Selbstsperrende Zugausgleichseinrichtung fuer ein Steuerseilpaar,insbesondere fuer Flugzeuge

摘要

1,096,238. Control line regulators. PACIFIC SCIENTIFIC CO. April 18, 1966 [June 1, 1965], No. 16888/66. Heading F2G. A shaft 1 turnably supported in a bracket 2 has a splined arm 3 for connection to a controlled member, surface or valve and has extending therethrough a tubular body 5 containing a lock shaft 7 supported at the respective ends thereof by a fitting 6 and a nut 8 engaging a transversely extending spring support bar 9. A compensating spring 10 surrounding the shaft 7 is compressed between the bar 9 and a locking crosshead 11 provided with a hub 12 slidable on the shaft; the crosshead extends outwardly from the hub to outer spring-guide tubes 15, 151 connected to the bar 9 and surrounded by compression springs 17, 171 and the crosshead is connected by links 18, 181 to sectors 20, 201 turnably supported on the shaft hub 4 and having anchored thereto control lines 23, 231. Attached to the sector 20 is a surge lock body 25 containing a rotor 28 which, together with a thrust ring 31, has depressions 29 for the reception of balls 30, the outer surface of the ring 31 having serrations 33 for engagement with opposing serrations 331 on the body 25. The ring 31 is urged toward the rotor 28 by a spring 32 surrounding the rotor hub 26 which carries a pinion 34 that meshes with a gear segment 35 fixed to the sector 201. During normal compensating action of the regulator should the cables contract or expand the springs 10, 17 and 171 expand and contract to permit such action and the sectors 20, 201 turn in opposite directions with respect to one another causing movement of the pinion 34 along the rack 35 which causes the rotor 28 to rotate within the body 25 and the spring 32 holds the ring 31 against the balls 30 to retain the latter in the depressions 29. Should the tension on one cable be increased while the tension on the other cable is slackened a greater force is applied to one of the springs 17, 171 and the crosshead turns slightly upon the shaft 7 causing the hub 12 to bind on the shaft to prevent further deflection of the springs so that the regulator is locked and acts as an ordinary sheave. Breakage of a cable causes excessive angular acceleration between the sectors 20, 201 and turning of the gear segment 35 drives the pinion 34 to rotate the rotor 28 when the balls 30 ride out of the depressions 29 to force outwardly the ring 31 whereby the serrations 33 thereon lock against the serrations 331 on the body 25 thereby immediately stopping relative turning of the two sectors and converting the regulator to a rigid member.