Title:
ヘリコプタのロータ制動装置
Document Type and Number:
Japanese Patent JP3625509
Kind Code:
B2
Abstract:
A helicopter rotor brake device includes a fixed casing. A shaft is supported in a rotationally free manner inside the casing and is rotatably connectable to the rotor. A pair of first friction disks connected to the casing. A hub is fitted integral with a second friction disk interposed axially between the first friction disks and cooperates in a sliding manner with the same when loaded axially. A clutch is interposed between the shaft and the hub and is movable between an idle position corresponding to a rotational disconnection of the hub and the shaft, and an operating position corresponding to a rotational connection of the hub and the shaft.
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Inventors:
Santino Pancotti
Application Number:
JP277695A
Publication Date:
March 02, 2005
Filing Date:
January 11, 1995
Export Citation:
Assignee:
Agusta Sochieta Per Atsushioni
International Classes:
B64C27/12; B64C27/14; F16D55/36; F16D67/02; F16D65/12; (IPC1-7): B64C27/14
Domestic Patent References:
| JP52027951A | ||||
| JP5620840A | ||||
| JP5149351A |
Attorney, Agent or Firm:
Takashi Ishida
Jun Tsuruta
Masaya Nishiyama
Higuchi Souji
Jun Tsuruta
Masaya Nishiyama
Higuchi Souji