Integrated starter-generator of modular design includes a stator, a rotor connected to the output shaft of the gas turbine engine, a cooling system with cooling air supply and removal channels
2024-03-01
专利权人FEDERAL STATE BUDGETARY EDUCATIONAL (BUDG-Non-standard)
申请日期2024-03-01
专利号RU2823626-C1
成果简介NOVELTY - Invention relates to aircraft engineering, particularly, to devices for starting an aircraft engine and aircraft onboard power supply. Integrated starter-generator of the gas turbine engine includes a stator, a rotor connected to the output shaft of the gas turbine engine, a cooling system with cooling air supply and removal channels. Integrated starter-generator is made modular and comprises a housing in which a stator with a winding and a sealed cylindrical insert is fixed, rotor with permanent magnets pressed to it by bandage, fixed on hub by means of coupling, and installed with possibility of rotation relative to stator in front and rear end shields attached to housing. At the same time the rear end shield is made in the form of a flange, and the cooling system is combined with air and liquid coolant supply and discharge channels. USE - Aviation. ADVANTAGE - Improving reliability, energy efficiency and simplifying maintenance.
IPC 分类号F02C-007/12 ; H02K-009/197
国家俄罗斯
专业领域能源矿产
语种英语
成果类型专利
文献类型科技成果
条目标识符http://119.78.100.226:8889/handle/3KE4DYBR/17919
专题中国科学院新疆生态与地理研究所
作者单位
FEDERAL STATE BUDGETARY EDUCATIONAL (BUDG-Non-standard)
推荐引用方式
GB/T 7714
ISMAGILOV F R,VAVILOV V E,OKHOTNIKOV M V,et al. Integrated starter-generator of modular design includes a stator, a rotor connected to the output shaft of the gas turbine engine, a cooling system with cooling air supply and removal channels. RU2823626-C1[P]. 2024.
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