AIRCRAFT ENGINE UNIT Russian patent published in 2012 - IPC B64D27/26

Abstract RU 2469917 C2

FIELD: aircraft engineering.

SUBSTANCE: proposed unit comprises turbojet 1 including blower cowl 3 and engine cowling 5, turbojet pylon and engine suspension. The latter comprises two front suspension connection rods 9, two rear suspension rods 11 and connection rod to take up thrust force that extends between engine cowling front part 17 and pylon 7 in the plane including axis A of said turbojet 1. Extra connection rod 19 is arranged between blower cowl 3 and pylon 6, parallel with said axis A.

EFFECT: decreased deformation of engine shaft.

8 cl, 7 dwg

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RU 2 469 917 C2

Authors

Baillard Andre

Dates

2012-12-20—Published

2008-08-28—Filed