Shellless shaftless high-pressure high-speed starting power generation device for aero-engine

The invention discloses a shellless shaftless high-pressure high-speed starting power generation device for aero-engines. The shellless shaftless high-pressure high-speed starting power generation device comprises a shellless stator assembly 3, a shaftless rotor assembly 2 and a rotating speed senso...

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Main Authors CAO ZHILIANG, SHEN XUESONG, ZHU XUEZHONG, LUO ZAIQI, YANG SHAO, CAO QINGYUAN, QIAN XINGLIANG, QU XIONGFEI, GUO XIAOFENG, CHEN WEIWEI, LIU JIHUA, GOU XUEZHONG, CHEN LI, WANG XIAOHUI
Format Patent
LanguageChinese
English
Published 01.03.2019
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Abstract The invention discloses a shellless shaftless high-pressure high-speed starting power generation device for aero-engines. The shellless shaftless high-pressure high-speed starting power generation device comprises a shellless stator assembly 3, a shaftless rotor assembly 2 and a rotating speed sensor assembly. The shellless stator assembly is arranged on a dedicated inner wall between an engine case 1 or an air compressor outlet and a combustion chamber. The shaftless rotor assembly 2 is free of a bearing, and is arranged on an engine shaft 5, the shaftless rotor assembly 2 is powered by an externally provided power source to generate electromagnetic torque to drive the engine shaft 5 to rotate during starting, when the given rotating speed is reached during starting, the state is converted to a power generation state through a controller, and the engine shaft 5 drives the shaftless rotor assembly 2 to rotate to generate power. The power generation quality is adjusted through the controller, and a monitoring
AbstractList The invention discloses a shellless shaftless high-pressure high-speed starting power generation device for aero-engines. The shellless shaftless high-pressure high-speed starting power generation device comprises a shellless stator assembly 3, a shaftless rotor assembly 2 and a rotating speed sensor assembly. The shellless stator assembly is arranged on a dedicated inner wall between an engine case 1 or an air compressor outlet and a combustion chamber. The shaftless rotor assembly 2 is free of a bearing, and is arranged on an engine shaft 5, the shaftless rotor assembly 2 is powered by an externally provided power source to generate electromagnetic torque to drive the engine shaft 5 to rotate during starting, when the given rotating speed is reached during starting, the state is converted to a power generation state through a controller, and the engine shaft 5 drives the shaftless rotor assembly 2 to rotate to generate power. The power generation quality is adjusted through the controller, and a monitoring
Author WANG XIAOHUI
CHEN LI
SHEN XUESONG
QIAN XINGLIANG
CAO ZHILIANG
LIU JIHUA
GUO XIAOFENG
YANG SHAO
CHEN WEIWEI
LUO ZAIQI
ZHU XUEZHONG
CAO QINGYUAN
GOU XUEZHONG
QU XIONGFEI
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– fullname: ZHU XUEZHONG
– fullname: LUO ZAIQI
– fullname: YANG SHAO
– fullname: CAO QINGYUAN
– fullname: QIAN XINGLIANG
– fullname: QU XIONGFEI
– fullname: GUO XIAOFENG
– fullname: CHEN WEIWEI
– fullname: LIU JIHUA
– fullname: GOU XUEZHONG
– fullname: CHEN LI
– fullname: WANG XIAOHUI
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DocumentTitleAlternate 种航空发动机用无壳无轴高压高速起动发电装置
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Snippet The invention discloses a shellless shaftless high-pressure high-speed starting power generation device for aero-engines. The shellless shaftless high-pressure...
SourceID epo
SourceType Open Access Repository
SubjectTerms AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
DYNAMO-ELECTRIC MACHINES
ELECTRICITY
GAS-TURBINE PLANTS
GENERATION
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
Title Shellless shaftless high-pressure high-speed starting power generation device for aero-engine
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