| タイトル | Centrifugal regulator for control of deployment rates of deployable elements |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800015013 |
| 著者（英） | Vermalle, J. C. |
| 著者所属（英） | Societe Nationale Industrielle Aerospatiale |
| 発行日 | 1980-05-01 |
| 言語 | eng |
| 内容記述 | The requirements, design, and performance of a centrifugal regulator aimed at limiting deployment rates of deployable elements are discussed. The overall mechanism is comprised of four distinct functional parts in a machined housing: (1) the centrifugal brake device, which checks the payout of a deployment cable; (2) the reducing gear, which produces the spin rate necesary for the braking device; (3) the payout device, which allows the unwinding of the cable; and (4) the locking device, which prevents untimely unwinding. The centrifugal regulator is set into operation by a threshold tension of the cable which unlocks the mechanism and allows unwinding. The pulley of the windout device drives the centrifugal brake with the help of the reducing gear. The centrifugal force pushes aside weights that produce friction of the studs in a cylindrical housing. The mechanism behaved well at qualification temperature and vibrations. |
| NASA分類 | MECHANICAL ENGINEERING |
| レポートNO | 80N23504 |
| 権利 | No Copyright |
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