| 摘要 |
1,092,344. Gyroscopic apparatus. AMERICAN BOSCH ARMA CORPORATION. March 16, 1965 [July 20, 1964], No. 11038 / 65. Heading G1C. A gyro rotor 44, which is mounted for rotation on a spherical bearing 46 is run up to speed by being driven from a spiral spring 74, the drive being disconnected when the spring has become unwound. The outer end of the spring is anchored to the gyro housing and its inner end is formed with a bent-over portion forming a catch 86. This engages a lip 88 formed in a drive shaft 56 when the spring is tensioned. The shaft 56 is journalled for rotation in bearings 58, 60 and can also slide axially in these bearings. A release leaf spring 124 acts on a nut 102 screwed on to the shaft 56 and urges the shaft to the right in Fig. 1, but with the spring in its wound condition a roller stop 146 engages one edge of the catch 86 to hold the shaft in the position shown in Fig. 1. In this position finger members 66, 68 on a yoke 64 solid with the shaft 56 engage slots 70, 72 in the web 54 of the rotor 44. Thus rotation imparted to the shaft 56 will drive the rotor 44. When the spring has become unwound the catch 86 disengages from the lip 88 and the stop 146 allowing the spring 124 to move the shaft 156 to the dotted line position shown in Fig. 1 and withdrawing the fingers 66, 68 from the rotor 44. During the transmission of the drive to the rotor, the rotor is caged by a flange 161 on a caging shaft 160 which is urged towards the rotor by a spring 162, the shaft 160 being concentric with and mounted in the shaft 56. As the shaft 56 moves to disconnect the drive, the spring 162 causes the flange 161 to stay in contact with the rotor 44 until the finger members 66, 68 have become disengaged from the rotor, before the flange 161 itself moves clear to allow free rotation of the rotor 44. Before use, the wound spring 74 is held from acting on the shaft 56 by a pawl 114 engaging with a recess in the nut 102. This pawl is released by an explosive charge, when required. The spring 124, as it moves to release the drive to the rotor may actuate a switch to signal that the rotor has been brought to speed. The rotor speed may be monitored by a permanent magnet 194 on the rotor co-operating with a stationary pick-off 196. Attitude pick-offs 180, 184 for the rotor are also provided. |
