Invention Grant
- Patent Title: Magnetorheological flight control clutch system
- Patent Title (中): 磁流变飞行控制离合器系统
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Application No.: US14482603Application Date: 2014-09-10
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Publication No.: US09541142B2Publication Date: 2017-01-10
- Inventor: Pasquale Spina , Carlos A Fenny , Jean-Sebastian Plante , Patrick Chouinard , Jean-Philippe Lucking Bigué , Yves St-Amant
- Applicant: Bell Helicopter Textron Inc.
- Applicant Address: US TX Fort Worth
- Assignee: Bell Helicopter Textron Inc.
- Current Assignee: Bell Helicopter Textron Inc.
- Current Assignee Address: US TX Fort Worth
- Main IPC: F16D37/00
- IPC: F16D37/00 ; B64C27/56 ; B64C27/64 ; B64C27/68 ; B64C27/12 ; B64C27/78 ; B64D35/02 ; F16D37/02 ; B64C13/28 ; B64C27/605 ; B64C27/08 ; B64D35/04 ; F16H25/20

Abstract:
In some embodiments, a redundant control system includes first and second control systems, having first and second clutches, and a shared clutch system. The shared clutch system may include a shared shaft configured to receive mechanical energy from a shared power source, a first shared clutch corresponding to the first clutch and configured to receive mechanical energy from the shared shaft, and a second shared clutch corresponding to the second clutch and configured to receive mechanical energy from the shared shaft. A first linkage provides mechanical communication between an output of the first clutch, an output of the first shared clutch, and a first output device in mechanical communication with the rotor system. A second linkage provides mechanical communication between an output of the second clutch, an output of the second shared clutch, and a second output device in mechanical communication with the rotor system.
Public/Granted literature
- US20150267762A1 Magnetorheological Flight Control Clutch System Public/Granted day:2015-09-24
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