AIRCRAFT WITH AN ENGINE SHAFT
2020-03-19
Patent
Electronic Resource
English
COMPOUND ENGINE ASSEMBLY WITH OFFSET TURBINE SHAFT, ENGINE SHAFT AND INLET DUCT
European Patent Office | 2023
|