The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 01, 2015

Filed:

May. 08, 2014
Applicant:

Hirobo Co., Ltd., Fuchu-shi, JP;

Inventors:

Takakazu Uebori, Fuchu, JP;

Shunichi Suzuki, Fuchu, JP;

Assignee:

Hirobo Co., Ltd., Hiroshima, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/10 (2006.01); B64C 39/02 (2006.01); G05D 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/10 (2013.01); B64C 39/024 (2013.01); G05D 1/0011 (2013.01); B64C 2201/024 (2013.01); B64C 2201/141 (2013.01); B64C 2201/146 (2013.01);
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.


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