DEVICE FOR TURBOJET ENGINE Russian patent published in 2016 - IPC B64D27/26

Abstract RU 2585368 C2

FIELD: aviation.

SUBSTANCE: invention relates to aircraft engineering, particularly, to suspension of turbojet engines. Device for suspension of turbojet engine includes an attachment with articulated links. Attachment comprises holder, having three branches with passages, through which pin passes. Pin is oriented parallel to direction, which is tangential to housing, and pivotally connected to the central branch of holder by means of ball joint.

EFFECT: possibility to hold a fan of increased diameter.

6 cl, 3 dwg

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RU 2 585 368 C2

Authors

Balk Vuter

Vensan Toma Alen Kristian

Dates

2016-05-27—Published

2011-12-20—Filed