Autogyro Trim Control

Bensen Autogyro Trim Control

Bensen-Autogyro-01-Logo

 

Bensen Aircraft, manufacturer of autogyro aircraft, in Raleigh, North Carolina.

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Steve Hines’ 4th-5th-year-college summer job.

 

       Two years before graduating from college, Steve Hines’ summer job in Research & Development at Bensen Aircraft under the direction of Igor Bensen, pioneer in autogyro aircraft.  


 

      The assignment was to develop an in-flight trim control, to compensate for the shifting weight of the fuel tank, mounted on the front-left.  As the fuel was used, the autogyro would gradually pitch up and roll to the right.  

      Before the summer was out, Steve had filled a notebook with technical ideas, notes, and photos of prototypes.  The solution used a single cable (shown in red) to do two things, to adjust the pitch, and the roll.  Pulling the red cable made the rotor and the craft pitch up.  Pulling the yellow cable changed the angle of the red cable from left to right, to affect the roll of the craft.  The in-flight trim control was successfully test flown by Igor Bensen, in a B-8 Gyrocopter like that shown above.  

     The trim control is based on the geometry of an ellipse which can be drawn with a string attached at two points, the foci. 

      The curved lower edge of the aluminum plate is the part of the circle which closely matches part of an ellipse. 

      The triangular frame swings around a pivot at the center of the circle, approximating an ellipse, within this angle.  This allows the red cable to follow a path, between the two foci of the ellipse, without changing path length.  The red cable pulls on the back of the rotor gimbal (out of view) from different angles which makes the rotor tilt left or right, and makes the craft bank left or right.

     The upper focus of the ellipse is the red cable’s attachment at the back of the gimbal (out of view).  The lower focus is where the intermediate red cable contacts the upper roller.  

      The movable roller swings in an arc, closely simulating a portion of an ellipse. 

 

      Regardless of how the roller swings left or right, the red cable maintains a constant path length between the foci of the ellipse.  Further, pulling the red pitch-control cable, around the rollers and through the mechanism, has no effect on the swing position of the lower roller.  Therefore, there is complete independence between the two adjustments, both of which are controlled by the same red cable in different ways.  

      The lower ends of both the pitch-control cable (red) and the roll-control cable (yellow) are routed with pulleys to adjustment knobs at the pilot’s seat.  The pitch-control knob is mounted on the side of the seat (so that turning the knob makes the autogyro pitch in the same direction that the knob is turned).  The roll-control knob is mounted on the front of the seat, so that rotation of the knob makes the autogyro roll in the same direction that the knob is turned.

 

Steve Hines, left, with Igor Bensen

 


 

      This is not a product for sale, but is shown as an example of technology, developed by Steve Hines, which clients may expect from HinesLab on a contract basis.

 

Please contact Steve Hines at :
HinesLab
Glendale, California, USA
email: Steve@HinesLab.com
ph. 818-507-5812