DEVICE FOR TESTING MEMBERS FOR CONTROLLING WING Russian patent published in 1994 - IPC

Abstract SU 1522885 A1

FIELD: aircraft engineering. SUBSTANCE: device has parallelogram mechanism and is coupled with leading-edge slat 10 to be tested through hydraulic cylinders 7,8 and with movable base 2 through rockers 4,5. One rotates base 2 synchronously with leading-edge slat 10 to be tested. In so doing axes of rotation of leading-edge slat 10 and base 2 are coincident. In addition rocker 4 reciprocates with respect to link 11 simultaneously. EFFECT: enhanced reliability. 3 dwg

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SU 1 522 885 A1

Authors

Sumarokov V.A.

Ljubimov G.E.

Kurushin V.M.

Dates

1994-12-15—Published

1988-04-05—Filed