Invention Grant
- Patent Title: Coaxial counter-rotating unmanned helicopter
- Patent Title (中): 同轴反转无人直升机
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Application No.: US14272839Application Date: 2014-05-08
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Publication No.: US09199729B1Publication Date: 2015-12-01
- Inventor: Takakazu Uebori , Shunichi Suzuki
- Applicant: Hirobo Co., Ltd.
- Applicant Address: JP Hiroshima
- Assignee: Hirobo Co., Ltd.
- Current Assignee: Hirobo Co., Ltd.
- Current Assignee Address: JP Hiroshima
- Agency: The Webb Law Firm
- Main IPC: B64C27/10
- IPC: B64C27/10 ; B64C39/02 ; G05D1/00

Abstract:
To configure the yaw axis control mechanism of a coaxial counter-rotating unmanned helicopter to be able to accurately control the pitch angle of the upper rotor blade by a simple configuration even if the precise adjustment is not performed. A rudder control rod is inserted into a main mast of a coaxial counter-rotating helicopter, a lower end portion thereof is connected to an output lever of the rudder servo, and a mixing rod head is fixed to an upper end portion. A link mechanism connected to the upper swash plate is attached to a side surface portion of the mixing rod head, the vertical displacement of the mixing rod head moving up and down together with the rudder control rod is converted into a displacement for tilting an upper blade holder around the spindle via the link mechanism, thereby changing the pitch angle of the upper rotor blades.
Public/Granted literature
- US20150321754A1 Coaxial Counter-Rotating Unmanned Helicopter Public/Granted day:2015-11-12
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