- Patent Title: Aircraft comprising at least one engine assembly linked to the fuselage of the aircraft by two connecting rods positioned at least partially in an air inlet of the engine assembly
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Application No.: US16173190Application Date: 2018-10-29
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Publication No.: US11084596B2Publication Date: 2021-08-10
- Inventor: Eric Bouchet , Jérôme Colmagro , Michel Garcia
- 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: FR1760258 20171030
- Main IPC: B64D27/26
- IPC: B64D27/26 ; B64D27/20 ; B64D27/14 ; B64D29/06 ; B64C7/02
Abstract:
An aircraft which comprises a fuselage and at least one propulsion assembly linked to the fuselage by at least two connecting rods positioned at least partially in an inner zone of the air inlet of the nacelle of the propulsion assembly. Thus, the connecting rods do not interfere with the secondary flow flowing inside the nacelle and do not affect the aerodynamic performance levels of the propulsion assembly.
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