Invention Grant
- 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.: US11022043B2Publication Date: 2021-06-01
- 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
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: FR1559444 20151005,FR1559445 20151005
- International Application: PCT/FR2016/052562 WO 20161005
- International Announcement: WO2017/060623 WO 20170413
- Main IPC: F02C7/36
- IPC: F02C7/36 ; F01D15/12 ; F02C3/107 ; F16H1/20 ; B64D35/02
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
- US20180306121A1 TURBINE ENGINE WITH FAN AND REDUCTION OF SPEED ON THE SHAFT OF THE POWER TURBINE Public/Granted day:2018-10-25
Information query
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