TORQUE CONSTRICTOR FOR AIRCRAFT TURBOJET NACELLE DRIVE Russian patent published in 2015 - IPC F16H25/20 F02K1/76 

Abstract RU 2538476 C2

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering. Torque restrictor comprises screw (101), nut fitted on screw, drive tube (105) rigidly coupled with said nut and means (109, 133) to actuate said screw. This constrictor is equipped with thrust (115, 119) to prevent revolution of said pipe (105) by friction caused by axial force brought by said screw (101) to said nut at its displacement. It allows rotation of said pipe (105) when the nut is shifted to contact with axial thrust of said screw to exceed preset threshold torque defined by said force.

EFFECT: higher efficiency.

7 cl, 4 dwg

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RU 2 538 476 C2

Authors

Moradell-Casellas Pierre

Dates

2015-01-10Published

2010-04-07Filed