Invention Application
- Patent Title: TURBINE ENGINE WITH FAN AND REDUCTION OF SPEED ON THE SHAFT OF THE POWER TURBINE
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Application No.: US15765450Application Date: 2016-10-05
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Publication No.: US20180306121A1Publication Date: 2018-10-25
- Inventor: Augustin Marc Michel Curlier
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Priority: FR1559444 20151005; FR1559445 20151005
- International Application: PCT/FR2016/052562 WO 20161005
- Main IPC: F02C7/36
- IPC: F02C7/36 ; F01D15/12 ; F02C3/107 ; F16H1/20
Abstract:
The present invention relates to an aircraft propulsion assembly comprising a turbine (15), at least one fan (10) and a mechanism for transmitting power between the turbine and the fan, characterized in that the power transmission mechanism comprises a speed reducer (20) with a motion input and a motion output, the input being in the continuation of the axis (16) of the turbine and the output connected to the fan.
Public/Granted literature
- US11022043B2 Turbine engine with fan and reduction of speed on the shaft of the power turbine Public/Granted day:2021-06-01
Information query
IPC分类:
