Invention Grant
US09328630B2 Lateral propulsion unit for aircraft comprising a turbine engine support arch
有权
包括涡轮发动机支撑拱的飞行器的侧向推进单元
- Patent Title: Lateral propulsion unit for aircraft comprising a turbine engine support arch
- Patent Title (中): 包括涡轮发动机支撑拱的飞行器的侧向推进单元
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Application No.: US14016296Application Date: 2013-09-03
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Publication No.: US09328630B2Publication Date: 2016-05-03
- Inventor: Wolfgang Brochard , Romain Terral
- Applicant: Airbus Operations (SAS)
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations (SAS)
- Current Assignee: Airbus Operations (SAS)
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain Ltd.
- Priority: FR1258335 20120906
- Main IPC: B64D27/00
- IPC: B64D27/00 ; F01D25/24 ; B64D27/20 ; B64D27/26 ; B64D29/06
Abstract:
A propulsion unit for an aircraft, comprising one turbine engine and a mounting device for a turbine engine designed to be added laterally on an aircraft structure and comprising a rigid mounting structure. The rigid mounting structure supports at least one arch which is concave towards the longitudinal axis of the propulsion unit and which has a distal end at an angular distance of between 45 and 120 degrees from a vertical plane passing through the axis, on the other side of the structure, and supporting a distal connecting element connecting the turbine engine to the arch.
Public/Granted literature
- US20140064950A1 Lateral propulsion unit for aircraft comprising a turbine engine support arch Public/Granted day:2014-03-06
Information query
