Invention Grant
- Patent Title: Turbojet engine with offset fans with a differential system
-
Application No.: US15284329Application Date: 2016-10-03
-
Publication No.: US10247108B2Publication Date: 2019-04-02
- Inventor: Augustin Marc Michel Curlier , Sebastien Courtois
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Womble Bond Dickinson (US) LLP
- Priority: FR1559446 20151005
- Main IPC: F02C7/36
- IPC: F02C7/36 ; F16H48/08 ; F01D5/02 ; F02C3/04 ; F04D29/053 ; F04D29/32 ; F02C3/107 ; F02C3/113
Abstract:
A propulsion unit of an aircraft including a turbine (15), at least one fan (10) with an axis offset relative to the axis of the turbine and a power transmission mechanism between the turbine and the fan. The power transmission mechanism includes a speed reducing gear (20) with an input and a movement output, the input being in the extension of the axis (16) of the turbine and the output connected to the fan.
Public/Granted literature
- US20170096942A1 TURBOJET ENGINE WITH OFFSET FANS WITH A DIFFERENTIAL SYSTEM Public/Granted day:2017-04-06
Information query
IPC分类:
