REAR BAND GAS-TURBINE ENGINE SUSPENSION SYSTEM Russian patent published in 1994 - IPC

Abstract RU 2005667 C1

FIELD: aviation. SUBSTANCE: rear band of engine suspension system mounted on pylon 1 with tenon 2 is provided with two additional inclined rods 8 articulated in one plane with side rods 6 (between them) and forming bush 10 together with drawbar attachment unit. Bush 10 is provided with spherical bearing 11 embracing tenon 2 of pylon 1. Units connecting side rods to pylon are provided with conical journals 3 and bearings 7. In mounting the engine, tenon 2 of pylon enters bearing 11 of rear band of suspension. Free motion of tenon 2 in bearing 11 provides for easy mounting of suspension system rods. EFFECT: facilitated assembly jobs and enhanced reliability of suspension system. 3 dwg

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RU 2 005 667 C1

Authors

Kocherov E.P.

Belov V.E.

Tibatin N.M.

Leushina L.I.

Suslikov V.I.

Dates

1994-01-15—Published

1992-06-05—Filed