-
公开(公告)号:US20220033097A1
公开(公告)日:2022-02-03
申请号:US17278770
申请日:2019-10-16
申请人: VOLTAERO
发明人: Jean Botti , Didier Esteyne
摘要: An engine (100) is provided with a powertrain including a heat engine (1) and an output shaft (A1), an electric motor (2), a battery (40) for supplying the electric motor (2) and a propeller propulsion system including a propeller (3) and a propeller shaft (A3), to which the propeller (3) is coupled. The powertrain includes a system of clutches (E123, E14, E23, E324) designed for different configurations to selectively drive the propeller using the heat engine without transmission of the rotation of the electric motor to the propeller; using the electric motor without transmission of the rotation of the heat engine to the propeller; using combined transmission of the rotation of the heat engine and the rotation of the electric motor to the propeller. The electric motor includes a stator and a rotor mounted for rotation about a shaft rigidly connected, or capable of being coupled, to the propeller shaft.
-
公开(公告)号:US12030654B2
公开(公告)日:2024-07-09
申请号:US17278770
申请日:2019-10-16
申请人: VOLTAERO
发明人: Jean Botti , Didier Esteyne
CPC分类号: B64D27/24 , B64D27/10 , B64D35/02 , B64D35/08 , B64D27/026
摘要: An engine (100) is provided with a powertrain including a heat engine (1) and an output shaft (A1), an electric motor (2), a battery (40) for supplying the electric motor (2) and a propeller propulsion system including a propeller (3) and a propeller shaft (A3), to which the propeller (3) is coupled. The powertrain includes a system of clutches (E123, E14, E23, E324) designed for different configurations to selectively drive the propeller using the heat engine without transmission of the rotation of the electric motor to the propeller; using the electric motor without transmission of the rotation of the heat engine to the propeller; using combined transmission of the rotation of the heat engine and the rotation of the electric motor to the propeller. The electric motor includes a stator and a rotor mounted for rotation about a shaft rigidly connected, or capable of being coupled, to the propeller shaft.
-
公开(公告)号:US11912421B2
公开(公告)日:2024-02-27
申请号:US17614458
申请日:2020-05-27
申请人: VOLTAERO
发明人: Jean Botti , Didier Esteyne
IPC分类号: B64D27/02 , B60L50/60 , B64D27/24 , B64D31/00 , B64C27/12 , B64D35/08 , B64U50/11 , B64U50/19
CPC分类号: B64D27/02 , B60L50/60 , B64C27/12 , B64D27/24 , B64D31/00 , B64D35/08 , B64U50/11 , B64U50/19 , B60L2200/10 , B64D2027/026 , Y02T50/60
摘要: The machine, such as an aircraft, is provided with a powertrain which comprises a vaned propulsion system (3), and a thermal drive system (1), including a first thermal engine (1A) and a second thermal engine (1B), which is configured to allow the vaned propulsion system (3) to be driven. The powertrain also includes an electric drive system (2) which allows the vaned propulsion system (3) to be driven, an electrical power supply system (4) including a battery (40) which allows the electric drive system (2) to be supplied with power. A clutch system (10) allows any or each of the thermal engines (1A, 1B) to be engaged in order to drive the vaned propulsion system (3), the clutch system (10) also being configured to allow any or each of the thermal engines (1A, 1B) to be disengaged from the vaned propulsion system (3).
-
公开(公告)号:US20220234744A1
公开(公告)日:2022-07-28
申请号:US17614458
申请日:2020-05-27
申请人: VOLTAERO
发明人: Jean Botti , Didier Esteyne
摘要: The machine, such as an aircraft, is provided with a powertrain which comprises a vaned propulsion system (3), and a thermal drive system (1), including a first thermal engine (1A) and a second thermal engine (1B), which is configured to allow the vaned propulsion system (3) to be driven. The powertrain also includes an electric drive system (2) which allows the vaned propulsion system (3) to be driven, an electrical power supply system (4) including a battery (40) which allows the electric drive system (2) to be supplied with power. A clutch system (10) allows any or each of the thermal engines (1A, 1B) to be engaged in order to drive the vaned propulsion system (3), the clutch system (10) also being configured to allow any or each of the thermal engines (1A, 1B) to be disengaged from the vaned propulsion system (3).
-
-
-