Invention Application
- Patent Title: REAR ENGINE ATTACHMENT OF AN AIRCRAFT HAVING TWO-PART RODS AND AIRCRAFT COMPRISING AT LEAST ONE SUCH REAR ENGINE ATTACHMENT
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Application No.: US16827008Application Date: 2020-03-23
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Publication No.: US20200307816A1Publication Date: 2020-10-01
- Inventor: Michael BERJOT , Jean GELIOT
- Applicant: Airbus Operations SAS
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@34b0d648
- Main IPC: B64D27/26
- IPC: B64D27/26 ; B64F5/10
Abstract:
An aircraft rear engine attachment connecting a primary structure of a pylon and an engine of an aircraft. The rear engine attachment includes first and second rods, each of them including at least two parts, a first part including at least one support orifice, accommodating a support link bar, configured to connect the rod directly or indirectly to the primary structure, at least one second part including at least one engine orifice, accommodating an engine link bar, configured to connect the rod directly or indirectly to the engine, and also detachable link elements for connecting the first and second parts oriented parallel to the direction of the rod.
Public/Granted literature
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