Invention Publication
EP3150489A1 UNIFIED CONTROL OF MULTIPLE ACTIVE SYSTEMS FOR HELICOPTER VIBRATION SUPRESSION
审中-公开
为了降低直升机振动的多个活动系统的统一控制
- Patent Title: UNIFIED CONTROL OF MULTIPLE ACTIVE SYSTEMS FOR HELICOPTER VIBRATION SUPRESSION
- Patent Title (中): 为了降低直升机振动的多个活动系统的统一控制
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Application No.: EP16190182.2Application Date: 2016-09-22
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Publication No.: EP3150489A1Publication Date: 2017-04-05
- Inventor: HEVERLY, David E. , SINGH, Rupinder , LEE, Taeoh , SMITH, Michael
- Applicant: Bell Helicopter Textron Inc.
- Applicant Address: P.O. Box 482 Fort Worth, TX 76101 US
- Assignee: Bell Helicopter Textron Inc.
- Current Assignee: Bell Helicopter Textron Inc.
- Current Assignee Address: P.O. Box 482 Fort Worth, TX 76101 US
- Agency: Lawrence, John
- Priority: US201514871615 20150930
- Main IPC: B64C27/00
- IPC: B64C27/00
Abstract:
A vibration control system 200 for a rotorcraft 100 includes at least one of an integrated actuator 208 and an intermediate actuator 210 associated with a first source of vibration, a sensor configured to sense vibration from the first source of vibration, a dedicated actuator 212 configured for association with a fuselage 106, and a controller 204 configured to receive information from the sensor and configured to control the dedicated actuator and the at least one of the integrated actuator and the intermediate actuator.
Public/Granted literature
- EP3150489B1 UNIFIED CONTROL OF MULTIPLE ACTIVE SYSTEMS FOR HELICOPTER VIBRATION SUPRESSION Public/Granted day:2021-06-16
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